See also Born on this Day On this day in: 1947 -
1955 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -.
1958 - Launch Site: Cape Canaveral. Launch Complex: LC3. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris TV. LV Configuration: Polaris TV 1-204-10. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1961 - 21:25 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.36GT. -
Test mission Nation: USA. Agency: NASA. Apogee: 209 km (129 mi).
1962 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).
1962 - 20:00 GMT - Launch Site: Mud Lake DZ. Launch Complex: -. Launch Pad: 37.9 N x 117.1 W. Launch Vehicle: X-15. LV Configuration: X-15 3-2-3.
1962 - 21:02 GMT - Launch Site: Vandenberg. Launch Complex: 576B2. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 123D. -
Operational missile test Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).
1963 - -
Department of Defense (DOD) and NASA management responsibilities in the Cape Canaveral area. Nation: USA. NASA Administrator James E. Webb and Secretary of Defense Robert S. McNamara signed a new agreement on Department of Defense (DOD) and NASA management responsibilities in the Cape Canaveral area. The Air Force would continue as single manager of the Atlantic Missile Range and host agency at the 15,000-acre Cape Canaveral launch area. NASA's Launch Operations Center would manage and serve as host agency at the Merritt Island Launch Area, north and west of existing DOD installations. DOD and NASA would each be responsible for their own logistics and administration in their respective areas. Specific mission functions - e.g., preparation, checkout, launch, test evaluation - would be performed by each agency in its own behalf, regardless of location. DOD retained certain fundamental range functions, including scheduling, flight safety, search and rescue operations, and downrange airlift and station operation.
1963 - -
Mercury MA-10 a possibility. Nation: USA. Program: Mercury. Spacecraft: Mercury. Flight: Mercury MA-9. Asked by a Congressional committee if NASA planned another Mercury flight after MA-9, Dr Robert C. Seamans stated, in effect, that schedules for the original Mercury program and the 1-day orbital effort were presumed to be completed in fiscal year 1963. If sufficient test data were not accumulated in the MA-9 flight, backup launch vehicles and spacecraft were available to fulfill requirements.
1963 - 18:59 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 3-14-24.
1964 - 05:01 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.31DA. -
Composition / Airglow Aeronomy mission Nation: USA. Agency: NASA. Apogee: 925 km (574 mi).
1966 - 16:42 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P-393. -
Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1966 - 17:56 GMT - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C127. -
Ionosphere mission Nation: France. Agency: CNES. Apogee: 124 km (77 mi).
1966 - 22:39 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.262CM. -
Sodium release Aeronomy mission Nation: USA. Agency: NASA. Apogee: 206 km (128 mi).
1967 -
1967 - Launch Site: Hammaguira. Launch Complex: Blandine. Launch Pad: -. Launch Vehicle: Veronique. Model: Veronique 61. LV Configuration: Veronique 61 VA85.
1967 - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sandhawk. LV Configuration: Sandhawk Sandia 281-3. -
Test / aeronomy mission Nation: USA. Agency: Sandia. Apogee: 188 km (116 mi).
1967 - 19:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AG3.526. -
Extreme ultraviolet Mon Solar extreme ultraviolet mission Nation: USA. Agency: AFCRL. Apogee: 243 km (150 mi).
1968 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena D.
1968 - -
Afanasyev inspects the TsPK. Nation: USSR. Program: Lunar L1, Lunar L3. Spacecraft: Soyuz 7K-L1, Soyuz 7K-LOK. He is shown the Volga and L1 trainers, takes a seat in the trainer, and is given a simulated space flight. At the air base he reviews the aircraft and the TBK-60 altitude chamber. Throughout the tour, Mishin constantly wore a soft expression and used coarse language. Afanasyev was briefed on and recognised problems with development and delivery of the Salyut digital computer needed for the L1 guidance system. But he was not told that cooperation had broken down totally on the L3 simulator development and crew selection.
1968 - 10:12 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 498 / Agena D 2733. -
OPS 1965 Nation: USA. Payload: Ferret 12 / Agena D 2733. Mass: 1,500 kg (3,300 lb). Class: Sigint. Spacecraft: Ferret. Agency: NRO/USAF. Perigee: 462 km (287 mi). Apogee: 536 km (333 mi). Inclination: 75.10 deg. Period: 94.60 min. COSPAR: 1968-004A. USAF Sat Cat: 3097. Decay Date: 1970-07-07.
1968 - 23:08 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.634. -
Atmospheric / TMA Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 193 km (119 mi).
1969 - 18:34 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.313IM. -
RTG SNC 2A / 1 Aeronomy mission Nation: Sweden. Agency: NASA/RTG. Apogee: 117 km (72 mi).
1969 - 21:32 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.306GM. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 112 km (69 mi).
1969 - -
Landing of Soyuz 4 Nation: USSR. Program: Soyuz. Flight: Soyuz 4, Soyuz 4/5. Soyuz 4 landed at 06:51 GMT 48 km south-west of Karaganda, 40 km from the planned point, with the crew of Khrunov, Shatalov and Yeliseyev aboard. Shatalov's performance has been outstanding -- all manoeuvres were made correctly with minimal expenditure of propellant. The soft landing system performed well, in temperatures of -30 deg C and in 60 to 80 cm of snow. The first recovery helicopter reached the capsule only five minutes after touchdown. 25 minutes later the crew is on a helicopter, on their way to the airfield at Karaganda. The crew is given a medical examination at the Hotel Chaika and then taken downstairs for a press conference. At 16:45 they board an An-24, bound for Tyuratam.
1970 - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67M. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1970 - 01:20 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210-3. -
X-ray astronomy mission Nation: Japan. Agency: ISAS. Apogee: 119 km (73 mi).
