Encyclopedia Astronautica
November 12


November 12 Chronology


1903 November 12 - .
1908 November 12 - .
1932 November 12 - . Launch Vehicle: ARS.
  • AIS tests rocket motor. - . Nation: USA. Summary: American Interplanetary Society performed static tests of rocket based on VfR design at Stockton, New Jersey. The motor produced 27 kgf of thrust for 20-30 seconds. It was damaged in the test and not subsequently flown..

1937 November 12 - .
1944 November 12 - . Launch Site: Heidekraut. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 19510. FAILURE: Exploded after launch.
  • V-2 Ma263 235 L9 - . Nation: Germany. Summary: Planned range 250 km. Exploded after launch 50 km to the right of the planned trajectory. Circular error 207.1 km from aim point..

1946 November 12 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 5R.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1948 November 12 - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 30R.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1952 November 12 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Deacon.
  • XF2Y-1 Model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1953 November 12 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-1. Launch Vehicle: R-1 8A11. LV Configuration: R-1 8A11 No 1120.
  • Operational test - . Nation: USSR. Agency: Korolev. Apogee: 100 km (60 mi).

1954 November 12 - .
  • Birth of John Edward 'Hawk' Hawker - . Nation: USA. Summary: American photointerpreter payload specialist astronaut, 1988-1991. Chief Warrant Officer CW3, US-Army; graduated from Rotary Wing Flight School; in 1988 selected for TERRA SCOUT - US Army Project; retired from USA on 1994.04.01..

1954 November 12 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Snark. Launch Vehicle: Snark. LV Configuration: Snark N-69B GM-11116.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 10 km (6 mi).

1956 November 12 - . 11:47 GMT - . Launch Site: Fort Churchill. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-A-1a. LV Configuration: Aerobee RTV-A-1a SM1.01.
  • Grenades Aeronomy mission - . Nation: USA. Agency: USA. Apogee: 67 km (41 mi). Summary: Temperature, winds research. Launched at 0546 local time. Reached 67.5 km..

1958 November 12 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LA. Launch Pad: LA?. LV Family: Matador. Launch Vehicle: Matador. LV Configuration: Matador Training #1.
  • Test mission - . Nation: USA. Agency: USAF. Apogee: 12 km (7 mi).

1959 November 12 - . 19:24 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Thor DM-18A. LV Configuration: Thor DM-18A 181.
  • IWST - . Nation: USA. Agency: RAF. Apogee: 520 km (320 mi).

1960 November 12 - . 18:40 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.24GE.
  • SBE 8 (LE SCR) Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 129 km (80 mi).

1960 November 12 - . 20:43 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1E. LV Family: Delta. Launch Vehicle: Thor Agena B. LV Configuration: Thor Agena B 297 / Agena B 1062.
  • Discoverer 17 - . Payload: KH-2 9012 / Agena B 1062. Mass: 1,091 kg (2,405 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-2. Decay Date: 1960-12-29 . USAF Sat Cat: 61 . COSPAR: 1960-Omicron-1. Apogee: 984 km (611 mi). Perigee: 190 km (110 mi). Inclination: 81.7000 deg. Period: 96.40 min. KH-1; film capsule recovered 2.1 days later. Mission failed. Obtained orbit successfully. Film separated before any camera operation leaving only 1.7 ft of film in capsule. On December 2, the Air Force revealed that exceedingly valuable information had been obtained from human tissues carried by Discoverer 17 (the cover story for the mission). The tissues had been exposed to an unexpectedly heavy dose of radiation for more than 50 hours in flight.

1960 November 12 - . 23:32 GMT - . Launch Site: Fort Churchill. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.15GE.
  • SBE 9 Magnetosphere mission - . Nation: USA. Agency: NASA. Apogee: 129 km (80 mi).

1961 November 12 - . LV Family: Atlas. Launch Vehicle: Atlas D.
  • Mercury 5 launch postponed - . Nation: USA. Program: Mercury. Class: Manned. Type: Manned spacecraft. Spacecraft: Mercury. Summary: Mercury-Atlas 5, scheduled for launch no earlier than November 14, ran into technical difficulties, postponing launch for several days..

1962 November 12 - .
  • Plans for Vostok female cosmonaut flight discussed. - . Nation: USSR. Program: Vostok. Flight: Vostok 5; Vostok 6; Vostok 6A. A meeting was held to discuss alternatives for the next two Vostok flights. Alternatives were simultaneous flight of two capsules, each with a female cosmonaut; or one female flight and a male 5 to 7 day flight. The flight would occur no earlier than April 1963.

