| astronautix.com | March 24 |
1932 - Nation: Netherlands.
1932 - Nation: Russia.
1939 - Nation: USA.
Series P section B was a series of tests by Goddard in development of a gas generator to run turbines. Through April 28 a series of eleven static tests (Pa-k) of a new gas generator was made near the shop. The best form developed ran steadily for 10 sec at 180 psi for 250-psi tank pressures, with the rate of flow of oxygen at 0.49 lb/sec. References: 482 .
1949 - Nation: USA. Launch Site: 11.3 S / 82.1 W . Launch Vehicle: Aerobee. LV Configuration: RTV-N-8.
Cosmic radiation, magnetic field research. Launched at 1514 GMT. Reached 6 km.
1950 - Nation: USA. Launch Site: Wallops Island .
First successful ramjet research model flown at Wallops Island by NACA Langely's PARD. References: 17 .
1951 - Nation: USSR. Launch Vehicle: Buran.
Myasishchev was tasked with building an intercontinental jet-powered bomber, something veteran aircraft designer Tupolev said was impossible. Myasishchev managed to complete the first prototype 103M (called M-4 Bear in the West) bomber ten months after go-ahead. Myasishchev would later play a key role in Soviet spaceplane development.
1951 - Nation: USA.
1956 - Nation: USA.
Second powered flight, mach 0.91. References: 49 , 97 .
1957 - Nation: USA.
1958 - Nation: USSR. Launch Vehicle: Burya.
State Committee for Defence Technology (GKOT) Decree 'On the Creation of the Burya Winged Missile--course of work on 40 Burya' was issued. References: 474 .
1959 - Nation: USA. Launch Site: Wallops Island .
NASA announced that Wallops Station had made over 3,300 rocket firings since 1945. References: 17 .
1960 - Nation: USSR. Launch Site: Baikonur . Launch Vehicle: R-7A 8K74. LV Configuration: 8K74.
1961 - Nation: USA.
After analyzing launch vehicle behavior in the Mercury-Redstone 1A (MR-1A) and Mercury-Redstone 2 (MR-2), officials at the Marshall Space Flight Center and the Space Task Group were of the opinion that there were a number of problems that needed to be corrected prior to the advent of manned flight. The problems to be resolved included jet-vane vibration, instrumentation compartment vibration, failure of the thrust-controller system, and several other areas that needed attention. Many of these problems were studied by the personnel of engineering activities and proposed solutions were formulated. It was felt, however, that flight was necessary to verify the corrections and the Mercury-Redstone Booster Development test was scheduled and flown. All test objectives were met; as a result of this test, the launch vehicle was man-rated for the planned suborbital flights. References: 483 .
1961 - Nation: USA.
After booster problems on the Mercury MR-2 chimp test flight, Von Braun insisted on a further unmanned booster test flight, against the wishes of Shepard and others at NASA. A Mercury boilerplate capsule was launched on a flawless test on 24 March. If NASA had overruled Von Braun, the manned Freedom 7 capsule would have flown instead. Shepard would have been the first man in space (though not in orbit), beating Gagarin's flight by three weeks. References: 5 , 26 , 33 , 59 , 60 .
1961 - Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC13. Launch Vehicle: Atlas E. LV Configuration: Atlas 16E. FAILURE: Electrical Failure.
Suborbital test of Redstone modifications using a boilerplate Mercury capsule. The test was done at von Braun's insistence against Shepard's wishes, thereby putting the first US manned flight after Gagarin's. References: 5 , 26 , 59 .
1964 - Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17. Launch Vehicle: Delta C. LV Configuration: Thor LV-2C s/n 240 / Delta. FAILURE: Second stage fired, then shut down, repeating the sequence several times.
Suborbital test of subscale model of X-20 Dynasoar. Aero-thermodynamic structural test vehicle (ASV) for heat shield tests. Good first stage burn, but the second stage fired, then shut down, repeating the sequence several times. The spacecraft separated, and began to maneuver in a 60 degree bank to recover course, when the self-destruct package blew it apart. The debris impacted the Atlantic 800 km downrange near San Salvador Island. References: 5 , 126 .
1964 - - 22:22 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: LC1-1. Launch Vehicle: TA Thor Agena D. LV Configuration: Thor 2C s/n 396 / Agena D s/n 1175. FAILURE: Agena-D guidance system failed. No orbit.
KH-4A. Mission failed. References: 5 , 126 .
1966 - - 21:00 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC81L. Launch Vehicle: Proton 8K82. LV Configuration: Proton 8K82 s/n 211. FAILURE: Second stage malfunction.
1967 - - 11:44 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC41. Launch Vehicle: Kosmos 11K65.
Possible test flight. References: 1 , 2 , 5 , 6 , 279 .
1969 - - 10:04 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Voskhod 11A57.
High resolution photo reconnaissance satellite; returned film capsule; also carried science package. References: 1 , 2 , 6 .
