| astronautix.com | Chronology - 1992 - Quarter 4 |
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- 1992 Oct 6 - - 06:28 GMT. Nation: China. Launch Site: Jiuquan . Launch Complex: LA2. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C s/n CZ2C-13.
Fanhui Shi Weixing; remote sensing, microgravity experiments; capsule recovered 10/13/92. Second stage of a two stage rocket. Aug 9 launch: designation 03. Oct 6 launch: designation 04. References: 1 , 2 , 5 , 6 .
Ionospheric, auroral, amgnetospheric studies. Freja is a Swedish/German satellite designed for research into the aurora. The satellite was launched piggyback on a Long March 2C (CZ-2C) rocket and weighs 214 kg in orbit. It is a sun-pointing spinner (10 rpm) with a 2.2 m diameter. It will make high re solution measurements in the upper ionosphere and lower magnetosphere. Data will be received at Esrange, Kiruna, Sweden and at the Prince Albert Satellite Station in Canada's Saskatchewan Province. Launch time 0620 UT. References: 1 , 2 , 5 , 6 .
- 1992 Oct 8 - - 19:12 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC43/4. Launch Vehicle: Soyuz 11A511U.
250 orbits. Microgravity research. Space materials research (conducted jointly with Germany). References: 1 , 2 , 6 , 69 .
- 1992 Oct 12 - - 09:47 GMT. Nation: Germany. Launch Site: Cape Canaveral . Launch Complex: LC17B. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 / Delta s/n 215.
Stationed at 33.5 deg E. Communication satellite. Longitude 33.5 deg E. Delta II flight no 212. References: 1 , 2 , 5 , 6 .
- 1992 Oct 14 - - 20:09 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC43/3. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / ML.
Operation of the long-range telephone and telegraph radio communications system, transmission of television programmes to stations in the Orbita network and international cooperation. References: 1 , 2 , 5 , 6 .
- 1992 Oct 16 - Nation: USA. Launch Vehicle: Castor/Orbus. FAILURE: Failure.
- 1992 Oct 20 - - 12:57 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC32. Launch Vehicle: Tsyklon 3.
Six satellites launched by a single carrier rocket. References: 1 , 2 , 5 , 6 , 105 .
- 1992 Oct 21 - - 10:33 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC16/2. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / 2BL.
Covered Oko constellation plane 8 - 201 degree longitude of ascending node. References: 1 , 2 , 5 , 6 , 100 .
- 1992 Oct 22 - - 17:16 GMT. Nation: Canada. Launch Site: Cape Canaveral . Launch Complex: LC39B. Launch Vehicle: Shuttle. LV Configuration: STS-52.
Canadian Target Assembly; deployed from STS-52 10/22/92. References: 1 , 2 , 5 , 6 .
60 cm diameter sphere with laser reflectors; deployed from STS-52 10/23/92. References: 1 , 2 , 5 , 6 .
- 1992 Oct 22 - Nation: USA. Launch Vehicle: Aries. FAILURE: Failure.
- 1992 Oct 22 - - 17:16 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC39B. Launch Vehicle: Shuttle. LV Configuration: STS-52.
Deployed Lageos 2, CTA. Payloads: Laser Geodynamic Satellite (LAGEOS) II/ Italian Research Interim Stage (IRIS), Canadian Experiments (CANEX) 2, United States Micro-gravity Payload (USMP) 1, Attitude Sensor Pack-age (ASP), Tank Pressure Control Experiment (TPCE), Physiological Systems Experiment (PSE), Heat Pipe Performance (HPP) experiment, Commercial Protein Crystal Growth (CPCG), Shuttle Plume Impingement Experiment (SPIE), Commercial Materials ITA Experiment (CMIX), Crystals by Vapor Transport Experiment (CVTE). Additional Details: STS-52. References: 1 , 2 , 5 , 6 , 7 .
General Electric received the $ 398 million contract to develop the satellite, including Hughes' $ 120 million infrared thematic mapper.
- 1992 Oct 27 - - 21:50 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC31. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 s/n 15000-061.