1970 - 03:03 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.65UE. -
Aurora mission Nation: USA. Agency: NASA. Apogee: 252 km (156 mi).
1971 - 14:48 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C37/2. -
ESRO C37 / 2 MPE Ba Ionosphere / barium release mission Nation: Europe. Agency: ESRO. Apogee: 215 km (133 mi).
1971 - 15:33 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk DLR A-NT-39. -
MPE Barium release / Brigitte Ionosphere / fields mission Nation: Germany. Agency: DLR. Apogee: 328 km (203 mi).
1974 - -
Kamanin sees Comet Kohoutek. Nation: USSR.
1974 - 02:37 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.160GE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 298 km (185 mi).
1974 - 10:07 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53753-208.
1975 - 09:07 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
1975 - 09:35 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 9M. LV Configuration: Kappa 9M K-9M-49. -
Airglow Aeronomy / ionosphere mission Nation: Japan. Agency: ISAS. Apogee: 363 km (225 mi).
1975 - 22:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Ute Tomahawk. LV Configuration: Ute Tomahawk CRL A09.301-9. -
Aladdin 75 Sphere Aeronomy / plasma mission Nation: USA. Agency: USAF CRL. Apogee: 190 km (110 mi).
1976 - 23:27 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2914. LV Configuration: Delta 2914 606/D119.
1978 - 03:26 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53716-327.
1978 - 20:21 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25C. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4. LV Configuration: Trident C-4 C4X-13. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1979 - 20:00 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Astrobee. Model: Astrobee F. LV Configuration: Astrobee F NASA 25.10AS. -
Solar mission Nation: USA. Agency: NASA. Apogee: 226 km (140 mi).
1981 - Launch Vehicle: Shuttle.
1982 - 14:11 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4. -
DASO-9 demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1984 - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: K?. Launch Vehicle: SB-735. Model: ST-735. LV Configuration: ST-735-1 ST-735-1. -
SRB Sep test Nation: Japan. Agency: ISAS. Apogee: 50 km (31 mi).
1984 - 20:00 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A MAP/WINE. -
M-F 26 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 116 km (72 mi).
1985 - 15:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: LC35 L-21B. Launch Vehicle: Aerobee. Model: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.342UG. -
JHU Airglow 14 (HUT) Airglow mission Nation: USA. Agency: NASA. Apogee: 169 km (105 mi).
1985 - 17:46 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65034-138. -
Cosmos 1624 Nation: USSR. Program: Strela. Mass: 700 kg (1,540 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-2M. Agency: MO SSSR. Perigee: 777 km (482 mi). Apogee: 797 km (495 mi). Inclination: 74.00 deg. Period: 100.60 min. COSPAR: 1985-006A. USAF Sat Cat: 15482. Replaced Cosmos 1570.
1986 - 07:21 GMT - Launch Site: Plesetsk. Launch Complex: LC32. Launch Pad: LC32/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-3. -
Cosmos 1726 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 53. Mass: 2,000 kg (4,400 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MO SSSR. Perigee: 590 km (360 mi). Apogee: 618 km (384 mi). Inclination: 82.50 deg. Period: 96.80 min. COSPAR: 1986-006A. USAF Sat Cat: 16495.
1986 - 10:20 GMT - Launch Site: Baikonur. Launch Complex: LC200/40. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM. LV Configuration: Proton-K/DM 331-02.
1989 - 19:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.47GU. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).
1990 - -
NASA Astronaut Training Group 13 selected. Nation: USA. The group was selected to provide pilot, engineer, and scientist astronauts for space shuttle flights.. Qualifications: Pilots: Bachelor's degree in engineering, biological science, physical science or mathematics. Advanced degree desirable. At least 1,000 flight-hours of pilot-in-command time. Flight test experience desirable. Excellent health. Vision minimum 20/50 uncorrected, correctable to 20/20 vision; maximum sitting blood pressure 140/90. Height between 163 and 193 cm.
Mission Specialists: Bachelor's degree in engineering, biological science, physical science or mathematics and minimum three years of related experience or an advanced degree. Vision minimum 20/150 uncorrected, correctable to 20/20. Maximum sitting blood pressure of 140/90. Height between 150 and 193 cm.. Reported to the Johnson Space Center in late July 1990 to begin their year long training. Chosen from 1945 qualified applicants, then 106 finalists screened between September and November 1989.
1990 - 14:45 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1991 - 10:30 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1992 - Launch Site: White Sands. Launch Complex: SULF. Launch Pad: -. Launch Vehicle: Storm. LV Configuration: Storm S1. -
BTTV-1 Validation test Nation: USA. Agency: USA. Apogee: 200 km (120 mi).
1993 -
1996 - 05:40 GMT -
1997 - 01:17 GMT - Launch Site: Vandenberg. Launch Complex: LF03. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 MSLS IFT-1.
1997 - 16:28 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925 D241. FAILURE: T+12 sec GEM strap-on number 2 structural failure.
2001 - 04:31 GMT - Launch Site: Balasore. Launch Complex: IC4. Launch Pad: -. Launch Vehicle: Agni. Model: Agni 2. -
Agni RV Mk 2 Research and development launch Nation: India. Agency: IDRDL. Apogee: 1,000 km (600 mi).
2002 - -
Galileo, Io 33 Flyby Nation: USA. Spacecraft: Galileo.
2003 - 13:00 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. -
SAGE-3 3 Aeronomy mission Nation: Germany. Agency: NASA. Apogee: 112 km (69 mi).
2004 - 15:30 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: K. Launch Vehicle: S. Model: S-310. LV Configuration: S-310-33. -
WAVE2004 Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 141 km (87 mi).
Born on this day in:
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