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1933 - Launch Vehicle: Magdeburg.

  • Nebel rocket Nation: Germany. Apogee: 0.0020 km (0.0012 mi).

    Second attempt from Schwielow Lake. The rocket goes horizontal and hits the water in the lake's steamboat channel. It cannot be recovered.

1933 - Launch Vehicle: GIRD-09. FAILURE: Failure.
  • GIRD-09 launch attempt. Nation: USSR.

    Launch failure.

1950 -
  • XS-1 Flight 140 Nation: USA. Payload: XS-1 # 2 flight 59. Class: Manned. Type: Rocketplane. Spacecraft: XS-1. Crew: Griffith.

    NACA flight 39. For pressure distribution and stability and control data. Check of stabilizer effectiveness.

1957 - 05:16 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 70.4 N x 57.0 W. Launch Vehicle: Rockoon. Model: Loki Rockoon. LV Configuration: Loki Rockoon II5.10F. FAILURE: Failure.
  • SUI 65 Aeronomy / Chemical release mission Nation: USA. Agency: SUI. Apogee: 0 km ( mi).

    Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP10 - - Latitude: 70.40 N - Longitude: 57.00 W.

1957 - 20:30 GMT - Launch Site: Atlantic Ocean. Launch Complex: -. Launch Pad: 66.7 N x 54.9 W. Launch Vehicle: Rockoon. Model: Loki Rockoon. LV Configuration: Loki Rockoon II5.11F.
  • SUI 66 Aeronomy / Chemical release mission Nation: USA. Agency: SUI. Apogee: 100 km (60 mi).

    Launched at IGY Rockoon Launch Site 1, Atlantic Ocean LP11 - - Latitude: 66.67 N - Longitude: 54.93 W.

1959 - 18:01 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas D. LV Configuration: Atlas D 14D.
  • Research and development launch Nation: USA. Agency: USAF. Apogee: 1,800 km (1,100 mi).

1961 - 14:30 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Exos. LV Configuration: Exos CRL AA13.194.
  • Ion density Test / ionosphere mission Nation: USA. Agency: USAF. Apogee: 114 km (70 mi).

1962 -
  • Eight companies to bid on Apollo lunar excursion module Nation: USA. Program: Apollo. Spacecraft: Apollo LM.

    Of the 11 companies invited to bid on the lunar excursion module on July 25, eight planned to respond. NAA had notified MSC that it would not bid on the contract. No information had been received from the McDonnell Aircraft Corporation and it was questionable whether the Northrop Corporation would respond.

1962 -
  • NASA schedule for Apollo command and service modules Nation: USA. Program: Apollo. Spacecraft: Apollo CSM.

    A NASA program schedule for the Apollo spacecraft command and service modules through calendar year 1965 was established for financial planning purposes and distributed to the NASA Office of Manned Space Flight, Marshall Space Flight Center, and MSC. The key dates were: complete service module drawing release, May 1, 1963; complete command module drawing release, June 15, 1963; manufacture complete on the first spacecraft, February 1, 1964; first manned orbital flight, May 15, 1965. This tentative schedule depended on budget appropriations.

1962 - 01:48 GMT - Launch Site: Kronogard. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun K-62-3.
  • Air sample Aeronomy mission Nation: Sweden. Agency: RTG/AFCRL. Apogee: 105 km (65 mi).

1962 - 08:30 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K.
  • Vostok 3 Nation: USSR. Program: Vostok. Payload: Vostok 3KA s/n 5. Mass: 4,722 kg (10,410 lb). Class: Manned. Type: Spacecraft. Spacecraft: Vostok. Agency: RVSN. Perigee: 166 km (103 mi). Apogee: 218 km (135 mi). Inclination: 65.00 deg. Period: 88.30 min. COSPAR: 1962-A-Mu-1. USAF Sat Cat: 363. Duration: 3.93 days. Decay Date: 1962-08-15. Crew: Nikolayev. Flight: Vostok 3.

    Joint flight with Vostok 4. The first such flight, where Vostok capsules were launched one day apart, coming within a few kilometers of each other at the orbital insertion of the second spacecraft. The flight was supposed to occur in March, but following various delays, one of the two Vostok pads was damaged in the explosion of the booster of the third Zenit-2 reconnsat in May. Repairs were not completed until August. Vostok 3 studied man's ability to function under conditions of weightlessness; conducted scientific observations; furthered improvement of space ship systems, communications, guidance and landing. Immediately at orbital insertion of Vostok 4, the spacecraft were less than 5 km apart. Popovich made radio contact with Cosmonaut Nikolayev. Nikolayev reported shortly thereafter that he had sighted Vostok 4. Since the Vostok had no maneuvering capability, they could not rendezvous or dock, and quickly drifted apart. The launches did allow Korolev to offer something new and different, and gave the launch and ground control crews practice in launching and handling more than one manned spacecraft at a time. The cosmonaut took colour motion pictures of the earth and the cabin interior. - Additional details.

