Encyclopedia Astronautica
USAF AFSC


American agency. Air Force Systems Command, USA.

AKA: USAF.

More... - Chronology...


Associated Countries
See also
  • Agency Agencies or institutions overseeing design, development, construction, or operation of space-related systems. More...

Associated Programs

USAF AFSC Chronology


1946 August 22 - . 17:15 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 11. FAILURE: Launch failure..
  • UM Aeronomy Aeronomy mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 0 km ( mi). Summary: Launched 10:15 local time. Launch failure. Carried pressure, density, ionosphere, sky brightness experiments for Air Research and Development Command..

1946 November 21 - . 16:55 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 15.
  • UM Aeronomy Aeronomy / ionosphere mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 100 km (60 mi). Summary: Launched 10:00 local time. Reached 101.6 km. Carried pressure, temperature, ionosphere, sky brightness experiments for Air Research and Development Command..

1947 February 20 - . 18:16 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 20.
  • Blossom I Ionosphere/Biological mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 109 km (67 mi). Launched 11:16 local time. Reached 109.7 km. Carried pressure, ionosphere, sky brightness, biological, photo experiments for Air Research and Development Command. First of a series of V-2 firings known as Blossom Project, tested ejection of canister and its recovery by parachute, containing fruit flies and various types of seeds exposed to cosmic rays.

1948 June 11 - . 10:22 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 37.
  • Blossom III Biological/Ionosphere/Aeronomy mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 63 km (39 mi). Launched 03:22 local time. Reached 62.4 km. Carried pressure, temperature, composition, ionosphere, sky brightness, solar radiation experiments for Air Research and Development Command. Also carried Albert, the first American primate in space, who died of suffocation.

1949 March 22 - . 06:43 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 41.
  • Blossom IVA Ionosphere-solar mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 129 km (80 mi). Summary: Launched 23:43 local time. Reached 133.9 km. Carried Ionosphere, sky brightness, solar radiation, composition, photo experiments for Air Research and Development Command..

1949 June 14 - . 22:35 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 47.
  • Blossom IVB Ionosphere-solar/Biological mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 134 km (83 mi). Launched 15:35 local time. Reached 133.9 km. Carried cosmic and solar radiation, temperature, pressure, ionosphere, photo experiments for Air Research and Development Command. Second V-2 flight carrying a live AF Aero Medical Laboratory monkey, Albert II. The monkey survived but died on impact.

1949 September 16 - . 23:19 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 32. FAILURE: Failure.
  • Blossom IVC Solar/Biological mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 5.00 km (3.10 mi). Launched 16:19 local time. Reached 4.2 km. Carried Composition, ionosphere, meteorites, solar and cosmic radiation, sky brightness, biological experiments for Air Research and Development Command. Third V-2 flight carrying a live AF Aero Medical Laboratory monkey, Albert III. The monkey survived but died on impact.

1949 December 2 - . 22:20 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 1.
  • MX-1011 Solar x-ray / aeronomy / imaging mission - . Nation: USA. Agency: USAF AFSC. Apogee: 96 km (59 mi). Summary: Solar radiation, temperature, photography research. Launched at 1520 local time. Reached 96 km. First firing of USAF Aerobee research rocket (RTV-A-1a) at Holoman AFB, the development of which was initiated earlier in the year..

1949 December 8 - . 19:15 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 31.
  • Blossom IVD Solar/Biological mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 127 km (78 mi). Launched 12:14 local time. Reached 130.6 km. Carried Composition, ionosphere, meteorites, solar radiation, sky brightness experiments for Air Research and Development Command. Last monkey, Albert IV, launched in V-2 series. The successful flight indicated no ill effects on monkey until impact of V-2.

1949 December 15 - . 17:10 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 2. FAILURE: Failure.
  • MX-1011 Solar x-ray / aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 0 km ( mi). Summary: Solar radiation, pressure, temperature, photography research. Launched at 1010 local time. Reached 0.3 km..

1950 March 14 - . 20:43 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 3. FAILURE: Failure.
  • Solar X-rays / Airglow Solar x-ray / ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 3.00 km (1.80 mi). Summary: Solar radiation, sky brightness research. Launched at 1343 local time. Reached 3.2 km..

1950 May 26 - . 19:43 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 4.
  • Insolation Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 67 km (41 mi). Summary: Solar radiation research. Launched at 1243 local time. Reached 67.6 km..

1950 June 2 - . 17:07 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 5.
  • Optical Astronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 24 km (14 mi). Summary: Sky brightness research. Launched at 1007 local time. Reached 24.8 km..

1950 June 20 - . 15:38 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 6.
  • UM T / p Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 93 km (57 mi). Summary: Temperature, pressure research. Launched at 0838 local time. Reached 92.6 km..

1950 August 31 - . 17:09 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 51.
  • Blossom IVG Ionosphere-solar/Biological mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 137 km (85 mi). Launched 10:09 local time. Reached 136.8 km. Carried Ionosphere, meteorites, sky brightness, density, biological experiments for Air Research and Development Command. Last of five Aeromedical Laboratory experiments (first four known as Albert series), it carried a nonanesthetized mouse, photographed by a camera, which survived the impact.

1950 October 12 - . 19:36 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 7.
  • Photo / Temp Imaging mission - . Nation: USA. Agency: USAF AFSC. Apogee: 87 km (54 mi). Summary: Photography research. Launched at 1236 local time. Reached 91.3 km..

1950 November 2 - . 16:29 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 8.
  • Airglow Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 92 km (57 mi). Summary: Airglow research. Launched at 0929 local time. Reached 91.8 km..

1950 December 12 - . 18:26 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 9.
  • UM T / p Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 106 km (65 mi). Summary: Pressure, temperature research. Launched at 1126 local time. Reached 108.2 km..

1951 March 9 - . 03:16 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 57. FAILURE: Failure.
  • Blossom IVE Ionosphere/Aeronomy mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 3.00 km (1.80 mi). Summary: Launched 20:16 local time. Reached 3.1 km. Carried composition, air glow, sky brightness, ionosphere experiments for Air Research and Development Command..

1951 March 28 - . 23:14 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 10.
  • GRD-2 NaCl release Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 66 km (41 mi). Summary: Airglow research. Launched at 1614 local time. Reached 68 km..

1951 April 12 - . 17:26 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 11.
  • Colorado UVS Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 29 km (18 mi). Summary: Solar radiation research. Launched at 1029 local time. Reached 20 km..

1951 April 18 - . 18:39 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 12.
  • Aeromed 1 Biological mission - . Nation: USA. Agency: USAF AFSC. Apogee: 61 km (37 mi). Summary: Biological research. Launched at 1139 local time. Reached 61.2 km. The first Aerobee research rocket containing a biomedical experiment (monkey - name unknown)..

1951 May 29 - . 19:46 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 13. FAILURE: Failure.
  • Ionosphere Propagation Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 4.00 km (2.40 mi). Summary: Ionosphere research. Launched at 1246 local time. Reached 3.7 km..

1951 June 8 - . 00:11 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 14.
  • Solar X-rays / NaCl release Solar x-ray / aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 88 km (54 mi). Summary: Solar radiation, airglow research. Launched at 1711 local time. Reached 88.5 km..

