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July 4
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See also Born on this Day On this day in: 1054 - - The Crab Nebula Supernova
1945 - Launch Vehicle: Corporal.
1957 - 17:15 GMT - Launch Site: Fort Churchill. Launch Vehicle: Aerobee 150. Model: Aerobee Hi. LV Configuration: Aerobee Hi NN3.08F. -
Aerobee 150 NRL NN3.08F Ionosphere mission Nation: USA. Agency: NRL. Apogee: 237 km (147 mi).
1958 - Launch Site: China Lake. Launch Complex: G-2. Launch Vehicle: Project Pilot. Model: Project Pilot 1. FAILURE: Vehicle exploded after 1 sec. -
Project Pilot Test mission Nation: USA. Agency: USN.
1960 -
1961 - 04:00 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Vehicle: R-7A. LV Configuration: R-7A L2-4. -
R-7A II-5 Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1961 - 20:20 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Vehicle: R-7A. LV Configuration: R-7A L2-2.
1966 - -
Soyuz simulators Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 1, Soyuz 2A, Souyz 3A, Soyuz 4A. The 7K-OK simulator consists of a mock-up of the BO living compartment and SA re-entry capsule only. The interiors are not yet fitted out with equipment, and development of the optical equipment to allow the cosmonauts to train with simulated dockings is proceeding very slowly. Mishin has promised a dozen times to speed up the work on the trainers, but produced nothing. Meanwhile Mishin is proceeding to train his cosmonaut team for Soyuz flights in September. It is said that he has other leaders, including Burnazyan and Keldysh, on his side.
1967 - 05:59 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: LC31. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57. LV Configuration: Voskhod 11A57 Ya15001-05.
1968 - 17:26 GMT - Launch Site: Vandenberg. Launch Complex: SLC2. Launch Pad: SLC2E. Launch Vehicle: Delta J. Model: Thor Delta J. LV Configuration: Thor Delta J 476/D57.
1971 - Launch Vehicle: N1.
1973 - Launch Site: Baikonur. Launch Complex: LC140. Launch Pad: LC140/18. Launch Vehicle: R-36M. Model: R-36M 15A14. -
R-36M State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1973 - Launch Site: Plesetsk. Launch Complex: LC43. Launch Pad: LC43. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57. FAILURE: Failure.
1973 - 01:15 GMT - Launch Site: Thumba. Launch Vehicle: Centaure. Model: Centaure 2A. LV Configuration: Centaure 2A ISRO 5.21. -
Centaure ISRO 5.21 Fields mission? Nation: India. Agency: ISRO. Apogee: 150 km (90 mi).
1973 - 03:27 GMT - Launch Site: Andoya. Launch Vehicle: Black Brant. Model: Black Brant VC. LV Configuration: Black Brant VC A-BBVC-49. -
Black Brant DLR A-BBVC-49 Barbara Aeronomy/Ionosphere mission Nation: Germany. Agency: DFVLR. Apogee: 260 km (160 mi).
1974 - Launch Site: Baikonur. Launch Complex: LC109. Launch Vehicle: R-36M. Model: R-36M 15A14. -
R-36M State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1975 - Launch Site: Baikonur. Launch Vehicle: UR-100N. FAILURE: Failure. -
UR-100N Operational missile test Nation: USSR. Agency: RVSN.
1975 - 00:56 GMT - Launch Site: Plesetsk. Launch Complex: LC132. Launch Pad: LC132/1. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53721-259.
1977 - 22:20 GMT - Launch Site: Plesetsk. Launch Complex: LC132. Launch Pad: LC132/2. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53746-303.
1978 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
Minuteman 1 ABRES ANT-2 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1980 - Launch Site: Baikonur. Launch Complex: LC109. Launch Vehicle: R-36M. Model: R-36M 15A14. -
R-36M DP Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1982 -
1983 - Launch Site: Kapustin Yar. Launch Vehicle: Kosmos 65MP. Model: K65M-RB.
1987 - 12:25 GMT - Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
1989 - 15:21 GMT - Launch Site: Plesetsk. Launch Complex: LC133. Launch Pad: LC133/3. Launch Vehicle: Kosmos 11K65M. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65061-250. -
Nadezhda 1 Nation: USSR. Payload: Tsikada-Kospas. Mass: 825 kg (1,818 lb). Class: Navigation. Spacecraft: Nadezhda. Agency: MO SSSR. Perigee: 956 km (594 mi). Apogee: 1,013 km (629 mi). Inclination: 83.00 deg. Period: 104.80 min. COSPAR: 1989-050A. USAF Sat Cat: 20103. Civilian maritime navigation satellite. Positioned in plane 11 of constellation. Signals at 150,00 MHz and 400.00 MHz. Carried COSPAS/SARSAT search and rescue package. Location of vessels in the Soviet merchant marine and fishing fleet; work within the international space search and rescue system for locating vessels and aircraft in distress (COSPAS-SARSAT).
