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March 4
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See also Born on this Day On this day in: 1945 - Launch Site: V-2 Gruppe Nord. Launch Vehicle: V-2.
1947 - -
Soviet Union rejects U.S. plan for UN atomic-energy control Nation: International.
1948 -
1953 - Launch Site: Cape Canaveral. Launch Vehicle: Hermes A-2. Model: RV-A-10. LV Configuration: RV-A-10 2. -
Hermes A-2 Test mission Nation: USA. Agency: USA. Apogee: 50 km (31 mi).
1957 - Launch Site: Baikonur. Launch Vehicle: R-7. -
Checkout of first R-7 starts Nation: USSR.
1958 - 06:02 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AM6.04. -
Nike-Cajun Aeronomy mission Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).
1958 - 19:30 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun AM6.05. -
Nike-Cajun Aeronomy mission Nation: USA. Agency: USAF. Apogee: 181 km (112 mi).
1959 - Launch Vehicle: R-12.
1960 - Launch Site: Edwards. Launch Complex: TL1. Launch Pad: TL2?. Launch Vehicle: Minuteman 1. Model: Minuteman 1A. FAILURE: Failure. -
Minuteman 1 Silo test launch Nation: USA. Agency: USAF.
1961 - Launch Site: Kapustin Yar. Launch Vehicle: R-12. -
R-12 V-1000 target mission Nation: USSR. Agency: OKB-30. Apogee: 460 km (280 mi).
1963 - Launch Site: Baikonur. Launch Complex: LC41. Launch Pad: LC41/4. Launch Vehicle: R-16. Model: R-16U. -
R-16 Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1964 - Launch Site: Baikonur. Launch Complex: LC41. Launch Pad: LC41/4?. Launch Vehicle: R-16. Model: R-16U. -
R-16 Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1964 - 09:53 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Vehicle: HAD. LV Configuration: HAD HAD 127. -
HAD Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 111 km (68 mi).
1965 - -
Apollo Boilerplate 28 third water drop test Nation: USA. Program: Apollo. Spacecraft: Apollo CSM. North American gave boilerplate 28 its third water drop test. Upon impact, the spacecraft again suffered some structural damage to the heatshield and the core, though much less than it had experienced on its initial drop. Conditions in this test were at least as severe as in previous ones, yet the vehicle remained watertight.
1965 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: Bacchus?. Launch Vehicle: Centaure. LV Configuration: Centaure C85. -
Centaure Solar mission? Nation: France. Agency: CNES. Apogee: 120 km (70 mi).
1965 - 18:32 GMT - Launch Site: Barking Sands. Launch Vehicle: HJ Nike Nike. LV Configuration: HJ Nike Nike Sandia 152-16. -
HJ Nike Nike Test mission Nation: USA. Agency: Sandia. Apogee: 181 km (112 mi).
1966 - 12:29 GMT - Launch Site: Vandenberg. Launch Complex: ABRES. Launch Pad: ABRESA1. Launch Vehicle: Atlas D. LV Configuration: Atlas D 303D. FAILURE: Failure. -
Atlas D NTMP KX-35 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 500 km (310 mi).
1967 - Launch Site: Baikonur. Launch Complex: PU32. Launch Vehicle: R-36. Model: R-36 8K67. -
R-36 Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1967 - Launch Site: Baikonur. Launch Complex: LC41. Launch Pad: LC41/3?. Launch Vehicle: R-16. Model: R-16U. -
R-16 Operational missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1967 - 20:05 GMT - Launch Site: Eglin. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AF07.582. -
Nike Iroquois Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 196 km (121 mi).
1968 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3P-666. -
Polaris A3 Operational Test mission Nation: USA. Agency: RN. Apogee: 1,000 km (600 mi).
1968 - 13:06 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: LC13. Launch Vehicle: Atlas / Agena D SLV-3A. Model: SLV-3A Agena D. LV Configuration: SLV-3A Agena D 5602A (AA26) / Agena D 6503 (AA26). -
OGO 5 Nation: USA. Payload: OGO E. Mass: 634 kg (1,397 lb). Class: Earth. Type: Magnetosphere. Spacecraft: OGO. Agency: NASA GSF. Perigee: 36,021 km (22,382 mi). Apogee: 111,034 km (68,993 mi). Inclination: 50.30 deg. Period: 3,746.50 min. COSPAR: 1968-014A. USAF Sat Cat: 3138. OGO 5 carried 25 experiments, 17 of which were particle studies, and two were magnetic field studies. In addition, there was one each of the following types of experiments: radio astronomy, UV spectrum, Lyman-alpha, solar X ray, plasma waves, and electric field. By April 1971, spacecraft perigee had increased to 26,400 km and inclination had increased to 54 deg. The spacecraft attitude control failed on August 6, 1971, after 41 months of normal operation. The spacecraft was placed in a standby status on October 8, 1971. Four experiments (Meyer, Blamont, Thomas, and Simpson) were reactivated for the period from June 1 to July 13, 1972, after which all operational support terminated. Spacecraft orbit parameters changed significantly over the spacecraft life.