1951 June 28 - . 21:43 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 52. FAILURE: Failure.
  • Blossom IVF Solar/Aeronomy mission - . Nation: USA. Agency: USA; USAF AFSC. Apogee: 6.00 km (3.70 mi). Summary: Launched 14:43 local time. Reached 5.8 km. Carried solar radiation, air glow, sky brightness experiments for Air Research and Development Command..

1951 July 25 - . 16:26 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 15.
  • Airglow / NLC Imager Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 71 km (44 mi). Summary: Sky brightness, photography research. Launched at 0926 local time. Reached 71.3 km..

1951 August 7 - . 16:36 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 16.
  • Ionosphere Propagation Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 83 km (51 mi). Summary: Ionosphere research. Launched at 0036 local time. Reached 83.5 km..

1951 August 30 - . 22:40 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1b. LV Configuration: Aerobee RTV-A-1b USAF 17.
  • Rocket test - . Nation: USA. Agency: USAF AFSC. Apogee: 75 km (46 mi). Summary: Rocket performance test. Launched at 1540 local time. Reached 75.7 km..

1951 September 13 - . 11:37 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 18.
  • UM T / p Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 76 km (47 mi). Summary: Pressure, temperature research. Launched at 0437 local time. Reached 75.7 km..

1951 September 20 - . 16:31 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 19.
  • Aeromed 2 Biological mission - . Nation: USA. Agency: USAF AFSC. Apogee: 71 km (44 mi). Biological research. Launched at 0931 local time. Reached 70.8 km. USAF made first successful recovery of animals from a rocket flight when an instrumented monkey (Yorick aka Albert VI) and 11 mice survived an Aerobee flight to an altitude of 70.8 km from Holloman AFB.

1951 October 17 - . 18:17 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 20.
  • Ionosphere Propagation Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 114 km (70 mi). Summary: lonosphere research. Launched at 1117 local time. Reached 114..3 km..

1952 January 30 - . 20:45 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 21. FAILURE: Failure..
  • AF / Utah Ionosphere 1 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 0 km ( mi). Summary: Ionosphere research. Launched at 1345 local time. Failure..

1952 February 19 - . 14:49 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1c. LV Configuration: Aerobee RTV-A-1c USAF 22. FAILURE: Failure.
  • Airglow Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 0 km ( mi).

1952 February 29 - . 14:40 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 23.
  • Airglow Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 88 km (54 mi). Summary: Sky brightness research. Launched at 0740 local time. Reached 89.3 km..

1952 April 22 - . 17:28 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 24.
  • Ionosphere Propagation Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 116 km (72 mi). Summary: Ionosphere research. Launched at 1028 local time. Reached 112.7 km..

1952 May 1 - . 15:42 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 25.
  • Solar flux Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 91 km (56 mi).

1952 May 21 - . 15:15 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 26.
  • Aeromed 3 Biological mission - . Nation: USA. Agency: USAF AFSC. Apogee: 61 km (37 mi). Biological research. Launched at 0818 local time. Reached 26.1 km. Air Force Aerobee rocket placed an aeromedical payload containing two Phillipine monkeys (Pat and Mike) and two mice to an altitude of 26.1 km, which were recovered unharmed and without apparent ill effect.

1952 June 18 - . 17:50 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 27.
  • UV / Opt spectrographs Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 100 km (60 mi). Summary: Solar radiation research. Launched at 1050 local time. Reached 99.8 km..

1952 June 30 - . 14:32 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 28.
  • AF Airglow 1 Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 101 km (62 mi). Summary: Sky brightness research. Launched at 0732 local time. Reached 101.4 km..

1952 August 26 - . 18:53 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 29. FAILURE: Failure..
  • AF / Utah Ionosphere 2 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 32 km (19 mi). Summary: Ionosphere research. Launched at 1153 local time. Altitude not reported; possible failure..

1952 October 10 - . 14:24 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 30.
  • UV / Opt spectrographs Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 101 km (62 mi). Summary: Solar radiation research. Launched at 0724 local time. Reached 109.5 km..

1952 October 22 - . 14:35 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 31.
  • T-day Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 100 km (60 mi). Summary: Pressure, temperature research. Launched at 0735 local time. Reached 99.8 km..

1952 November 6 - . 15:56 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 32.
  • AF Airglow 2 Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 76 km (47 mi). Summary: Sky brightness research. Launched at 0858 local time. Reached 75.7 km..

1952 December 12 - . 19:38 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1. LV Configuration: Aerobee RTV-A-1 USAF 33.
  • Colorado / UVS? Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 88 km (54 mi). Summary: Solar radiation research. Launched at 1238 local time. Reached 88.5 km..

1953 February 18 - . 17:42 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 34.
  • Heating / beacon test - . Nation: USA. Agency: USAF AFSC. Apogee: 117 km (72 mi). Summary: Rocket performance test. Launched at 1042 local time. Reached 117.5 km..

1953 April 14 - . 15:47 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 35.
  • Heating test - . Nation: USA. Agency: USAF AFSC. Apogee: 122 km (75 mi). Summary: Rocket performance test. Launched at 0847 local time. Reached 122.3 km..

1953 May 20 - . 14:04 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 36.
  • AF Airglow 3 Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 114 km (70 mi). Summary: Sky brightness, day airglow research. Launched at 0704 local time. Reached 114.3 km..

1953 May 21 - . 15:47 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 37.
  • AF Airglow 4 Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 114 km (70 mi). Summary: Sky brightness, day airglow research. Launched at 0847 local time. Reached 114.3 km..

1953 June 26 - . 19:10 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 38.
  • AF / Utah Ionosphere 3 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 135 km (83 mi). Summary: Ionosphere research. Launched at 1210 local time. Reached 135.2 km..

1953 July 1 - . 17:52 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 39.
  • AF / Utah Ionosphere 4 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 138 km (85 mi). Summary: Ionosphere research. Launched at 1052 local time. Reached 138.4 km..

1953 July 14 - . 15:30 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 40.
  • Solar flux Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 103 km (64 mi). Summary: Solar radiation research. Launched at 0830 local time. Reached 103 km..

1953 July 23 - . 09:47 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 41.
  • Airglow spectrograph Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 95 km (59 mi). Summary: Atmospheric composition research. Launched at 0247 local time. Reached 95.6 km..

1953 September 15 - . 15:02 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 42. FAILURE: Early cut-off due to a thrust chamber burn-through..
  • AF Airglow 5 Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 32 km (19 mi). Summary: Sky brightness research. Launched at 0802 local time. Reached 32.2 km. Suffered an early cut-off due to a thrust chamber burn-through. Improved chamber cooling was developed in subsequent engines..

1953 October 7 - . 17:00 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 43.
  • Solar spectrum Solar mission - . Nation: USA. Agency: USAF AFSC. Apogee: 100 km (60 mi). Summary: Solar radiation research. Launched at 1000 local time. Reached 99.8 km..

1953 November 2 - . 18:32 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 44.
  • AF / Utah Ionosphere 5 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 120 km (70 mi). Summary: Ionosphere research. Launched at 1132 local time. Reached 120.7 km..

1953 November 3 - . 18:15 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 45.
  • AF / Utah Ionosphere 6 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 121 km (75 mi). Summary: Ionosphere research. Launched at 1115 local time. Reached 121.5 km..

1954 May 11 - . 15:00 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 46.
  • Beacon test - . Nation: USA. Agency: USAF AFSC. Apogee: 98 km (60 mi). Summary: Rocket performance test. Launched at 0800 local time. Reached 98.2 km..