1963 November 12 - . LV Family: Saturn V. Launch Vehicle: Saturn V.
  • Contract for the construction of Saturn V LC-39A - . Nation: USA. Program: Apollo. Summary: NASA awarded a $19.2 million contract to Blount Brothers Corporation and M. M. Sundt Construction Company for the construction of Pad A, part of the Saturn V Launch Complex 39 at LOC..

1963 November 12 - . 18:58 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.76UA.
  • JHU Airglow 6 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 223 km (138 mi).

1964 November 12 - . 03:05 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 8L. LV Configuration: Kappa 8L K-8L-6.
  • Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 100 km (60 mi).

1964 November 12 - . 10:00 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: HAD. LV Configuration: HAD 157.
  • Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 103 km (64 mi).

1964 November 12 - . 10:53 GMT - . Launch Site: Atlantic Ocean. Launch Pad: 35.0 N x 75.0 W. Launch Platform: CVE-25. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.116CA.
  • Sodium release Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 204 km (126 mi). Summary: Launched from Atlantic Ocean during Croatan 1964 cruise..

1964 November 12 - . 10:56 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.113CA.
  • Sodium release Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 204 km (126 mi).

1964 November 12 - . 19:30 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NE3.155.
  • Solar ultraviolet mission - . Nation: USA. Agency: NRL. Apogee: 189 km (117 mi).

1965 November 12 - .
  • Apollo portable life support system Preliminary Design Review - . Nation: USA. Program: Apollo. Spacecraft: A7L. Summary: The portable life support system Preliminary Design Review was completed. The design was essentially complete and no major discrepancies were noted during the review..

1965 November 12 - .
  • USAF MOL Astronaut Training Group 1 selected. - . Nation: USA. Related Persons: Adams; Finley; Lawyer; Macleay; Neubeck; Taylor. The group was selected to provide crews for flights of the Manned Orbiting Laboratory, a classified military manned space station.. Qualifications: Qualified military pilot; graduate of Aerospace Research Pilot School; serving military officer; US citizen by birth..

1965 November 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/4. LV Family: R-16. Launch Vehicle: R-16U.
  • Military training launch - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1965 November 12 - . Launch Site: Barking Sands. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-84.
  • Environment Aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi).

1965 November 12 - . 05:02 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Molniya 8K78M.
  • Venera 2 - . Payload: 3MV-4 s/n 4. Mass: 962 kg (2,120 lb). Nation: USSR. Agency: MOM. Program: Venera. Class: Venus. Type: Venus probe. Spacecraft: Venera 3MV-4. USAF Sat Cat: 1730 . COSPAR: 1965-091A. Apogee: 315 km (195 mi). Perigee: 205 km (127 mi). Inclination: 51.8000 deg. Period: 89.71 min. Venera 2 was launched towards the planet Venus and carried a TV system and scientific instruments. On February 27, 1966, the spacecraft passed Venus at a distance of 24,000 km and entered a heliocentric orbit. The spacecraft system had ceased to operate before the planet was reached and returned no data.

1965 November 12 - . 22:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1 C2X-4.
  • STAFF 4 test - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1966 November 12 - . Launch Site: Las Palmas. LV Family: Berenice. Launch Vehicle: Titus. LV Configuration: Titus 001.
  • FU-150 A Solar Eclipse mission - . Nation: France. Agency: CNES. Apogee: 274 km (170 mi).

1966 November 12 - . 09:50 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 131 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4. Duration: 8.00 days. Decay Date: 1966-11-20 . USAF Sat Cat: 2568 . COSPAR: 1966-105A. Apogee: 335 km (208 mi). Perigee: 202 km (125 mi). Inclination: 72.8000 deg. Period: 89.80 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1966 November 12 - . 10:40 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.191DS.
  • NRL ND3.188 XUV-H2? Solar extreme ultraviolet / eclipse mission - . Nation: USA. Agency: NASA; NRL. Apogee: 174 km (108 mi).

1966 November 12 - . 12:00 GMT - . Launch Site: Cassino. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-93.
  • Solar x-ray / eclipse mission - . Nation: USA. Agency: Sandia. Apogee: 297 km (184 mi).