1991 - 02:32 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17. Launch Pad: LC17A. Launch Vehicle: Delta 7000. Model: Delta 7925. LV Configuration: Delta 7925 D206.
1992 - 08:58 GMT - Launch Site: Arecibo. Launch Vehicle: Black Brant. Model: Black Brant IX. LV Configuration: Black Brant IX NASA 36.83DE. -
Black Brant EL COQUI AA-7 Plasma mission Nation: USA. Agency: NASA. Apogee: 250 km (150 mi).
1997 -
2000 - 23:44 GMT - Launch Site: Baikonur. Launch Complex: LC200. Launch Pad: LC200/39. Launch Vehicle: Proton 8K82K / 11S861. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 389-02.
2004 - 04:40 GMT - Launch Site: Balasore. Launch Complex: IC4. Launch Vehicle: Agni 1. -
Agni 1 Agni A-1 Test mission Nation: India. Agency: IDRDL. Apogee: 300 km (180 mi).
2005 - - Deep Impact, Comet Tempel 1 Impact/Flyby, Successful Spacecraft: Deep Impact.
2006 -
2006 - 18:32 GMT - Launch Site: Gitdaeryung. Launch Vehicle: Hwasong 6. - Agency: CMIK. Apogee: 150 km (90 mi).
Test
2006 - 18:38 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39. Launch Pad: LC39B. Launch Vehicle: Shuttle. Model: Space Shuttle. LV Configuration: STS-121. -
STS-121 Nation: USA. Program: ISS. Payload: Discovery F32 / Leonardo. Mass: 121,094 kg (266,966 lb). Class: Manned. Type: Spaceplane. Spacecraft: Discovery. Manufacturer: Boeing. Agency: NASA. Perigee: 332 km (206 mi). Apogee: 351 km (218 mi). Inclination: 51.60 deg. Period: 91.40 min. COSPAR: 2006-028A. USAF Sat Cat: 29251. Duration: 12.78 days. Crew: Lindsey, Kelly Mark, Fossum, Nowak, Wilson, Sellers, Reiter. Flight: STS-121, ISS EO-13, ISS Astrolab. The shuttle was launched using external tank ET-119 and solid motors RSRM-93. Cameras revealed that large chunks of foam were still shed from the external tank during the ascent to orbit. However examination of the heat shield using a new extension and sensors attached to the shuttle's robot arm revealed no significant damage. Discovery docked with the PMA-2 adapter on the Destiny module of the ISS at 14:52 GMT on 6 July. On July 7 the Leonardo cargo module was moved from the shuttle payload bay by the robot arm and docked to the Unity Module of the ISS between 09:42 and 11:50 GMT. The crew then began unloading the spare parts and supplies in the module to the station. A series of three EVAs conducted on 8 to 12 July tested the new equipment and techniques for repairing the shuttle heat shield in case of damage, and did some preliminary installations on the exterior of the ISS to pave the way for continued station assembly missions. On 14 July, the station's SSRMS robot moved the Leonardo module from the station back to the shuttle cargo bay between 13:08 and 14:50 GMT. The shuttle separated from the ISS, and fired its engines at 12:07 GMT on 17 July to make a 92 m/s deorbit maneuver. Discovery landed at the Kennedy Space Center at 13:14 GMT. European astronaut Reiter was left behind to make up part of the EO-13 resident crew on the station.
2006 - 19:04 GMT - Launch Site: Gitdaeryung. Launch Vehicle: Nodong 1. LV Configuration: Nodong 1 ?. - Agency: CMIK. Apogee: 150 km (90 mi).
Test
2006 - 22:12 GMT - Launch Site: Musudan. Launch Vehicle: Pekdosan 2. FAILURE: Failure. -
North Korean missile test Nation: Korea North. Agency: CMIK. Apogee: 150 km (90 mi). Test
2006 - 22:31 GMT - Launch Site: Gitdaeryung. Launch Vehicle: Nodong 1. - Agency: CMIK. Apogee: 150 km (90 mi).
Test
2006 - 22:32 GMT - Launch Site: Gitdaeryung. Launch Vehicle: Nodong 1. LV Configuration: Nodong 1 ?. - Agency: CMIK. Apogee: 150 km (90 mi).
Test
Died on this day in: - 1981 - Viktor Pavlovich Morozov. Russian Military Officer.
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© Mark Wade, 1997 - 2007 except where otherwise noted.
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