1954 June 2 - . 16:10 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 47.
  • Solar ultraviolet spectrum test - . Nation: USA. Agency: USAF AFSC. Apogee: 93 km (57 mi). Summary: Rocket performance test. Launched at 0910 local time. Reached 93.4 km..

1954 July 14 - . 13:55 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 48.
  • UM wind vanes Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 92 km (57 mi). Summary: Temperature, aspect research. Launched at 0855 local time. Reached 91.8 km..

1954 August 11 - . 17:25 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 49.
  • AF / Utah D-layer Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 92 km (57 mi). Summary: Ionosphere research. Launched at 1025 local time. Reached 91.8 km..

1954 September 17 - . 14:31 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 50.
  • Solar flux Solar ultraviolet mission - . Nation: USA. Agency: USAF AFSC. Apogee: 94 km (58 mi). Summary: Solar radiation research. Launched at 1731 local time. Reached 94.7 km..

1955 January 22 - . 00:45 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 51.
  • Sodium Release 1 Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 94 km (58 mi). Summary: Airglow research. Launched at 1754 local time. Reached 94.8 km..

1955 February 7 - . 18:51 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a USAF 52.
  • AF / Utah D-layer Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 120 km (70 mi). Summary: Ionosphere research. Launched at 1151 local time. Reached 120.4 km..

1956 November 1 - . 12:57 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee AJ10-34. LV Configuration: Aerobee AJ10-34 USAF 73.
  • Sodium Release Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 66 km (41 mi). Summary: Sodium emission research. Launched at 0557 local time. Reached 68 km..

1956 November 2 - . 05:39 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee AJ10-34. LV Configuration: Aerobee AJ10-34 USAF 74.
  • Sodium Release 4 Aeronomy mission - . Nation: USA. Agency: USAF AFSC. Apogee: 146 km (90 mi).

1956 December 13 - . 21:44 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee Hi. LV Configuration: Aerobee Hi USAF 75.
  • AJ11-6 engine test - . Nation: USA. Agency: USAF AFSC. Apogee: 193 km (119 mi). Summary: Rocket test, 80 kg payload payload. Launched at 1444 local time. Reached 193 km..

1957 February 2 - . 08:05 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee AJ10-34. LV Configuration: Aerobee AJ10-34 USAF 76.
  • Firefly (Ethelyne) Aeronomy / chemical release mission - . Nation: USA. Agency: USAF AFSC. Apogee: 143 km (88 mi). Summary: Ethylene gas release (Firefly). Launched at 0105 local time. Reached 140.6 km..

1957 April 9 - . 15:19 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee AJ10-25. LV Configuration: Aerobee AJ10-25 USAF 77.
  • Meteorites mission - . Nation: USA. Agency: USAF AFSC. Apogee: 61 km (37 mi). Summary: Micrometeorites research. Launched at 0819 local time. Reached 61 km..

1957 June 18 - . 14:00 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee Hi. LV Configuration: Aerobee Hi USAF 78.
  • AU4.26 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 171 km (106 mi). Summary: Ionosphere research. Launched at 0700 local time. Reached 171 km..

1957 June 25 - . 14:07 GMT - . Launch Site: Holloman. Launch Complex: Holloman A. LV Family: Aerobee. Launch Vehicle: Aerobee Hi. LV Configuration: Aerobee Hi USAF 79.
  • AU4.27 Ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 202 km (125 mi). Summary: Ionosphere research. Launched at 0707 local time. Reached 202 km..

1962 February 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I SM-18. FAILURE: Failure.
  • Research and development Cat II / operational test - . Nation: USA. Agency: USAF AFSC. Apogee: 50 km (31 mi).

1962 May 4 - . 21:43 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I SM-34.
  • Research and development Category II test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1962 June 7 - . 18:21 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-1.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 July 11 - . 18:51 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-6.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 July 25 - . 16:17 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-4.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 September 12 - . 15:50 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-5.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 October 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I SM-35.
  • Research and development Category II test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1962 October 12 - . 16:24 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-9.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 October 19 - . 18:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 14F.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1962 October 26 - . 10:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 159D.
  • NTMP K-5 / Pod 20 Target - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1962 October 26 - . 17:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-12.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1962 November 7 - . 19:43 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 16F.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1962 November 11 - . 20:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 128D / Agena B SPS 2405.
  • FTV 2405 RV - . Payload: E-6 RV. Nation: USA. Agency: USAF AFSC. Spacecraft: Samos. COSPAR: 1962-B-Pi-xx.
  • TRS 1 - . Payload: ERS 1. Nation: USA. Agency: USAF AFSC. Class: Earth. Type: Magnetosphere satellite. Spacecraft: ERS. COSPAR: 1962-B-Pi-xx.

1962 November 14 - . 22:36 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 13F. FAILURE: Failure. Failed Stage: 1.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 300 km (180 mi).

1962 December 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I SM-11.
  • Research and development Category II test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1962 December 5 - . 21:25 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 21F.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi). Summary: Last Atlas F R&D flight..

1962 December 6 - . 20:31 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-11. FAILURE: Failure.
  • Mk 4 re-entry vehicle test - . Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi). Titan II flight N-11, the eighth in a series being conducted by the Air Force to develop the weapon system, was launched from Cape Canaveral. It carried a design change intended to reduce the amplitude of longitudinal oscillations which had appeared during first stage operation on all seven previous Titan II flights. This phenomenon, which subsequently became known as POGO, generated g-forces as high as nine in the first stage and over three at the position on the missile corresponding to the location of the spacecraft on the Gemini launch vehicle. Fearing the potentially adverse effect on astronaut performance of such superimposed g-forces, NASA established 0.25g at 11 cycles per second as the maximum level tolerable for Gemini flights. As a first try at solving the POGO problem, Titan II N-11 carried standpipes in each leg of the stage I oxidizer feed lines to interrupt the coupling between the missile's structure and its propulsion system. This coupling was presumed to be the cause of the instability. Postflight analysis, however, revealed that the POGO fix was unsuccessful; longitudinal oscillation had actually been multiplied by a factor of two.

1962 December 12 - . 11:38 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 161D.
  • NTMP K-6 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1962 December 17 - . 20:36 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 131D / Agena B 1205. FAILURE: Failure.
  • TRS 4 - . Payload: ERS 4. Nation: USA. Agency: USAF AFSC. Spacecraft: Midas. COSPAR: F621217C.
  • TRS 3 - . Payload: ERS 3. Nation: USA. Agency: USAF AFSC. Spacecraft: Midas. COSPAR: F621217B.

1962 December 18 - . 17:26 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF1. LV Family: Atlas. Launch Vehicle: Atlas E. LV Configuration: Atlas E 64E. FAILURE: Failure. Failed Stage: 1.
  • NTMP K-4 ABM test - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1962 December 19 - . 20:08 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-13.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 January 10 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-15. FAILURE: Failure.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi).

1963 January 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I SM-8.
  • Research and development Category II test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1963 February 6 - . 17:59 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-16.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 February 16 - . 21:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-7. FAILURE: Failure.
  • Awful Tired - . Nation: USA. Agency: USAF AFSC. Apogee: 5.00 km (3.10 mi). Summary: Research and development launch - Mk 6 re-entry vehicle.