1966 November 12 - . 13:42 GMT - . Launch Site: Las Palmas. LV Family: Berenice. Launch Vehicle: Titus. LV Configuration: Titus 002.
  • FU-150 B Solar Eclipse mission - . Nation: France. Agency: CNES. Apogee: 270 km (160 mi).

1966 November 12 - . 13:54 GMT - . Launch Site: Cassino. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-94.
  • Solar x-ray / eclipse mission - . Nation: USA. Agency: Sandia. Apogee: 115 km (71 mi).

1966 November 12 - . 14:01 GMT - . Launch Site: Cassino. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.77CA.
  • Aeronomy / eclipse mission - . Nation: USA. Agency: NASA. Apogee: 185 km (114 mi).

1966 November 12 - . 14:05 GMT - . Launch Site: Cassino. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.274UI.
  • Ionosphere / eclipse mission - . Nation: USA. Agency: NASA. Apogee: 197 km (122 mi).

1966 November 12 - . 14:07 GMT - . Launch Site: Cassino. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.302UI.
  • Ionosphere / eclipse mission - . Nation: USA. Agency: NASA. Apogee: 160 km (90 mi).

1966 November 12 - . 14:10 GMT - . Launch Site: Cassino. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.304UI.
  • Ionosphere / eclipse mission - . Nation: USA. Agency: NASA. Apogee: 195 km (121 mi).

1966 November 12 - . 14:29 GMT - . Launch Site: Cassino. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-9 Sandia 152-95.
  • Solar x-ray / eclipse mission - . Nation: USA. Agency: Sandia. Apogee: 115 km (71 mi).

1966 November 12 - . 14:45 GMT - . Launch Site: Cassino. LV Family: Nike. Launch Vehicle: Nike Hydac.
  • Solar mission - . Nation: USA. Agency: AFCRL. Apogee: 250 km (150 mi).

1966 November 12 - . 14:55 GMT - . Launch Site: Cassino. LV Family: Nike. Launch Vehicle: Nike Hydac. LV Configuration: Nike Hydac D-4.
  • Ionosphere mission - . Nation: USA. Agency: AFCRL. Apogee: 115 km (71 mi).

1966 November 12 - . 15:09 GMT - . Launch Site: Cassino. LV Family: Nike. Launch Vehicle: Nike Hydac. LV Configuration: Nike Hydac D-11.
  • Ionosphere mission - . Nation: USA. Agency: AFCRL. Apogee: 250 km (150 mi).

1966 November 12 - . 15:22 GMT - . Launch Site: Cassino. LV Family: Nike. Launch Vehicle: Nike Hydac. LV Configuration: Nike Hydac D-13.
  • Ionosphere mission - . Nation: USA. Agency: AFCRL. Apogee: 115 km (71 mi).

1966 November 12 - . 15:35 GMT - . Launch Site: Cassino. LV Family: Sonda. Launch Vehicle: Sonda 1. LV Configuration: Sonda 1 D-16C.
  • Eclipse mission - . Nation: Brazil. Agency: IAE. Apogee: 65 km (40 mi).

1966 November 12 - . 16:00 GMT - . Launch Site: Cassino. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.303UI.
  • Ionosphere / eclipse mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1966 November 12 - . 16:15 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.153GS.
  • Solar eclipse mission - . Nation: USA. Agency: NASA. Apogee: 151 km (93 mi).

1966 November 12 - . 16:15 GMT - .
  • EVA Gemini 12-1 - . Crew: Aldrin. EVA Type: Stand-Up External Vehicular Activity. EVA Duration: 0.10 days. Nation: USA. Related Persons: Aldrin. Program: Gemini. Class: Manned. Type: Manned spacecraft. Flight: Gemini 12. Spacecraft: Gemini. Summary: Photographed earth and stars..

1968 November 12 - .
1968 November 12 - .
  • Land landing of the Apollo CSM in the area of the launch site after an abort assessed - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Recovery. The Apollo Crew Safety Review Board met to assess land landing of the CSM in the area of the launch site if a flight were aborted just before launch or during the initial phase of a flight. In general the Board was satisfied with overall planned recovery and medical operations. The only specific item to be acted on was some means of purging the interior of the spacecraft to expel any coolant or propellant fumes that might be trapped inside the cabin. The Board was also concerned about the likelihood of residual propellants trapped inside the vehicle even after abort sequence purging, a problem that MSC secured assistance from both the Ames and Lewis Research Centers to solve. At the Board's suggestion, MSC's Crew Systems Division also investigated the use of a helmet liner for the astronauts to prevent head injury upon impact. Finally, the Board recommended continued egress training with fully suited crews, including some night training.