1971 - - 21:05 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC3W. Launch Vehicle: LT Thor Agena D. LV Configuration: Thorad 2L s/n 538 / Agena D s/n 1660.
KH-4B. The overall image quality is good and comparable to the best of past missions. On-board program failed References: 1 , 2 , 5 , 6 .
1972 - - 08:46 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC10W. Launch Vehicle: Thor Burner. LV Configuration: Thor Burner 2A s/n 153.
Defense Meteorological Satellite Program. References: 1 , 2 , 5 , 6 .
The vehicle was turned off after its onboard fuel was depleted.
1977 - - 12:00 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Molniya 8K78M.
Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programmes to stations in the Orbita and participating international networks (international coope ration scheme). Uncertain if Molniya-1T model was Molniya-1 or Molniya-1T. References: 1 , 2 , 5 , 6 .
1979 - Nation: USA.
Ferry flight, shuttle carrier aircraft/Columbia (OV-102) from Eglin AFB to KSC (1 hour, 33 minutes) References: 15 .
1981 - - 03:31 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC41/1. Launch Vehicle: Molniya 8K78M.
Replace Molniya 3-11. Continued operation of the long-range telephone and telegraph radio-communication system within the Soviet Union and transmission of USSR central television programmes to stations in the Orbita and participating international networks (international coope ration scheme). References: 1 , 2 , 5 , 6 .
1982 - - 00:12 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC41/1. Launch Vehicle: Molniya 8K78M.
Replaced Molniya 3-15. Operation of the long-range telephone and telegraph radio communications system in the USSR; transmission of USSR Central Television programmes to stations in the Orbita network and within the framework of international cooperation. References: 1 , 2 , 5 , 6 .
1982 - - 19:40 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53767-253.
Military navigation satellite. Replaced Cosmos 1244. References: 1 , 2 , 5 , 6 .
1983 - - 20:52 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53739-548.
Carried COSPAS transponder; replaced Cosmos 1226. Investigation of the upper atmosphere and outer space; testing of systems for locating the position of ships and aircraft in difficulties (COSPAS-SARSAT system). References: 1 , 2 , 5 , 6 .
1987 - Nation: India. Launch Site: Sriharikota . Launch Vehicle: ASLV. LV Configuration: ASLV s/n ASLV-D1. FAILURE: Second stage failed to ignite.
1988 - - 14:09 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission. References: 1 , 2 , 6 , 179 .
1988 - - 21:05 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 s/n L15000-026.
Unmanned resupply vessel to Mir. Docked on 25 Mar 1988 22:21:35 GMT. Undocked on 5 May 1988 01:36:03 GMT. Destroyed in reentry on 5 May 1988 06:56:19 GMT. Total free-flight time 2.28 days. Total docked time 40.14 days. References: 1 , 2 , 6 , 275 .
1989 - - 13:26 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 65011-232.
Eight satellites launched by a single carrier rocket. References: 1 , 2 , 5 , 6 .
1989 - - 21:50 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17B. Launch Vehicle: Delta 3925. LV Configuration: Delta 3920-8 / Delta s/n 183.
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1992 - - 13:12 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC39A. Launch Vehicle: Shuttle. LV Configuration: STS-45.
Manned seven crew. Carried ATLAS-1 experimental package. Payloads: Atmospheric Laboratory for Applications and Science (ATLAS)-1, Shuttle Solar Backscat-ter Ultraviolet (SSBUV)-4, Getaway Special Experiment G-229, Space Tissue Loss (STL)-1, Radiation Monitoring Equipment (RME)-lIl, Visual Function Tester (VFT)-lI, Cloud Logic To Opti-mize Use of Defense Systems (CLOUDS)-1A, Investigations Into Polymer Membrane Process-ing (IPMP), Shuttle Amateur Radio Experiment (SAREX)-Il, Ultraviolet Plume Instrument (UVPl). Additional Details: STS-45. References: 1 , 2 , 5 , 6 , 7 .
1995 - Nation: USA. Launch Site: Vandenberg .
Final launch of an Atlas E booster from Vandenberg AFB (first launch on 7 June 1961). References: 88 .
1995 - - 14:09 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC3W. Launch Vehicle: Atlas E. LV Configuration: Atlas s/n 45E / Star-37S-ISS.
1998 - - 01:46 GMT. Nation: France. Launch Site: Kourou . Launch Complex: ELA2. Launch Vehicle: Ariane 4. LV Configuration: Ariane 40 s/n V107.
Developed by Matra Marconi Space/Toulouse for CNES, the satellite provided 10-m resolution images with a wide field of view. SPOT 4 also carried a wide field 'vegetation' imager and a laser communications experiment. Launch was by an Arianespace Ariane 40 rocket, the base Ariane 4 model with no strap-on boosters. The liquid hydrogen fuelled third stage of the Ariane 40 entered an 800 km sun-synchronous orbit together with SPOT 4.