1969 - 19:30 GMT - Launch Site: Vandenberg. Launch Complex: SLC4. Launch Pad: SLC4W. Launch Vehicle: Titan 3B. Model: Titan IIIB. LV Configuration: Titan IIIB 3B-7.
1970 - Launch Site: Vandenberg. Launch Complex: LF09. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 782. -
Minuteman 1 FOT GT54B Follow-on Test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1970 - 12:14 GMT - Launch Site: Plesetsk. Launch Complex: LC43. Launch Pad: LC43/4. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57.
1970 - 14:30 GMT - Launch Complex: Barter I. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.88GE.
1970 - 14:41 GMT - Launch Site: Poker Flat. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.109GE. -
Nike Tomahawk Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).
1970 - 22:15 GMT - Launch Site: Vandenberg. Launch Complex: SLC3. Launch Pad: SLC3W. Launch Vehicle: Thorad Agena D SLV-2H. Model: Thorad SLV-2H Agena D. LV Configuration: Thorad SLV-2H Agena D 551 / Agena D 1657.
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OPS 3402 Nation: USA. Payload: EHH B18. Class: Sigint. Spacecraft: SSF. Agency: USAF. COSPAR: 1970-016xx. USAF Sat Cat: 4343. Decay Date: 1971-11-10.
1971 - Launch Vehicle: N1, UR-700. -
N1/L3 Expert Commission Nation: USSR. Program: Lunar L3. Spacecraft: Soyuz 7KT-OK, LK-700, Krechet. Pushkin and Kuznetsov brief Kamanin on the results of the N1/L3 expert commission. They found that the N1/L3 is unreliable and that the design needs to be fundamentally re-examined. Therefore the Soviet Ministers and Central Committee passed a decree that the commission must determine by 1 May 1971 what to do with the lunar project. Kamanin's opinion: abandon the N1-L3, modify Chelomei's UR-700 design to replace it, and design a new lunar landing spacecraft for missions in 1974-1975. Mishin is afraid of such a solution. Kamanin believes that the commission, headed by Keldysh, will finally recommend continued development and flight of Mishin's bad booster and even worse spacecraft. It is true that the N1 design has been substantially reworked in the last 18 months, but Kamanin believes it to be fundamentally flawed and that nothing can make it reliable. After Mishin pushed his Indian Ocean recovery plan for the L3, the VVS insisted on sea trials of the capsule. These showed the cosmonauts had to get out within 30 to 35 minutes before the valves to the interior started leaking seawater. The L3 is also unsafe due to the EVA method of transfer to the LK of a single unassisted cosmonaut. The Krechet spacesuit is very bulky and unmanoeuvrable. Prague wanted Gagarin's widow for International Women's Day.since Tereshkkova couldn't go, but she wants no part of public appearances.
1972 - 10:00 GMT - Launch Site: Plesetsk. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57.
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Nauka Cosmos 477 Nation: USSR. Payload: Nauka. Spacecraft: Nauka. Agency: MOM. Perigee: 197 km (122 mi). Apogee: 291 km (180 mi). Inclination: 72.80 deg. Period: 89.38 min. COSPAR: 1972-013E. USAF Sat Cat: 5882. Decay Date: 1972-03-23.
1972 - 11:52 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12. -
MR-12 Aeronomy/Plasma mission Nation: USSR. Apogee: 174 km (108 mi).
1972 - 16:48 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12. -
MR-12 Aeronomy/Ionosphere/Chemical release mission Nation: USSR. Apogee: 184 km (114 mi).
1972 - 18:22 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12. -
MR-12 Aeronomy/Chemical release mission Nation: USSR. Apogee: 173 km (107 mi).
1975 - 07:39 GMT - Launch Site: Poker Flat. Launch Vehicle: Nike Javelin. LV Configuration: Nike Javelin DNA IC506.14-2. -
Nike Javelin ICECAP 75A Auroral mission Nation: USA. Agency: USAF. Apogee: 130 km (80 mi).
1976 - Launch Site: Vandenberg. Launch Complex: LF25. Launch Vehicle: Minuteman 3. -
Minuteman 3 FOT GT52GB Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).
1976 - 03:01 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12. -
MR-12 Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 175 km (108 mi).