1969 November 12 - . 11:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC41/1. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 309 - . Payload: Zenit-2 11F61 s/n 80. Mass: 4,720 kg (10,400 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2. Duration: 8.00 days. Decay Date: 1969-11-20 . USAF Sat Cat: 4223 . COSPAR: 1969-098A. Apogee: 364 km (226 mi). Perigee: 185 km (114 mi). Inclination: 64.5000 deg. Period: 90.00 min. Summary: Area survey photo reconnaissance satellite. First flight with Nauka external experiment container..
  • Nauka - . Payload: Nauka 3KS. Nation: USSR. Agency: MOM. Spacecraft: Nauka. Decay Date: 1969-11-30 . USAF Sat Cat: 4236 . COSPAR: 1969-098E. Apogee: 334 km (207 mi). Perigee: 188 km (116 mi). Inclination: 65.4000 deg. Period: 89.73 min.

1970 November 12 - . 11:00 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA2. Launch Vehicle: Cockatoo. LV Configuration: Cockatoo 105.
  • Lunar ultraviolet Ozone Aeronomy mission - . Nation: Australia. Agency: WRE. Apogee: 104 km (64 mi).

1971 November 12 - . Launch Site: WTR Launch Area. Launch Platform: EAG-154. LV Family: Polaris. Launch Vehicle: Polaris A2.
  • Safeguard M2-8 Target mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1973 November 12 - .
  • Death of Anatoli Alekeseyevich Vasilyev - . Nation: Russia. Related Persons: Vasilyev. Summary: Russian officer. Commander of GURVO 1964-1967. Chaired the Scientific-Technical Committee of the Strategic Missile Forces 1967-1969..

1973 November 12 - . 14:00 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.102UG.
  • Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 172 km (106 mi).

1973 November 12 - . 14:50 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.100DS.
  • Solar mission - . Nation: USA. Agency: NASA. Apogee: 154 km (95 mi).

1974 November 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC177. LV Family: MR-UR-100. Launch Vehicle: MR-UR-100.
  • Operational test launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 November 12 - . Launch Site: Baikonur. Launch Complex: Baikonur LC103. LV Family: R-36M. Launch Vehicle: R-36M. FAILURE: Failure.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1975 November 12 - .
  • X-24 Flight 62 - . Crew: Enevoldson. Payload: X-24B flight 34. Nation: USA. Related Persons: Enevoldson. Class: Manned. Type: Manned spaceplane. Spacecraft: X-24B. Summary: Maximum Speed - 734 kph. Maximum Altitude - 13720 m. Flight Time - 241 sec..

1976 November 12 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF21. LV Family: Minuteman. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 STM-12W.
  • Research and development launch - . Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1977 November 12 - . 06:59 GMT - . Launch Site: Poker Flat. Launch Vehicle: Rocketsonde.
  • Starute, Datasonde - . Nation: USA. Agency: MRN. Apogee: 50 km (31 mi).

1979 November 12 - . 16:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHOK. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1980 November 12 - .
  • Voyager 1, Saturn Flyby - . Nation: USA. Spacecraft: Voyager.

1980 November 12 - .
1980 November 12 - . 12:21 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1221 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-6U. Duration: 14.00 days. Decay Date: 1980-11-26 . USAF Sat Cat: 12058 . COSPAR: 1980-090A. Apogee: 399 km (247 mi). Perigee: 196 km (121 mi). Inclination: 72.9000 deg. Period: 90.50 min. Summary: Photo surveillance; returned film capsule..

1981 November 12 - .
1981 November 12 - . 15:10 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-2.
  • STS-2 - . Call Sign: Columbia. Crew: Engle; Truly. Payload: Columbia F02 / DFI. Mass: 8,517 kg (18,776 lb). Nation: USA. Related Persons: Engle; Truly. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-2. Spacecraft: Columbia. Duration: 2.26 days. Decay Date: 1981-11-14 . USAF Sat Cat: 12953 . COSPAR: 1981-111A. Apogee: 231 km (143 mi). Perigee: 222 km (137 mi). Inclination: 38.0000 deg. Period: 89.00 min. Summary: Second shuttle test flight. Payloads: Office of Space and Terrestrial Applications (OSTA)-1 experiments, Orbiter Experiments (OEX)..
  • OSTA-1 - . Nation: USA. Agency: NASA. Program: STS. Decay Date: 1981-11-14 . USAF Sat Cat: 12953 . COSPAR: 1981-111xx. Apogee: 265 km (164 mi). Perigee: 255 km (158 mi). Inclination: 38.0000 deg. Period: 89.70 min.
  • DFI - . Payload: DFI PLT. Nation: USA. Agency: NASA. Program: STS. Decay Date: 1981-11-14 . USAF Sat Cat: 12953 . COSPAR: 1981-111xx. Apogee: 265 km (164 mi). Perigee: 255 km (158 mi). Inclination: 38.0000 deg. Period: 89.70 min.