1963 -
  • Kamanin picks up a new Volga automobile. Nation: USSR. Flight: Vostok 6, Vostok 7, Vostok 8, Vostok 9, Vostok 10.

    Kamanin picks up a new Volga automobile. It cost him 5513 roubles, but one door doesn't fit and the trunk is scarred with excess hardened resin. Sukarno has asked for Tereshkova and Bykovskiy to visit Indonesia for two weeks in August, but this is impossible.

    In a three hour meeting Korolev goes over his future flight plans for Vostok. The first flight will be unmanned, with a biological payload, in February or March 1964. The flight is to last 10 or 11 days and take the specimens up to 600 to 1000 km altitude, into the lower reaches of the Van Allen radiation belts. This will be followed by three cosmonaut flights of ten days with significant military and scientific experiments. A new ground control system will be installed and tested to handle all in-flight emergencies. A new autonomous on-board navigation system will be flight tested. Korolev wants the military to take over conduct of future Vostok flights - they are taking up to much of his time and nerves. He has told this repeated to Khrushchev and Brezhnev without result. Meanwhile Kamanin lobbies within the military hierarchy for the removal of Odintsev. It is decided that the matter will be taken up at the next meeting of the Military Soviet.

1964 - Launch Site: Vandenberg. Launch Complex: 395-C. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 2. LV Configuration: Titan II B-9.
  • Double Talley Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

    Demonstration and shakedown operations launch

1964 - 02:00 GMT - Launch Site: Baikonur. Launch Complex: LC67/22. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. FAILURE: Failure.
  • State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1964 - 05:10 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 7C. LV Configuration: Skylark-7C SL301.
  • LUX Solar AC1 Solar x-ray and ultraviolet mission Nation: Australia. Agency: WRE/RAE. Apogee: 145 km (90 mi).

1964 - 10:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.82GG.
  • Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 172 km (106 mi).

1965 - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1 C2X-3.
  • STAFF 3 test Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1965 - 01:35 GMT - Launch Site: Pameungpeuk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8. LV Configuration: Kappa 8 K-8(L)-4.
  • SK-8-4 Aeronomy / ionosphere / Fields mission Nation: Japan. Agency: ISAS. Apogee: 191 km (118 mi).

1965 - 11:49 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.144GM.
  • Meteoroids Aeronomy / meteorites mission Nation: USA. Agency: NASA. Apogee: 129 km (80 mi).

1965 - 14:31 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36B. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Centaur D. LV Configuration: Atlas Centaur D AC-6 / Centaur D 151D.
  • Surveyor; Atlas Centaur 6 Nation: USA. Payload: Surveyor-SD-2. Mass: 950 kg (2,090 lb). Class: Planetary. Type: Lunar. Spacecraft: Surveyor. Agency: NASA/JPL. COSPAR: 1965-064A. USAF Sat Cat: 1503.

    Centaur AC-6 launched dummy Surveyor payload into a barycentric / translunar orbit.

1966 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-86.
  • ACS technology mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi).

1966 - 12:05 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: Kappa. Model: Kappa 8L. LV Configuration: Kappa 8L K-8L-10.
  • Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 130 km (80 mi).

1966 - 15:53 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 CRL AC3.364.
  • Auroral emissions Aurora mission Nation: USA. Agency: AFCRL. Apogee: 207 km (128 mi).

1966 - 17:44 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 1-66-111.
  • X-15A HS,MuMet,SB,Gas Technology/Meteor/Aeronomy mission Nation: USA. Agency: NASA/USAF. Apogee: 76 km (47 mi).

    Maximum Speed - 5776 kph. Maximum Altitude - 76500 m. Record dynamic pressure.

1967 - 09:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.223NA.
  • LUSTER II 1967 Meteorites mission Nation: USA. Agency: NASA. Apogee: 141 km (87 mi).

1967 - 20:25 GMT - Launch Site: Indian Ocean. Launch Complex: -. Launch Pad: 20.0 S x 65.0 E. Launch Vehicle: M-100. Model: M-100.
  • Ionosphere mission Nation: USSR. Agency: AN SSSR. Apogee: 90 km (55 mi).

1969 - 01:30 GMT - Launch Site: Kiruna. Launch Complex: C. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C51/1.
  • ESRO C51 / 1 Aeronomy mission Nation: Europe. Agency: ESRO. Apogee: 112 km (69 mi).

1969 - 15:30 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3E.
  • Operational test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1970 -
  • X-24 Flight 16 Nation: USA. Payload: X-24A flight 16. Class: Manned. Type: Spaceplane. Spacecraft: X-24A. Crew: Manke.