1978 - 07:40 GMT - Launch Site: Baikonur. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
1980 - 10:30 GMT - Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
1982 - Launch Site: Kapustin Yar. Launch Complex: LC107. Launch Pad: LC107/1. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53739-530. FAILURE: Launch vehicle failed to orbit - unknown cause.
1988 - Launch Site: Baikonur. Launch Complex: Jubilee.
1988 - 06:55 GMT - Launch Site: Poker Flat. Launch Vehicle: Black Brant. Model: Black Brant X. LV Configuration: Black Brant X NASA 35.023GE. -
Black Brant UCB Alaska '88 Plasma mission Nation: USA. Agency: NASA. Apogee: 1,000 km (600 mi).
1989 - 01:02 GMT - Launch Site: Kiruna. Launch Vehicle: Black Brant. Model: Black Brant VC. LV Configuration: Black Brant VC NASA 21.96GE. -
Black Brant Auroral mission Nation: USA. Agency: NASA. Apogee: 175 km (108 mi).
1990 -
1992 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Vehicle: Peacekeeper. LV Configuration: Peacekeeper 08PA. -
Peacekeeper Operational Test mission Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi).
1992 - 04:27 GMT - Launch Site: Plesetsk. Launch Complex: LC43. Launch Pad: LC43/4. Launch Vehicle: Molniya 8K78M. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M ML.
1994 - 13:53 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39. Launch Pad: LC39B. Launch Vehicle: Shuttle. Model: Space Shuttle. LV Configuration: Space Shuttle STS-62. -
STS-62 Nation: USA. Program: STS. Payload: Columbia F16 / USMP-2 / OAST-2. Mass: 8,870 kg (19,550 lb). Class: Manned. Type: Spaceplane. Spacecraft: Columbia. Agency: NASA JSC. Perigee: 246 km (152 mi). Apogee: 309 km (192 mi). Inclination: 39.00 deg. Period: 90.40 min. COSPAR: 1994-015A. USAF Sat Cat: 23025. Duration: 13.97 days. Decay Date: 1994-03-31. Crew: Allen Andy, Casper, Gemar, Ivins, Thuot. Flight: STS-62. Carried USMP-2, OAST-2, SAMPIE, TES, EISG. Payloads: United States Microgravity Payload (USMP) 2, Office of Aeronautics and Space Technology (OAST) 2, Dexterous End Effector (DEE), Shuttle Solar Backscatter Ultraviolet/A (SSBUV/A), Limited-Duration Space Environment Candidate Material Exposure (LDCE), Advanced Protein Crystal Growth (APCG), Physiological Systems Experiment (PSE), Commercial Protein Crystal Growth (CPCG), Commercial Generic Bioprocessing Apparatus (CGBA), Auroral Photography Experiment Phase B (APE-B), Middeck Zero-Gravity Dynamics Experiment (MODE), Air Force Maui Optical Site (AMOS) Calibration Test, Bioreactor Demonstration System A.
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USMP-2 Fwd Nation: USA. Program: STS. Agency: NASA. COSPAR: 1994-015xx. USAF Sat Cat: 23025. Decay Date: 1994-03-18.
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EDO Nation: USA. Program: STS. Agency: NASA. COSPAR: 1994-015xx. USAF Sat Cat: 23025. Decay Date: 1994-03-18.
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USMP-2 Aft Nation: USA. Program: STS. Agency: NASA. COSPAR: 1994-015xx. USAF Sat Cat: 23025. Decay Date: 1994-03-18.
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OAST-2 Nation: USA. Program: STS. Agency: NASA. COSPAR: 1994-015xx. USAF Sat Cat: 23025. Decay Date: 1994-03-18.
1995 - Launch Site: Wallops Island. Launch Vehicle: Aries. -
Aries LEAP FTV-3 Target Target mission Nation: USA. Agency: BMDO. Apogee: 300 km (180 mi).
1997 - 02:00 GMT - Launch Site: Svobodniy. Launch Complex: LC5. Launch Pad: LC5. Launch Vehicle: Start-1. Model: Start-1.2. -
Zeya Nation: Russia. Payload: Zeya No. 1. Class: Communications. Spacecraft: Zeya. Manufacturer: NPO Prikladnoi Mekhaniki, Zhelenogorsk. Agency: MO RF. Perigee: 460 km (280 mi). Apogee: 472 km (293 mi). Inclination: 97.30 deg. Period: 93.60 min. COSPAR: 1997-010A. USAF Sat Cat: 24744. Decay Date: 1999-10-25.
2002 -
2004 - Launch Site: Mojave. Launch Vehicle: Tier One.
2005 - - Rosetta, first Earth Gravity Assist, Successful Spacecraft: Rosetta.
Born on this day in:
Died on this day in: - 1974 - Mikhail Klavdiyevich Tikhonravov
. Russian Engineer.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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