1982 November 12 - . 07:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: KRENKEL'. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 59 km (36 mi).

1984 November 12 - . 13:25 GMT - .
  • EVA STS-51-A-1 - . Crew: Allen; Gardner. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.26 days. Nation: USA. Related Persons: Allen; Gardner. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-51-A. Spacecraft: Discovery. Summary: Retrieved Palapa satellite..

1985 November 12 - . 21:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 86 km (53 mi).

1986 November 12 - . 16:45 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC47. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 62 km (38 mi).

1987 November 12 - . 00:16 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A Sphere.
  • MAC / EPSILON E-F4 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 106 km (65 mi).

1987 November 12 - . 00:21 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-151.
  • MAC / E-T4 Ferdinand74 Test / aeronomy / ionosphere mission - . Nation: Norway. Agency: DLR. Apogee: 125 km (77 mi).

1987 November 12 - . 00:21 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-152.
  • MAC / E-T5 Total 11 Aeronomy mission - . Nation: Norway. Agency: DLR. Apogee: 125 km (77 mi).

1987 November 12 - . 00:22 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion NASA 31.65UE.
  • NEFS Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 124 km (77 mi).

1991 November 12 - . 20:09 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32. Launch Pad: LC32/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 2165 - . Payload: Strela-3 no. 65. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 21779 . COSPAR: 1991-077A. Apogee: 1,412 km (877 mi). Perigee: 1,395 km (866 mi). Inclination: 82.6000 deg. Period: 113.90 min. Summary: Six satellites launched by a single carrier rocket..
  • Cosmos 2166 - . Payload: Strela-3 no. 66. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 21780 . COSPAR: 1991-077B. Apogee: 1,412 km (877 mi). Perigee: 1,407 km (874 mi). Inclination: 82.6000 deg. Period: 114.00 min.
  • Cosmos 2167 - . Payload: Strela-3 no. 67. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 21781 . COSPAR: 1991-077C. Apogee: 1,412 km (877 mi). Perigee: 1,400 km (800 mi). Inclination: 82.6000 deg. Period: 113.90 min.
  • Cosmos 2168 - . Payload: Strela-3 no. 68. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 21782 . COSPAR: 1991-077D. Apogee: 1,412 km (877 mi). Perigee: 1,390 km (860 mi). Inclination: 82.6000 deg. Period: 113.80 min.
  • Cosmos 2169 - . Payload: Strela-3 no. 69. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 21783 . COSPAR: 1991-077E. Apogee: 1,413 km (877 mi). Perigee: 1,383 km (859 mi). Inclination: 82.6000 deg. Period: 113.70 min.
  • Cosmos 2170 - . Payload: Strela-3 no. 70. Mass: 220 kg (480 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-3. USAF Sat Cat: 21784 . COSPAR: 1991-077F. Apogee: 1,414 km (878 mi). Perigee: 1,412 km (877 mi). Inclination: 82.6000 deg. Period: 114.10 min.