    Maximum Speed - 1047 kph. Maximum Altitude - 19477 m. Flight Time - 413 sec.

1970 - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 2.
  • OT GT06F operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1972 -
  • M2 Flight 31 Nation: USA. Program: NASA Lifting Body. Payload: M2-F3 flight 15. Class: Manned. Type: Spaceplane. Spacecraft: M2-F3. Crew: Dana.

    Maximum Speed - 1168 kph. Maximum Altitude - 20480 m. Flight Time - 375 sec.

1972 -
  • Soyuz 7K-S designs completed Nation: USSR. Spacecraft: Soyuz 7K-S, Soyuz OB-VI.

    The Soyuz 7K-S had two parallel designs - the base variant, which was for special-purpose military solo missions; and a space station transport variant 7K-ST. The Soyuz 7K-S program was to consist of four unmanned, followed by two manned test flights, then two operational launches.

1972 - 01:01 GMT - Launch Site: Syowa Base. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-210. LV Configuration: S-210JA-8.
  • Ionosphere / fields mission Nation: Japan. Agency: NIPR. Apogee: 127 km (78 mi).

1976 - 19:12 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Malemute. LV Configuration: Terrier Malemute NASA 12.36GT.
  • Test mission Nation: USA. Agency: NASA. Apogee: 612 km (380 mi).

1978 -
  • Complete forward RCS, Columbia (OV-102) Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Columbia.

1978 -
  • Complete test preparation, STA-099 Nation: USA. Program: STS.

1978 -
  • Complete forward RCS thermal test Nation: USA. Program: STS.

1978 - Launch Site: Baikonur. Launch Complex: LC173. Launch Pad: -. Launch Vehicle: MR-UR-100. Model: MR-UR-100.
  • Combat training launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1978 - 02:20 GMT - Launch Site: Cape Canaveral. Launch Complex: LC25C. Launch Pad: -. Launch Vehicle: Trident. Model: Trident C-4. LV Configuration: Trident C-4 C4X-18.
  • Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1979 -
  • Ferry flight, Atlanta to St. Louis Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise.

    Ferry flight, shuttle carrier aircraft/Enterprise (OV-101), Atlanta to St. Louis (1 hour, 50 minutes)

1979 - 09:15 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
  • Cosmos 1120 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4MKM. Agency: MOM. Perigee: 170 km (100 mi). Apogee: 362 km (224 mi). Inclination: 70.60 deg. Period: 89.80 min. COSPAR: 1979-073A. USAF Sat Cat: 11485. Duration: 13.00 days. Decay Date: 1979-08-24.

    High resolution photo reconnaissance satellite; returned film capsule; maneuverable.

1982 - 00:35 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: Taurus Orion. LV Configuration: Taurus Orion NASA 33.29UL.
  • Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1982 - 23:30 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P214K.
  • CAMP Aeronomy mission Nation: UK. Agency: SRC. Apogee: 129 km (80 mi).

1990 - 08:10 GMT - Launch Site: Kwajalein. Launch Complex: RN. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Taurus Nike Tomahawk. LV Configuration: Taurus Nike Tomahawk NASA 38.17UE.
  • CRRES AA-5 Plasma mission Nation: USA. Agency: NASA. Apogee: 375 km (233 mi).

1991 -
  • Landing of STS-43 Nation: USA. Program: STS. Flight: STS-43.

    STS-43 landed at 12:28 GMT.

1994 - 15:27 GMT - Launch Site: Baikonur. Launch Complex: LC81/23. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 367-02.
  • Cosmos 2287 Nation: Russia. Payload: Glonass s/n 67L. Mass: 1,400 kg (3,000 lb). Class: Navigation. Spacecraft: Glonass . Agency: MOM. Perigee: 19,118 km (11,879 mi). Apogee: 19,142 km (11,894 mi). Inclination: 64.90 deg. Period: 675.70 min. COSPAR: 1994-050A. USAF Sat Cat: 23203.

    Glonass navigation satellite.

  • Cosmos 2288 Nation: Russia. Payload: Glonass s/n 70L. Mass: 1,400 kg (3,000 lb). Class: Navigation. Spacecraft: Glonass. Agency: MOM. Perigee: 19,091 km (11,862 mi). Apogee: 19,168 km (11,910 mi). Inclination: 64.81 deg. Period: 675.73 min. COSPAR: 1994-050B. USAF Sat Cat: 23204.

    Glonass navigation satellite.

  • Cosmos 2289 Nation: Russia. Payload: Glonass s/n 75L. Mass: 1,400 kg (3,000 lb). Class: Navigation. Spacecraft: Glonass. Agency: MOM. Perigee: 19,126 km (11,884 mi). Apogee: 19,133 km (11,888 mi). Inclination: 64.81 deg. Period: 675.73 min. COSPAR: 1994-050C. USAF Sat Cat: 23205.