1963 March 1 - . 21:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 134F.
  • ABRES REX-I / Pod 1 Re-entry vehicle test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1963 March 21 - . 15:23 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-18.
  • Mk 6 re-entry vehicle test launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 March 21 - . 21:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 83F.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1963 April 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I V-1.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1963 April 11 - . 20:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 534.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 April 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 565.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 April 19 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-21. FAILURE: Failure.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi). Summary: Mk 6 re-entry vehicle.

1963 April 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 585.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 April 24 - . 20:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF1. LV Family: Atlas. Launch Vehicle: Atlas E. LV Configuration: Atlas E 65E.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,600 km (900 mi). Summary: First successful E missile from OSTF-1, SMS 576.

1963 April 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-8.
  • Dinner Party - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: Research and development launch. Mk 6 re-entry vehicle..

1963 April 27 - . 02:03 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 135F.
  • ABRES REX-II re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1963 April 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 595.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 May 1 - . 10:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-A1. LV Family: Titan. Launch Vehicle: Titan 1. LV Configuration: Titan I V-4. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC.

1963 May 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 604.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 May 9 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-14. FAILURE: Failure.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi). Summary: Mk 6 re-entry vehicle..

1963 May 9 - . 20:06 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 119D / Agena B S01 1206.
1963 May 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-D. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-19.
  • Flying Frog - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: Research and development launch. Mk 6 re-entry vehicle..

1963 May 18 - . 17:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 425B. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1963 May 24 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 658.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 May 24 - . 17:33 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-17.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: Mk 6 re-entry vehicle.

1963 May 29 - . 03:45 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 428.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 May 29 - . 16:56 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC16. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-20. FAILURE: Failed 55 seconds after launch.. Failed Stage: 1.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Titan II flight N-20, the 19th in the series of Air Force research and development flights, was launched from Cape Canaveral. It carried oxidizer standpipes and fuel accumulators to suppress longitudinal oscillations (POGO). During the spring of 1963, static firings of this configuration had been successful enough to confirm the hypothesis that POGO was caused by coupling between the missile structure and its propulsion system, resulting in an unstable closed loop system. Standpipes and accumulators, by interrupting the coupling reduced the source of instability. Flight N-20 failed 55 seconds after launch and yielded no POGO data. Although the failure was not attributed to the installed POGO fix, Air Force Ballistics Systems Division decided officially that no further Titan II development flights would carry the POGO fix because so few test flights remained to qualify the weapon system operationally. This decision did not stand, however, and the POGO fix was flown again on N-25 (November 1), as well as on two later flights.

1963 June 4 - . 20:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF1. LV Family: Atlas. Launch Vehicle: Atlas E. LV Configuration: Atlas E 62E.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,600 km (900 mi).

1963 June 6 - . 03:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 427.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 June 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 139D / Agena B SPS 1204. FAILURE: Failure.
  • TRS 8 - . Payload: ERS 8. Nation: USA. Agency: USAF AFSC. Spacecraft: Midas. COSPAR: F630613C.
  • TRS 7 - . Payload: ERS 7. Nation: USA. Agency: USAF AFSC. Spacecraft: Midas. COSPAR: F630613B.

1963 June 20 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-22.
  • Thread Needle - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: Research and development launch. Mk 6 re-entry vehicle..

1963 June 28 - . 02:34 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 429.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 July 1 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 431.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 July 5 - . 21:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 1A. LV Configuration: Minuteman 1A 518.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 July 16 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 430. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1963 July 19 - . 03:51 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Agena B. LV Configuration: Atlas Agena B 75D / Agena B S01 1207.
  • TRS 10 - . Payload: ERS 10. Nation: USA. Agency: USAF AFSC. Class: Earth. Type: Magnetosphere satellite. Spacecraft: ERS. COSPAR: 1963-030xx.

1963 July 24 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 432.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 August 5 - . 16:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 433. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 100 km (60 mi).

1963 August 21 - . 23:23 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-24.
  • Research and development / Pod T-202 test / plume study mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Titan II development flight N-24 was launched from the Atlantic Missile Range. This was the first of five flight tests in the Gemini malfunction detection system (MDS) piggyback series. All MDS parameters were lost 81 seconds after liftoff because of a short circuit in the MDS. Operation in the second flight (N-25 on November 1) was normal except for two minor instrumentation problems. Three more test flights (N-29 on December 12, 1963; N-31 on January 15, 1964; and N-33 on March 23, 1964) verified the performance of the Gemini MDS under actual conditions of flight environment and engine operation.

1963 August 27 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 435.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 August 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 625.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 September 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-D. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-23.
  • Tar Top - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: Research and development launch. Mk 6 re-entry vehicle..

1963 September 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 770.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 October 4 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 695.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 October 4 - . 05:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 45F. FAILURE: Failure. Failed Stage: 1.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC.

1963 October 28 - . 03:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 136F. FAILURE: Failure. Failed Stage: 1.
  • ABRES WAC-1 / Pod 21 Reentry test / plume mission - . Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi).

1963 November 1 - . 20:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-25.
  • Research and development / Pod T test / plume study mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Titan II development flight N-25 was launched from the Atlantic Missile Range. It carried the oxidizer surge chamber and fuel accumulator kit intended to reduce the amplitude of longitudinal vibration which had characterized earlier flights. NASA regarded 0.25g as the maximum level tolerable in manned space flight; this flight achieved a level of 0.22g, the first to fall within acceptable limits. Although the kit had been tested on only one flight, Gemini Project Office had sufficient confidence in it to decide, on November 6, to procure several more such kits for subsequent installation in Gemini launch vehicles. Two later Titan II development flights (N-29 on December 12, 1963, and N-31 on January 15, 1964) and the flight of Gemini-Titan 1 confirmed the validity of this decision. The required kits for the remaining Gemini launch vehicles were then procured.

1963 November 7 - . 17:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 434. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1.00 km (0.60 mi).

1963 November 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-27.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 November 13 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 446.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 December 12 - . 20:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-29.
  • Research and development / Pod T test / plume study mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 December 17 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-D. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-28.
  • Research and development / Pod T? test / plume study mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1963 December 18 - . 22:56 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg OSTF2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 109F.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1963 December 19 - . 06:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 447.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 January 15 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-31.
  • Research and development / Pod T test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 January 16 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 438.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 January 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-26.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 January 28 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 448.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 February 13 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 436.
  • Research and development [After 48E] test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 February 17 - . 16:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-B. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II B-15.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 February 25 - . 20:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas E. LV Configuration: Atlas E 5E.
  • ABRES WAC-3 / Pod 18 Re-entry vehicle test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,600 km (900 mi).