1995 November 12 - . 12:30 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39A. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-74.
  • STS-74 - . Call Sign: Atlantis. Crew: Cameron; Hadfield; Halsell; McArthur; Ross. Payload: Atlantis F15 / 316GK SM. Mass: 6,134 kg (13,523 lb). Nation: USA. Related Persons: Cameron; Hadfield; Halsell; McArthur; Ross. Agency: NASA Houston. Program: Mir. Class: Manned. Type: Manned spaceplane. Flight: STS-74; Mir EO-20. Spacecraft: Atlantis. Duration: 8.19 days. Decay Date: 1995-11-20 . USAF Sat Cat: 23714 . COSPAR: 1995-061A. Apogee: 342 km (212 mi). Perigee: 257 km (159 mi). Inclination: 51.6000 deg. Period: 91.40 min. Rendezvoused and docked with Mir space station on November 15. Delivered the Russian-built 316GK Shuttle-Mir docking module to Mir.Payloads: Shuttle-Mir Mission 2; docking module with two attached solar arrays; IMAX Cargo Bay Camera (ICBC); Glow Experiment (GLO-4)/ Photogrammetric Appendage Structural Dynamics Experiment (PASDE) Payload (GPP); Shuttle Amateur Radio Experiment (SAREX) II.
  • External Airlock/ODS - . Payload: EAL/ODS. Nation: USA. Agency: NASA. Program: Mir. Flight: STS-74; Mir EO-20. Decay Date: 1995-11-20 . USAF Sat Cat: 23714 . COSPAR: 1995-061xx. Apogee: 347 km (215 mi). Perigee: 336 km (208 mi). Inclination: 51.6000 deg. Period: 91.40 min.
  • Mir-Shuttle Docking Module - . Payload: DM 316GK s/n 1. Mass: 6,134 kg (13,523 lb). Nation: Russia. Agency: NASA. Manufacturer: Korolev. Program: Mir. Class: Manned. Type: Manned space station. Flight: STS-74; Mir EO-20. Spacecraft: Mir-Shuttle Docking Module. Duration: 8.19 days. COSPAR: 1995-061xx. Apogee: 342 km (212 mi). Perigee: 356 km (221 mi). Inclination: 51.6000 deg. Summary: Atlantis rendezvoused and docked with Mir space station on Nov 15. After departure the Russian-built 316GK Shuttle-Mir docking module remained attached to Mir to provide easier docking capability in the future..

1997 November 12 - .
  • Death of William L Van Horn - . Nation: USA. Related Persons: Van Horn. Summary: American manager. Program Director for the Atlas Weapon System. Manager of Long Range Planning in the Atlas production program. Later Vice President and Program Director for the Atlas Weapon System..

1997 November 12 - . 17:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M 382-01.
  • Kupon - . Payload: Kupon K95K. Nation: Russia. Agency: TsBank. Manufacturer: Lavochkin. Class: Communications. Type: Civilian communications satellite. Spacecraft: Kupon. Completed Operations Date: 1998-03-01 . USAF Sat Cat: 25045 . COSPAR: 1997-070A. Apogee: 35,792 km (22,240 mi). Perigee: 35,778 km (22,231 mi). Inclination: 0.0000 deg. Period: 1,435.50 min. Geosynchronous. Kupon is the first communications satellite for the Russian banking system, and the first commercial communications satellite sold by the Lavochkin, who have in the past been more commonly associated with planetary probes and early warning satellites. Kupon, owned by the Russian Federation Central Bank (and possibly Global Information Systems of Moscow), relays financial data for the Bankir network. Positioned in geosynchronous orbit at 55 deg E in 1997-1998 As of 1 September 2001 located at 86.25 deg E drifting at 0.142 deg W per day. As of 2007 Mar 11 located at 78.29E drifting at 0.156E degrees per day.

1997 November 12 - . 21:48 GMT - . Launch Site: Kourou. Launch Complex: Kourou ELA2. LV Family: Ariane. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L-3 V102.
  • Sirius 2 - . Nation: Sweden. Agency: NSAB. Manufacturer: Cannes. Program: Sirius. Class: Communications. Type: Civilian communications satellite. Spacecraft: Spacebus 3000. USAF Sat Cat: 25049 . COSPAR: 1997-071A. Apogee: 35,791 km (22,239 mi). Perigee: 35,781 km (22,233 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Geosynchronous. Stationed over 4.8E Positioned in geosynchronous orbit at 5 deg E in 1997-1999 As of 5 September 2001 located at 4.81 deg E drifting at 0.001 deg E per day. As of 2007 Mar 8 located at 4.77E drifting at 0.004W degrees per day..
  • Cakrawarta 1 - . Payload: Indostar 1. Nation: Indonesia. Agency: Indostar. Manufacturer: McLean. Class: Communications. Type: Civilian communications satellite. Spacecraft: Star bus. USAF Sat Cat: 25050 . COSPAR: 1997-071B. Apogee: 35,812 km (22,252 mi). Perigee: 35,761 km (22,220 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Summary: Geosynchronous. Stationed over 100.6E Positioned in geosynchronous orbit at 107 deg E in 1997-1999 As of 4 September 2001 located at 107.71 deg E drifting at 0.006 deg W per day. As of 2007 Mar 11 located at 107.62E drifting at 0.005W degrees per day..