    Glonass navigation satellite.

1997 - 13:38 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki Falling Sphere.
  • CRISTA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 107 km (66 mi).

1997 - 13:43 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Viper. Model: Viper 3A. LV Configuration: Viper 3A Falling Sphere.
  • CRISTA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 119 km (73 mi).

1997 - 18:18 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.164US.
  • USC-2 SOHO Cal Solar extreme ultraviolet mission Nation: USA. Agency: NASA GSFC. Apogee: 307 km (190 mi).

1997 - 21:34 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki Falling Sphere.
  • CRISTA Aeronomy mission Nation: USA. Agency: NASA. Apogee: 106 km (65 mi).

2003 -
  • Galileo Enters Solar Conjunction Nation: USA. Spacecraft: Galileo.

2004 - Launch Site: Sriharikota. Launch Complex: -. Launch Pad: -. Launch Vehicle: Shahab. Model: Shahab 3.
  • Nation: Iran. Agency: Iran. Apogee: 150 km (90 mi).

    Missile demonstration flight. Stretched Shahab-3 launched into Dasht-E-Kavir desert.

2004 - 05:01 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz-U. LV Configuration: Soyuz-U D15000-685.
  • Progress M-50 Nation: Russia. Program: ISS. Payload: Progress M s/n 250. Mass: 7,250 kg (15,980 lb). Class: Manned. Type: Logistics. Spacecraft: Progress M. Manufacturer: RKK Energia. Agency: RKA. Perigee: 358 km (222 mi). Apogee: 365 km (226 mi). Inclination: 51.60 deg. Period: 91.80 min. COSPAR: 2004-032A. USAF Sat Cat: 28399. Duration: 133.73 days. Decay Date: 2004-12-23. Flight: ISS EO-9.

    Delayed from July 22 and 28. Docked with the International Space Station at 05:01 GMT on August 14. Undocked from the Zvezda module of the ISS on December 22 at 19:34 GMT and was deorbited over the Pacific at 22:32 GMT.

2004 - 10:25 GMT - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100N. Model: UR-100NU.
  • Operational missile test Nation: Russia. Agency: RVSN RF. Apogee: 1,000 km (600 mi).

2005 - 08:20 GMT - Launch Site: Kourou. Launch Complex: ELA3. Launch Pad: -. Launch Vehicle: Ariane 5. Model: Ariane 5GS. LV Configuration: Ariane 5GS V166 (523).
  • Ipstar 1 Nation: Thailand. Payload: Thaicom 4, LS-1300SX. Mass: 6,486 kg (14,299 lb). Class: Communications. Spacecraft: FS-1300. Manufacturer: Space Systems/Loral. Agency: Shin Satellite. Perigee: 35,777 km (22,230 mi). Apogee: 35,797 km (22,243 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2005-028A. USAF Sat Cat: 28786.

    Ariane 5GS version maiden flight. Launch delayed from July 8 and 11, 2005. Heaviest geosynchronous transfer orbit payload to date. As of 2007 Mar 11 located at 119.46E drifting at 0.009W degrees per day.

2006 - 22:15 GMT - Launch Site: Kourou. Launch Complex: ELA3. Launch Pad: -. Launch Vehicle: Ariane 5. Model: Ariane 5ECA. LV Configuration: Ariane 5ECA V172 (531).
  • JCSAT 10 Nation: Japan. Payload: AS2100AX. Mass: 4,048 kg (8,924 lb). Class: Communications. Spacecraft: AS 2100. Manufacturer: Lockheed Martin, Sunnyvale. Agency: JSAT. Perigee: 35,781 km (22,233 mi). Apogee: 35,793 km (22,240 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2006-033A. USAF Sat Cat: 29272.

    Ku/C-band television broadcasting satellite for the Japanese market; mass 1858 kg dry. As of 2007 Mar 11 located at 128.01E drifting at 0.012W degrees per day.

  • Syracuse 3B Nation: France. Payload: Spacebus 4000B3. Mass: 3,750 kg (8,260 lb). Class: Communications. Type: Military. Spacecraft: Spacebus 4000. Manufacturer: Alcatel Alenia Space. Agency: DGA. Perigee: 35,777 km (22,230 mi). Apogee: 35,796 km (22,242 mi). Inclination: 0.00 deg. Period: 1,436.10 min. COSPAR: 2006-033B. USAF Sat Cat: 29273.

    SHF and EHF military communications links for the French military. As of 2007 Mar 9 located at 5.21W drifting at 0.004W degrees per day.


Born on this day in:

Died on this day in:
  • 1999 - Robert (RT) Jones.  American Engineer. Cause of Death: Los Altos, Santa Clara, CA, SSN 549-46-9011.

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