1964 February 26 - . 01:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 437.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 February 26 - . 20:15 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-32.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 February 28 - . 02:04 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 439.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 March 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 395-C. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-30.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 March 13 - . 17:05 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 440.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 March 20 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 442.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 March 24 - . 01:42 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-33.
  • Research and development / Pod T-207 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 March 31 - . 02:33 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 441.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 April 1 - . 20:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC11. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 137F.
  • ABRES WAC-2 / Pod 2 Reentry test / plume mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1964 April 7 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 443.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 April 9 - . 20:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC15. LV Family: Titan. Launch Vehicle: Titan 2. LV Configuration: Titan II N-3A.
  • Research and development / Pod RVIP test / plume study mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). This Air Force conducted test program contributed significantly to the development of the Gemini launch vehicle; the Gemini malfunction detection system was tested on five flights, Gemini guidance components on three, and the longitudinal oscillation fix on four. In addition to flight testing these (and other) critical components, these flights also enhanced confidence in the use of the Titan II as a launch vehicle. Thirty-two Titan II test flights were analyzed to determine whether any characteristic of the flight would have demanded a Gemini abort; 22 were adjudged successful from the standpoint of a Gemini mission, nine would have required Gemini to abort, and one resulted in a prelaunch shutdown.

1964 April 24 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 444.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 June 29 - . 21:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1141.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 September 24 - . 16:04 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 449.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 September 29 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 445. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1.00 km (0.60 mi).

1964 October 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Atlas. Launch Vehicle: Atlas Agena D SLV-3. LV Configuration: SLV-3 Agena D 7103 / Agena D. FAILURE: Failure.
1964 October 23 - . 18:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4W. LV Family: Atlas. Launch Vehicle: Atlas Agena D. LV Configuration: Atlas Agena D 353D / Agena D.
  • OPS 5063 - . Payload: EHH A4. Nation: USA. Agency: USAF AFSC. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: SSF. Decay Date: 1965-02-23 . USAF Sat Cat: 914 . COSPAR: 1964-068xx. Apogee: 185 km (114 mi). Perigee: 185 km (114 mi). Inclination: 95.4000 deg. Period: 88.20 min.

1964 October 29 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 450.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 December 15 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 451.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1964 December 19 - . 00:07 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 452.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 January 29 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 453.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 March 26 - . 09:01 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 297D.
  • ABRES LORV-7 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 April 6 - . 13:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 150D.
  • ABRES WAC-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 May 8 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 455.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 May 26 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 456.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 May 28 - . 02:54 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 68D / OV-1. FAILURE: Failure.. Failed Stage: 1.
  • OV1-03 - . Nation: USA. Agency: USAF AFSC. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1965-05-28 . COSPAR: F650528A.

1965 June 3 - . 10:38 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 177D.
  • NTMP RMV-304 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 June 8 - . 15:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 299D.
  • ABRES LORV-6 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 June 10 - . 12:26 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 302D.
  • NTMP RMV-303 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 July 1 - . 09:54 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 59D.
  • NTMP KX-32 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 July 12 - . 19:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Atlas. Launch Vehicle: Atlas Agena D SLV-3. LV Configuration: SLV-3 Agena D 7112 / Agena D. FAILURE: Failure.
1965 August 4 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 457.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 August 4 - . 12:43 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 183D.
  • ABRES WAC-5 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 August 5 - . 13:21 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 147F.
  • ABRES LORV-2A re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1965 August 18 - . 11:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2001.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 August 23 - . 20:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 454.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 August 26 - . 11:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 61D.
  • NTMP KX-41 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 September 24 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 458.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 September 29 - . 10:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 125D.
  • NTMP KX-45 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 October 1 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 459.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 October 5 - . 09:07 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 34D.
  • OV1-02S - . Nation: USA. Agency: USAF AFSC. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 1613 . COSPAR: 1965-078xx. Apogee: 2,418 km (1,502 mi). Perigee: 401 km (249 mi). Inclination: 144.2000 deg. Period: 114.00 min.
  • NB20.170 - . Payload: SPP 29. Nation: USA. Agency: USAF AFSC. Spacecraft: OV1. USAF Sat Cat: 1613 . COSPAR: 1965-078xx. Apogee: 2,418 km (1,502 mi). Perigee: 401 km (249 mi). Inclination: 144.2000 deg. Period: 114.00 min.

1965 October 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF22. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2002.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 November 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2009.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 November 29 - . 14:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 200D.
  • NTMP KX-33 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 December 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF24. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2017.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1965 December 20 - . 13:39 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 85D.
  • NTMP KX-31 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1965 December 21 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. LV Family: Titan. Launch Vehicle: Titan 3C. LV Configuration: Titan IIIC 3C-8.
  • Transtage 8 - . Nation: USA. Agency: USAF AFSC. Spacecraft: OV2. Decay Date: 1975-08-17 . USAF Sat Cat: 1863 . COSPAR: 1965-108xx. Apogee: 22,114 km (13,740 mi). Perigee: 337 km (209 mi). Inclination: 26.9000 deg. Period: 387.40 min.

1966 January 5 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 461.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 January 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2053.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 January 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2022.
  • Force modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 February 10 - . 09:48 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 305D.
  • NTMP KX-38 / Pod 32 Reentry test / plume mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 February 11 - . 01:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 460.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 February 11 - . 13:04 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 86D.
  • NTMP KX-51 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 February 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF25. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2033.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 February 19 - . 09:56 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 73D.
  • NTMP KX-47 Re-entry Vehicle test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 March 4 - . 12:29 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 303D. FAILURE: Failure. Failed Stage: 1.
  • NTMP KX-35 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi).

1966 March 17 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2049. FAILURE: Failure.
  • Force modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 March 19 - . 12:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 304D.
  • NTMP KX-43 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 March 30 - . 09:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 72D.
  • OV1-04S - . Nation: USA. Agency: USAF AFSC. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. USAF Sat Cat: 2121 . COSPAR: 1966-025xx. Apogee: 1,002 km (622 mi). Perigee: 879 km (546 mi). Inclination: 144.5000 deg. Period: 103.80 min.

1966 April 1 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 462.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 May 3 - . 10:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 208D. FAILURE: Failure. Failed Stage: 1.
  • NTMP KX-37 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi).

1966 May 13 - . 11:43 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 98D.
  • ABRES WAC-5A re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 May 26 - . 12:04 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 41D.
  • NTMP KX-47 Re-entry Vehicle test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 June 10 - . 11:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 96D.
  • NTMP KX-42 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 June 24 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2083.
  • Force modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 June 26 - . 15:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 147D.
  • NTMP KX-20 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 June 30 - . 10:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 298D.
  • NTMP KX-39 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 July 9 - . 02:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 463.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 July 14 - . 02:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 58D. FAILURE: Partial Failure..
  • OV1-08 PasComSat - . Nation: USA. Agency: USAF AFSC. Class: Earth. Type: Magnetosphere satellite. Spacecraft: OV1. Decay Date: 1978-01-04 . USAF Sat Cat: 2324 . COSPAR: 1966-063xx. Apogee: 410 km (250 mi). Perigee: 393 km (244 mi). Inclination: 144.2000 deg. Period: 92.60 min.

1966 July 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2045. FAILURE: Failure.
  • Force modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1966 August 8 - . 17:47 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 149F. FAILURE: Failure. Failed Stage: 1.
  • ABRES MBRV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi).

1966 October 11 - . 19:59 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 115F. FAILURE: Failure. Failed Stage: 1.
  • ABRES SBGRV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 50 km (31 mi).

1966 December 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2036.
  • ERCS 1 Communications mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: First Emergency Rocket Communications Satellite test.