1999 November 12 - .
  • ISS Status Report: ISS 99-44 - . Nation: USA. Program: ISS. Battery cycling of the five usable storage units inside the Zarya module was completed this week as controllers prepare for the next round of deep-cycling scheduled to begin late next week. The deep cycling of each battery takes about five days. The batteries store solar energy, which then is converted into electrical power for the Station's systems. Periodically, each battery is cycled to ensure its health and maintain its life. Additional Details: ISS Status Report: ISS 99-44.

2001 November 12 - .
  • ISS Status Report: ISS 01-43 - . Nation: USA. Related Persons: Culbertson; Dezhurov; Tyurin. Program: ISS. Flight: ISS EO-3. Expedition Three Commander Frank Culbertson and Pilot Vladimir Dezhurov completed the external outfitting of the Pirs Docking Compartment on the International Space Station (ISS) this evening, conducting a 5 hour, 4 minute spacewalk outside the orbital outpost. Additional Details: ISS Status Report: ISS 01-43.

2002 November 12 - . Launch Site: Mojave. Launch Vehicle: Tier One.
  • White Knight Flight 16 - . Nation: USA. Related Persons: Binnie; Siebold. Program: X-Prize. Spacecraft: SpaceShipOne. Flight Time: 2.0 hours Pilot: Binnie Copilot: Siebold. Objectives: Continued engine, ECS and avionics evaluation. Simulated wheel brake failure landing rollout. Results: Conclusion: aircraft can be landed at MHV if a wheel brake fails. More engine irregularities at high altitude. Engines removed and sent to test cell for fuel control calibration and adjustments.

2003 November 12 - .
  • Soyuz TMA-3A (cancelled) - . Crew: Dezhurov; Kuipers; Skripochka. Nation: Russia. Related Persons: Dezhurov; Kuipers; Skripochka. Agency: RAKA. Program: ISS. Class: Manned. Type: Manned spacecraft. Flight: Soyuz TMA-3A. Spacecraft: Soyuz TMA. Soyuz TMA-3 was originally to switch lifeboats on the International Space Station. The crew would have returned to earth in the Soyuz TMA-2 already docked to the station. After the Columbia disaster, the remaining shuttles were grounded. The Soyuz was then the only means of keeping the station manned. It was therefore decided that Soyuz TMA-3 would fly with the skeleton crew of Foale and Kaleri.

2004 November 12 - .
  • International Space Station Status Report #04-61 - . Nation: USA. Related Persons: Chiao; Sharipov. Program: ISS. Flight: ISS EO-10. Summary: Expedition 10 Commander Leroy Chiao this week extended his reach beyond the confines of the pressurized compartments of the International Space Station as he and Flight Engineer Salizhan Sharipov near the one month mark in space since launch Oct. 14.. Additional Details: International Space Station Status Report #04-61.

2005 November 12 - .
  • Hayabusa releases Minerva nano-lander. - . Nation: Japan. Hayabusa probe skimmed at an altitude of 55 m over asteroid Itokawa. The Minerva nano-lander was released, but missed the asteroid and floated out into deep space. Hayabusa was then moved to a safe position 5 km from the surface and the control team considered its next move.

2005 November 12 - .
  • Hayabusa, MINERVA Landing, Failed - . Nation: Japan. Spacecraft: Hayabusa.

2005 November 12 - .
  • Death of Richard Earl Lawyer at Palmdale, California. Natural causes. - . Nation: USA. Related Persons: Lawyer. Summary: American pilot astronaut, 1965-1969..

2008 November 12 - . Launch Site: Semnan. LV Family: Seijil. Launch Vehicle: Seijil.
  • Iran RV - . Nation: Iran. Summary: Technology payload..

2008 November 12 - . 05:55 GMT - . Launch Site: Balasore. Launch Vehicle: Shourya.
2009 November 12 - . 02:45 GMT - . Launch Site: Jiuquan. LV Family: CZ. Launch Vehicle: CZ-2C.
  • SJ-11-01 - . Nation: China. Agency: SISE. Spacecraft: SJ-11. USAF Sat Cat: 36088 . COSPAR: 2009-061A. Apogee: 705 km (438 mi). Perigee: 688 km (427 mi). Inclination: 98.3000 deg. Period: 98.70 min. Summary: Experimental Satellite, believed to carry infrared surveillance system sensors..

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