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1947 -

  • XS-1 Flight 18 Nation: USA. Payload: XS-1 # 2 flight 8. Class: Manned. Type: Rocketplane. Spacecraft: XS-1. Crew: Goodlin.

    Bell flight 8. Buffet boundary investigation. Full-power climb. Plane reached mach 0.82.

1955 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -.
  • Rocket-towed model. Nation: USA.

    First launching of a test model towed by a rocket vehicle with a flexible towline, by Langley Laboratory's PARD at Wallops Island, Va.

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.
  • X-15A MH-96. Mach 5 test Nation: USA. Agency: NASA/USAF. Apogee: 40 km (24 mi).

    Maximum Speed - 6058 kph. Maximum Altitude - 40690 m.

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.
  • X-15A VO Alt, IR expt Test/Technology mission Nation: USA. Agency: NASA/USAF. Apogee: 82 km (50 mi).

    First civilian flight above 80 km. Maximum Speed - 5917 kph. Maximum Altitude - 82810 m. Second astronaut wings flight (USAF definition).

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.
  • FU-145B astronomy Test / ultraviolet astronomy mission Nation: France. Agency: FR. Apogee: 205 km (127 mi).

    FU145b X-ray and UV astronomy / Stab mission.

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.
  • Final launch of a Thrust-Augmented-Thor/Agena Nation: USA.

    Final launch of a Thrust-Augmented-Thor/Agena space booster from Vandenberg (first launch on 28 February 1963).

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.
  • Cosmos 628 Nation: USSR. Mass: 550 kg (1,210 lb). Class: Navigation. Spacecraft: Tsiklon. Agency: MO SSSR. Perigee: 952 km (591 mi). Apogee: 1,008 km (626 mi). Inclination: 83.00 deg. Period: 104.70 min. COSPAR: 1974-001A. USAF Sat Cat: 7094.

    Military navigation satellite.

1975 - 09:07 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Voskhod 11A57.
  • Cosmos 702 Nation: USSR. Mass: 6,000 kg (13,200 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2M. Agency: MOM. Perigee: 205 km (127 mi). Apogee: 313 km (194 mi). Inclination: 71.30 deg. Period: 89.70 min. COSPAR: 1975-002A. USAF Sat Cat: 7606. Duration: 12.00 days. Decay Date: 1975-01-29.

    Area survey photo reconnaissance satellite; returned film capsule.

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.
  • CTS 1 Nation: Canada. Payload: Hermes. Mass: 500 kg (1,100 lb). Class: Communications. Spacecraft: CTS. Agency: CRC. Perigee: 35,704 km (22,185 mi). Apogee: 35,840 km (22,260 mi). Inclination: 12.80 deg. Period: 1,435.40 min. COSPAR: 1976-004A. USAF Sat Cat: 8585. Completed Operations Date: 1979-12-08.

    Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Americas at 116 deg W in 1976-79; over the Pacific Ocean 142 deg W in 1979 As of 5 September 2001 located at 135.36 deg W drifting at 0.161 deg W per day. As of 2007 Mar 10 located at 131.55W drifting at 0.190W degrees per day.

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.
  • Cosmos 985 Nation: USSR. Mass: 810 kg (1,780 lb). Class: Navigation. Spacecraft: Parus. Agency: MO SSSR. Perigee: 938 km (582 mi). Apogee: 1,015 km (630 mi). Inclination: 82.90 deg. Period: 104.60 min. COSPAR: 1978-007A. USAF Sat Cat: 10599.

    Military navigation satellite.

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.
  • Shuttle MPTA-098 625-second firing. Nation: USA.

    This firing used the three flight engines, which had been removed from Columbia.

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.
  • Raduga 18 Nation: USSR. Payload: Raduga s/n 29L. Mass: 1,940 kg (4,270 lb). Class: Communications. Type: Military. Spacecraft: Raduga . Agency: MOM. Perigee: 35,909 km (22,312 mi). Apogee: 36,493 km (22,675 mi). Inclination: 5.80 deg. Period: 1,457.30 min. COSPAR: 1986-007A. USAF Sat Cat: 16497. Completed Operations Date: 1991-12-04.

    Stationed at 335 deg. E. Provision of telephone and telegraph radiocommunications and television broadcasting. Positioned in geosynchronous orbit at 25 deg W in 1986-1989; 170 deg W in 1989-1991 As of 28 August 2001 located at 163.25 deg W drifting at 5.255 deg W per day. As of 2007 Mar 10 located at 22.49E drifting at 5.257W degrees per day.

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.
  • Cosmos 2055 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Earth. Type: Landsat. Spacecraft: Zenit-8. Agency: MOM. Perigee: 248 km (154 mi). Apogee: 260 km (160 mi). Inclination: 62.80 deg. Period: 89.60 min. COSPAR: 1990-003A. USAF Sat Cat: 20426. Duration: 12.00 days. Decay Date: 1990-01-29.

    Military cartographic satellite; returned film capsule.

1991 - 10:30 GMT - Launch Site: Plesetsk. Launch Complex: LC16/2. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 2121 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Earth. Type: Landsat. Spacecraft: Zenit-8. Agency: MOM. Perigee: 165 km (102 mi). Apogee: 247 km (153 mi). Inclination: 82.60 deg. Period: 88.60 min. COSPAR: 1991-004A. USAF Sat Cat: 21059. Duration: 24.00 days. Decay Date: 1991-02-10.

    Military cartographic satellite; returned film capsule.

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 -
  • EVA STS-54-1 Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Endeavour. Crew: Harbaugh, Runco. Flight: STS-54. EVA Duration: 0.18 days.

    Tested tools and techniques for extravehicular activity.

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.
  • IFT-1 EKV Target Target mission Nation: USA. Agency: USAF AFMC. Apogee: 1,300 km (800 mi).

    Minuteman launched an MSLS target vehicle for the EKV anti-ballistic missile interceptor launched from Kwajalein Atoll.

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.
  • GPS 42 Nation: USA. Program: Navstar. Payload: GPS 2R-1 / GPS SVN 42. Mass: 2,030 kg (4,470 lb). Class: Navigation. Spacecraft: GPS Block 2R. Manufacturer: Lockheed Martin, Valley Forge. Agency: MDSSC. COSPAR: F970117A.

    Destroyed in launch vehicle 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:

Died on this day in:
  • 2008 - Werner Karl Dahm.  German Rocket engineer.

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