1966 December 21 - . 22:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas SLV-3. LV Configuration: Atlas SLV-3 7001.
  • Prime 1 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,500 km (900 mi). The first test of the X-23A SV-5D lifting body re-entry shape. It was a zero cross-range suborbital flight, with recovery 6935 km downrange. The ballute deployed at 30.440 m, followed by the main parachute at 13,700 m, and the vehicle was descending within 275 m of the target point. Nevertheless the air-snatch was unsuccessful, and the vehicle sank. However 90% of the planned telemetry was successfully transmitted by radio.

1967 January 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2073.
  • Force modification research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 January 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 4300C. Launch Pad: 4300C. LV Family: Sergeant. Launch Vehicle: Castor.
  • Marquardt Scramjet Technology mission - . Nation: USA. Agency: USAF AFSC. Apogee: 54 km (33 mi).

1967 January 18 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 464.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 January 18 - . 01:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 148F.
  • ABRES TVX-13 (21) re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 January 22 - . 15:44 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 35D.
  • ABRES Mk 12R PDV re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1967 February 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2087.
  • ERCS 2 Communications mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 February 13 - . 22:05 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 121F.
  • ABRES TX-22 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 February 25 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 465.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 March 5 - . 23:05 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas SLV-3. LV Configuration: Atlas SLV-3 7002.
  • Prime 2 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,500 km (900 mi). Summary: The X-23A SV-5D lifting body vehicle demonstrated a 1055 km cross-range manoeuvre, but again air snatch failed..

1967 March 16 - . 17:56 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 151F.
  • ABRES MBRV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 April 7 - . 11:19 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 38D.
  • ABRES AX-1 / Pod 30 Reentry test / ionosphere mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1967 April 17 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2143.
  • ERCS 3 Communications mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: Last Emergency Rocket Communications Satellite test.

1967 April 20 - . 01:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas SLV-3. LV Configuration: Atlas SLV-3 7003.
  • Prime 3 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,500 km (900 mi). The full design 1145 km cross range was demonstrated, and the X-23A SV-5D lifting body vehicle was successfully snatched at 3700 m altitude, 8 km from the target point. With this success the rest of the project was cancelled, and the two remaining unflown X-22A's were sent to the USAF Museum at Wright Patterson Air Force Base.

1967 April 28 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1019.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 May 11 - . 14:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2095.
  • Force modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 May 19 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 667.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 May 19 - . 22:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 119F.
  • ABRES SBGRV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 June 9 - . 10:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 122F.
  • ABRES SPDS (RMP-B-1) re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 June 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 751.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 July 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 65D.
  • ABRES PDV re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1967 July 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2337.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 July 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 755.
  • GIN BABY I research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 July 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 114F.
  • RMP-B-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 July 27 - . 19:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 92D. FAILURE: Partial Failure..
  • OV1-11 - . Nation: USA. Agency: USAF AFSC. Spacecraft: OV1. Decay Date: 1972-02-22 . USAF Sat Cat: 2893 . COSPAR: 1967-072xx. Apogee: 146 km (90 mi). Perigee: 144 km (89 mi). Inclination: 101.7000 deg. Period: 87.40 min. Summary: OV-1 11 did not reach orbit..

1967 July 29 - . 08:48 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 150F.
  • ABRES MBRV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 August 17 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 466.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 October 11 - . 11:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 69D.
  • ABRES TVX-13 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1967 October 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 118F.
  • ABRES MBRV-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 October 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 81F. FAILURE: Failure. Failed Stage: 1.
  • RMP-B-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1.00 km (0.60 mi).

1967 November 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 820.
  • GIN BABY II research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 November 7 - . 00:56 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 467.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 November 7 - . 13:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 94D.
  • ABRES Mk 11 AX-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi). Summary: Final launch of an Atlas D missile (first operational at Vandenberg on 9 September 1959)..

1967 November 10 - . 12:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 113F.
  • ABRES BGRV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 November 17 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2386.
  • GIN BABY III research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 November 21 - . 14:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2071.
  • Research and technology/modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 December 8 - . 21:03 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 948.
  • GIN BABY IV research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 December 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 117F.
  • RMP-B-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1967 December 28 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2435.
  • GIN BABY V research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1968 January 31 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 94F.
  • RMP-B-5 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 February 7 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 468.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1968 February 10 - . 11:42 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2307.
  • Research and technology/modification test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1968 February 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 116F.
  • ABRES BGRV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi). Summary: The Boost Glide Re-entry Vehicle was launched from Vandenberg AFB, California to the area of Wake Island in the Pacific Ocean. It was launched from an Atlas missile booster and served to provide data on hypersonic manoeuvring flight characteristics..

1968 March 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident E. LV Configuration: Atlas E/Trident 74E.
  • RMP-B-6 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,600 km (900 mi).

1968 April 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas E. LV Configuration: Atlas E 77E.
  • ABRES RVTO-1A-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,600 km (900 mi).

1968 April 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident E. LV Configuration: Atlas E/Trident 78E.
  • RMP-B-7 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,600 km (900 mi).

1968 May 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 95F. FAILURE: Failure. Failed Stage: 1.
  • ABRES Penaid TVX re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 100 km (60 mi).

1968 June 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A2. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 89F.
  • ABRES PDV re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 June 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 86F.
  • RMP-B-8 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 June 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 32F.
  • ABRES RVTO-1A-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 August 16 - . 20:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-201.
  • Research and development test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). Summary: First Minuteman III flight test missile launched from Vandenberg AFB..

1968 August 16 - . 20:57 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3E. LV Family: Atlas. Launch Vehicle: Atlas Burner 2. LV Configuration: Atlas Burner 2 7004 / Burner-2 (No Agena). FAILURE: Failure.
  • EGRS 11 - . Payload: EGRS 11. Nation: USA. Agency: USAF AFSC. Spacecraft: Orbiscal. COSPAR: F680816J.
  • EGRS 12 - . Payload: EGRS 12. Nation: USA. Agency: USAF AFSC. Spacecraft: Orbiscal. COSPAR: F680816I.
  • OV5-8 - . Payload: OV5-8. Nation: USA. Agency: USAF AFSC. Spacecraft: OV5. COSPAR: F680816H.
  • Radcat - . Payload: Radcat. Nation: USA. Agency: USAF AFSC. Spacecraft: Radcat. COSPAR: F680816G.
  • Orbiscal 1 - . Payload: Orbiscal 1. Nation: USA. Agency: USAF AFSC. Spacecraft: Orbiscal. COSPAR: F680816F.
  • AVL-802 Grid Sphere 7-2 - . Payload: AVL-802. Nation: USA. Agency: USAF AFSC. Spacecraft: Calsphere. COSPAR: F680816B.
  • RM-18 - . Payload: RM-18. Nation: USA. Agency: USAF AFSC. Spacecraft: RM. COSPAR: F680816E.
  • AVL-802 Mylar Sphere - . Payload: AVL-802. Nation: USA. Agency: USAF AFSC. Spacecraft: Calsphere. COSPAR: F680816D.
  • AVL-802 Grid Sphere 7-1 - . Payload: AVL-802. Nation: USA. Agency: USAF AFSC. Spacecraft: Orbiscal. COSPAR: F680816C.
  • AVL-802 Rigid Sphere - . Payload: AVL-802. Nation: USA. Agency: USAF AFSC. Spacecraft: Calsphere. COSPAR: F680816L.

1968 September 1 - . 18:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 1442.
  • ST (Partial fuel) - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1968 September 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 99F.
  • RMP-B-9 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 September 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 84F.
  • RVTO-1A-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 October 24 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-202.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1968 November 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 56F. FAILURE: Failure. Failed Stage: 1.
  • RMP-B-10 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1968 November 24 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 60F.
  • RVTO-1A-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1968 December 20 - . 14:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2418.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 January 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 70F.
  • RMP-B-11 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1969 January 29 - . 10:34 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2504.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 January 29 - . 13:52 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2240.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 March 7 - . 08:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF05. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2252.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 March 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2415.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 March 26 - . 20:47 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-203.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 April 11 - . 08:55 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-301.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 April 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF25. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2287.
  • ST 3 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 April 22 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-204.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 May 2 - . 08:42 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2505.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 May 27 - . 20:55 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-205.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 May 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-302.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 June 20 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2320.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 June 25 - . 20:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-206.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 July 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2357.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 July 31 - . 21:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-207.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 August 20 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 112F.
  • ABRES RVTO-1A-5 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1969 September 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-303.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 September 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 100F.
  • RMP-B-12 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1969 September 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B STF-1. FAILURE: Failure.
  • SSTTP 1 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 100 km (60 mi).

1969 September 23 - . 20:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-208.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 October 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2510.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 October 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 98F. FAILURE: Failure. Failed Stage: 1.
  • RMP-B-13 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 10 km (6 mi).

1969 October 15 - . 11:16 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-305.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 October 31 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-304.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 November 6 - . 20:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-209.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 November 19 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2508.
  • ST - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 December 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 44F.
  • ABRES RVTO-1A-6 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1969 December 4 - . 20:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-210. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC.

1969 December 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 93F.
  • RMP-B-14 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1969 December 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B STF-2.
  • SSTTP 2 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 February 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 96F.
  • RMP-B-15 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 March 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 28F.
  • RMP-B-16 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 March 13 - . 20:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-212. FAILURE: Failure.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC.

1970 March 14 - . 18:00 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC31A. Launch Pad: LC31A/Truck. Launch Vehicle: M55E1.
  • Sheltered Base research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1.00 km (0.60 mi).

1970 April 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-309.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 April 3 - . 20:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-213.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 April 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-308.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 April 29 - . 16:02 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-214.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 May 8 - . 07:49 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-310.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 May 27 - . 15:59 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-215.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 May 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 91F.
  • RMP-B-17 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 June 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 92F.
  • ABRES RVTO-1A-7 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 June 17 - . 08:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-312.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 June 24 - . 04:33 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-313.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 July 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-3 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 July 28 - . 23:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 FTM-5008.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 August 28 - . 09:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-4 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 September 16 - . 20:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-1.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 October 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-27 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 November 4 - . 09:05 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-1W.
  • STM-1W research and development mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 December 2 - . 18:02 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-3.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 December 14 - . 15:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC32B. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-2.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1970 December 22 - . 08:38 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 105F.
  • ABRES RVTO-2A-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1970 December 24 - . 01:55 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-12 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 January 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-30 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 February 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-28 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 March 17 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-13 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 April 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 85F.
  • ABRES LAR-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1971 April 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-2W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 June 11 - . 14:55 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-6W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 June 27 - . 03:18 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M1-14 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 June 29 - . 13:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas/Trident F. LV Configuration: Atlas F/Trident 103F.
  • ABRES RVTO-2A-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1971 June 29 - . 13:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg PLC-C. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.116-1.
  • CHASER 1 ABM infrared sensor technology mission - . Nation: USA. Agency: USAF AFSC. Apogee: 161 km (100 mi).

1971 September 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 74F.
  • ABRES LAR-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1971 October 8 - . 01:56 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-2 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 October 20 - . 16:16 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-3W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1971 November 24 - . 06:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg PLC-C. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.116-3.
  • CHASER 2 ABM infrared sensor technology mission - . Nation: USA. Agency: USAF AFSC. Apogee: 145 km (90 mi).

1971 December 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-4W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 March 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-7 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 May 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-11 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 May 31 - . 14:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-1.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 June 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 2.
  • OBL/GIANT PATRIOT 1 test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 June 18 - . 00:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-5W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 June 20 - . 16:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg PLC-C. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 CRL A04.116-3. FAILURE: Failure.
  • CHASER ABM infrared sensor technology mission - . Nation: USA. Agency: USAF AFSC. Apogee: 8.00 km (4.90 mi).

1972 July 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-15 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 July 26 - . 05:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF07. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 Destruct test.
  • OBL/GIANT PATRIOT 2 test - . Nation: USA. Agency: USAF AFSC. Apogee: 21 km (13 mi).

1972 August 2 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-7W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 October 28 - . 03:23 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • HK-1 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 December 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-21 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1972 December 19 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • HK-3 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 March 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES NTV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 April 25 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • HK-2 - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 May 4 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-24 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 May 31 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-4.
  • PVM-4 test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 July 21 - . 00:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-18 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 August 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-20 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 August 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-3.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 August 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 78F.
  • BMRS RVTO-3A-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1973 September 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-44 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 September 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 108F.
  • BMRS ACE-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1973 November 29 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-25 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 December 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • HK-4? Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 December 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-20A Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1973 December 22 - . 08:05 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-8W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 January 23 - . 02:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-28 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 March 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 73F.
  • BMRS SFT-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1974 March 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 97F.
  • BMRS ACE-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1974 April 5 - . 01:25 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-5.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 April 10 - . 20:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Titan. Launch Vehicle: Titan 3D. LV Configuration: Titan IIID 23D-9.
  • S73-7 Cal Balloon - . Nation: USA. Agency: USAF AFSC. Spacecraft: S73-7 Cal Balloon. Decay Date: 1974-07-28 . USAF Sat Cat: 7242 . COSPAR: 1974-020xx. Apogee: 247 km (153 mi). Perigee: 148 km (91 mi). Inclination: 94.4000 deg. Period: 88.50 min.

1974 April 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-135 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 April 27 - . 08:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-35 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 May 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 54F.
  • BMRS SFT-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1974 June 28 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 82F.
  • BMRS SFT-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1974 July 11 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES/SAMAST re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 July 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-146 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 August 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SSTTP M2-46 Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 September 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A1. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 80F.
  • BMRS ACE-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1974 September 8 - . Launch Site: WTR Launch Area. Launch Platform: C-5A. Launch Vehicle: M55E1.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 50 km (31 mi).

1974 October 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF04. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-8.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 October 12 - . 05:54 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-6.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 October 12 - . 08:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF25. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-7.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1974 October 14 - . 04:46 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576A3. LV Family: Atlas. Launch Vehicle: Atlas F. LV Configuration: Atlas F 31F.
  • BMRS RVTO-3A-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,400 km (800 mi).

1974 October 24 - . Launch Site: WTR Launch Area. Launch Platform: C-5A. Launch Vehicle: M55E1.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 6.00 km (3.70 mi).

1974 November 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-9.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 January 19 - . 11:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Trident SFT-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 March 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • Trident SFT-101 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 May 7 - . 04:20 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-10.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 May 9 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-102 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 May 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-9W.
  • PAVE PEPPER test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 May 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES NTV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 July 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-11.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 July 26 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-10W.
  • PAVE PEPPER test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 August 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-103 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 September 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-104 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 September 30 - . 10:02 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-05 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1975 November 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-16 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 January 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-12.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 January 23 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SFT-105 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 February 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ANT-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 March 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-13.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 July 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-11W.
  • STM-11W test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 August 19 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SAMAST III/MINT II re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1976 November 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-12W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 January 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-13W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 May 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TDV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 June 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-14W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 September 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TDV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 November 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-15.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 November 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TDV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1978 January 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-15W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1978 March 25 - . 18:09 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC40. LV Family: Titan. Launch Vehicle: Titan 3C. LV Configuration: Titan IIIC 23C-17. FAILURE: Failure.
  • DSCS II F-10 - . Payload: DSCS II F-10. Nation: USA. Agency: USAF AFSC. Program: DSCS. Spacecraft: DSCS II. COSPAR: F780325B.

1978 April 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TREP-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1978 June 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ANT-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1978 June 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-16W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1978 July 4 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ANT-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1978 November 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ANT-3A re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1978 December 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-17W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 January 19 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES STREP-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 January 24 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ABRV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 February 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-16.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 April 19 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-17.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 July 6 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES LBRV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 August 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES STREP-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 August 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-18W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 September 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ABRV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1979 December 20 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES AMARV-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 January 31 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-18.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 March 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ABRV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 March 27 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 PVM-19.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 April 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES STREP-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 September 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES STREP-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 October 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES AMARV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1980 December 9 - . 07:18 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC3W. LV Family: Atlas. Launch Vehicle: Atlas E/MSD. LV Configuration: Atlas E/MSD 68E. FAILURE: Premature shut down of one of the Atlas booster engines turned the vehicle around, thereafter the sustainer thrust it back toward the earth..
  • LIPS 1 - . Payload: LIPS 1. Nation: USA. Agency: USAF AFSC. Spacecraft: LIPS. COSPAR: F801209E.
  • SSU - . Payload: SSU. Nation: USA. Agency: USAF AFSC. Spacecraft: NOSS. COSPAR: F801209D.
  • SSU - . Payload: SSU. Nation: USA. Agency: USAF AFSC. Spacecraft: NOSS. COSPAR: F801209C.
  • SSU - . Payload: SSU. Nation: USA. Agency: USAF AFSC. Spacecraft: NOSS. COSPAR: F801209B.

1980 December 16 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES ABRV-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 February 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES IRS-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 March 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES TDV-4 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 April 4 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES Mk500-PAS-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 September 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES Mk500-PAS-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1981 October 4 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • ABRES AMARV-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1982 October 8 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-21 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 January 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP LBRV-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 February 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-11 (HOE) re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 February 7 - . Launch Site: Kwajalein. Launch Vehicle: HOE. LV Configuration: HOE HOE 1.
  • HOE 1 ABM test - . Nation: USA. Agency: USAF AFSC. Apogee: 200 km (120 mi).

1983 May 5 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-22 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 May 28 - . Launch Site: Kwajalein. Launch Vehicle: HOE. LV Configuration: HOE HOE 2.
  • HOE 2 ABM test - . Nation: USA. Agency: USAF AFSC. Apogee: 200 km (120 mi).

1983 May 28 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-12 (HOE) Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 June 18 - . 02:10 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-1.
  • 6 RVs to BOA-KMR - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1983 October 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-2.
  • 6 RVs to BOA-KMR - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1983 December 15 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-12A (HOE) Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1983 December 15 - . Launch Site: Kwajalein. Launch Vehicle: HOE. LV Configuration: HOE HOE 3.
  • HOE 3 ABM test - . Nation: USA. Agency: USAF AFSC. Apogee: 200 km (120 mi).

1983 December 20 - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-3.
  • 8 RVs to BOA-Guam - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1984 March 30 - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-4.
  • 10 RVs sent to KMR impact area. - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1984 June 10 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP STREP-13 (HOE) Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1984 June 10 - . Launch Site: Kwajalein. Launch Vehicle: HOE. LV Configuration: HOE HOE 4.
  • HOE 4 ABM test - . Nation: USA. Agency: USAF AFSC. Apogee: 200 km (120 mi).

1984 June 15 - . 16:50 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-5.
  • 6 RVs to KMR(1 Mk21) - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1984 October 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-6.
  • RVs to KMR - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1984 October 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP IPA-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1985 February 1 - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-7.
  • 6 RVs Test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1985 May 22 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP IPA-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1985 June 3 - . Launch Site: Vandenberg. Launch Complex: Vandenberg TP-01. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-8.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1985 August 24 - . 16:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-9.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1985 November 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-10.
  • 4 RVs Test - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1986 March 7 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-11.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1986 March 17 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP IPA-3 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1986 April 18 - . 17:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC4E. LV Family: Titan. Launch Vehicle: Titan 34D. LV Configuration: Titan 34D 34D-9 (04D-2). FAILURE: Failure.
  • SRV-3 - . Payload: SRV-3. Mass: 11,400 kg (25,100 lb). Nation: USA. Agency: USAF AFSC. Spacecraft: KH-9. COSPAR: F860418D.
  • SRV-1 - . Payload: SRV-1. Mass: 11,400 kg (25,100 lb). Nation: USA. Agency: USAF AFSC. Spacecraft: KH-9. COSPAR: F860418F.
  • SRV-4 - . Payload: SRV-4. Mass: 11,400 kg (25,100 lb). Nation: USA. Agency: USAF AFSC. Spacecraft: KH-9. COSPAR: F860418E.
  • SRV-2 - . Payload: SRV-2. Mass: 11,400 kg (25,100 lb). Nation: USA. Agency: USAF AFSC. Spacecraft: KH-9. COSPAR: F860418C.

1986 May 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-12.
  • 10 Mk 21 warheads sent to KMR impact area. - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1986 August 23 - . 18:25 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-15.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1986 September 18 - . 12:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-13.
  • 6 RVs to KMR - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1986 December 5 - . 16:00 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF02. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-14.
  • 10 RV (2 ft deploy) - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1987 January 20 - . 08:35 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. FAILURE: Failure.
  • SENT-1 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 90 km (55 mi).

1987 February 13 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-16.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1987 March 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-17.
  • Test mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1987 April 2 - . 08:05 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • IPMS - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1987 September 1 - . 07:58 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF06. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • IPMS - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1987 September 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • SENT-2 re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1988 January 18 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP TDMaRV re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1989 March 19 - . 17:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF08. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper FTM-18.
  • 7 Mk 21 RVs to KMR - . Nation: USA. Agency: USAF AFSC. Apogee: 1,000 km (600 mi).

1990 February 14 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP MAST re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1990 June 8 - . 05:22 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC41. LV Family: Titan. Launch Vehicle: Titan 405A. LV Configuration: Titan 405A K-4 (45H-4).
1991 January 28 - . 18:03 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • GBI-1 ERIS Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1991 May 11 - . 20:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • GBI-2 ERIS Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi). This was intended to be the second ERIS intercept flight, but there was either an ERIS launcher problem or a range safety problem that aborted the attempt after the target vehicle was on its way towards Kwajalein.It took just over one year to recover from that abort and to perform the intercept attempt against target vehicle "2B".

1991 June 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • RSLP AST re-entry vehicle test flight - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1992 March 13 - . 18:15 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B.
  • GBI-2B ERIS Target mission - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

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