Deployed from MIR on 11/20/92. Launched from Mir airlock. Conduct of experiments to study physical processes in the Earth's ionosphere. Small satellite launched from the Mir station. References: 1 , 2 , 6 .
Unmanned resupply vessel to Mir. Docked with Mir on 29 Oct 1992 19:05:51 GMT. Undocked on 4 Feb 1993 00:44:53 GMT. After completion of the Znamya and autonomous operation experiments, destroyed in reentry on 7 Feb 1993 06:43:20 GMT. Total free-flight time 5.32 days. Total docked time 97.24 days. References: 1 , 2 , 6 , 275 .
Reflector mirror, deployed from Progress M-15 after separation from Mir space station. References: 279 .
- 1992 Oct 28 - - 00:15 GMT. Nation: USA. Launch Site: Kourou . Launch Complex: ELA2. Launch Vehicle: Ariane 42P. LV Configuration: Ariane 42P+ s/n V54.
Geostationary at 91 deg W. The Galaxy 7 satellite failed on November 22, 2000, the third such satellite to fall victim to a design flaw in the on-board computers. References: 1 , 2 , 5 , 6 .
- 1992 Oct 29 - - 10:33 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 65078-424.
Military navigation satellite. Positioned in plane 3 of constellation. References: 1 , 2 , 5 , 6 , 107 .
- 1992 Oct 30 - - 14:59 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC81L. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 372-01 / 11S861 s/n 58L.
Transmission of television programmes to a network of multiple user receiving stations. References: 1 , 2 , 5 , 6 , 67 , 274 .
- 1992 November - Nation: USSR.
Further financial difficulties in Russia and uncertainties with America's Freedom space station led Russia and the European Space Agency to open discussions on joint development and use of Mir-2.
- 1992 Nov 16 - - 21:50 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC16/2. Launch Vehicle: Soyuz 11A511U.
Carried descent module with greetings to American people. Delivery of a humanitarian cargo (messages to the American people, promotional materials of Russian and foreign firms, etc.) to the United States of America in connection with the 500th anniversary of the discovery of America by Columbus. References: 1 , 2 , 6 .
- 1992 Nov 17 - - 07:55 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC45L. Launch Vehicle: Zenit-2.
- 1992 Nov 20 - - 15:36 GMT. Nation: Russia. 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 .
- 1992 Nov 21 - - 13:40 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC5. Launch Vehicle: Scout G. LV Configuration: Scout G-1 s/n S210C.
BMDO technology demonstration; Miniature Seeker Technology Demonstration. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 1 , 2 , 5 , 6 .
- 1992 Nov 21 - - 23:45 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17A. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 / Delta s/n 216.
Global Positioning System. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
- 1992 Nov 24 - - 04:19 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC32. Launch Vehicle: Tsyklon 3.
Investigation of outer space. References: 1 , 2 , 5 , 6 .
- 1992 Nov 24 - Nation: USSR.
With abandonment of the Buran shuttle and 37K modules, the Mir-2 design was cut back again. Mir-2 returned to its original planned 65 degree orbit, and would be assembled and flown separately from Mir. It would now consist of the DOS-8 core module, and a cross beam called the NEP (scientific-energy platform). This was equipped with equipment already proven on Mir: MSB retractable solar panels, Sfora thruster packages, small scientific packages as demonstrated on Kvant.The add-on modules now used the Progress-M service module as a tug, and were reduced in size for launch by either the Soyuz or Zenit launch vehicles.
- 1992 Nov 25 - - 11:02 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC43/3. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / 2BL.
Covered Oko constellation plane 1 - 270 degree longitude of ascending node. References: 1 , 2 , 5 , 6 , 100 .
- 1992 Nov 27 - - 13:10 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC81L. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 364-01 / 11S861 s/n 65L.
Stationed at 53 deg E. Development of the communications and television broadcasting system. References: 1 , 2 , 5 , 6 , 67 , 111 , 274 .
- 1992 Nov 28 - - 21:34 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC4E. Launch Vehicle: Titan 4. LV Configuration: Titan 404A s/n K-3 (45J-1).
Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
- 1992 Dec 1 - - 22:48 GMT. Nation: Japan. Launch Site: Kourou . Launch Complex: ELA2. Launch Vehicle: Ariane 42P. LV Configuration: Ariane 42P+ s/n V55.
Stationed at 158 deg E. Domestic communications. Launching states: Japan and France. Launch time 2248 GMT. References: 1 , 2 , 5 , 6 .
- 1992 December - Nation: USA. Launch Vehicle: SHARP.
SHARP began operation and demonstrated velocities of 3 km/sec with 5 kg projectiles. However the $ 1 billion funding to elevate the tube and begin space launch tests of smaller projectiles at speeds of up to 7 km/sec was not forthcoming. By 1996 the gun was relegated to occasional test of sub-scale Mach 9 scramjet models.
- 1992 Dec 2 - - 01:57 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC43/3. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / ML.
Operation of the long-range telephone and telegraph radio communications system, transmission of television programmes to stations in the Orbita network and international cooperation. References: 1 , 2 , 5 , 6 .
- 1992 Dec 2 - - 13:24 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC39A. Launch Vehicle: Shuttle. LV Configuration: STS-53.
Manned five crew. Deployed classified military satellite USA 89. The ODERACS payload was unable to be deployed because of payload equipment malfunction. Payloads: Department of Defense (DOD)1; Glow Experiment/Cryogenic Heat Pipe Experiment Payload (GCP); Orbital Debris Radar Calibration System (ODERACS); Battlefield Laser Acquisition Sensor Test (BLAST); Cloud Logic To Optimize Use of Defense Systems (CLOUDS) 1A; Cosmic Radiation Effects and Activation Monitor (CREAM); Fluid Acquisition and Resupply Equipment (FARE); Hand-held, Earth-oriented, Real-time, Cooperative, User-friendly, Location-targeting and Environmental System (HER-CULES); Microencapsulation in Space (MIS)-1; Radiation Monitoring Equipment (RME) III; Spare Tissue Loss (STL); Visual Function Tester (VFT)2. Additional Details: STS-53. References: 1 , 2 , 5 , 6 , 7 .
Deployed from STS-53 12/2/92. References: 1 , 2 , 5 , 6 .
- 1992 Dec 9 - - 11:16 GMT. Nation: Russia. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U2.
Photo/digital surveillance. References: 1 , 2 , 6 .
- 1992 Dec 17 - - 12:45 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC200L. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 357-02 / 11S861 s/n 64L.
Geosynchronous ballistic missile early warning satellite. Stationed at 12 deg E. Declared purpose: 'Investigation of outer space and of processes occurring in the Earth's atmosphere. Prognoz series'. References: 1 , 2 , 5 , 6 , 67 , 107 , 274 .
- 1992 Dec 18 - Nation: USSR. Launch Vehicle: VKS-DM.
Subscale proof-of-concept vehicle for Gerakl / Molniya-1000 catamaran subsonic 900 tonne aircraft design that would be used for VKS-DM spaceplane.
- 1992 Dec 18 - - 22:16 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17B. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 / Delta s/n 217.
Global Positioning System. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
- 1992 Dec 21 - - 11:21 GMT. Nation: Australia. Launch Site: Xichang . Launch Complex: LC2. Launch Vehicle: CZ-2E. LV Configuration: Chang Zheng 2E s/n CZ2E-3. FAILURE: Shortcomings in the guidance system lead to the vehicle not anticipating the true effects of hoizontal wind-shear once the mountains surrounding the launch site were cleared. This caused the nose fairing to collapse 45 seconds after launch.
Despite collapse of the nose fairing and near-desctruction of the payload, the launch vehicle continued on to place the wreckage of Optus-B2, and the Star-63F Kick-Motor into low earth orbit. References: 1 , 2 , 5 , 6 .
- 1992 Dec 22 - - 12:00 GMT. Nation: Russia. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U2.
Long duration film return military reconnaissance satellite. After returning multiple film capsules, the spacecraft was deorbited. References: 1 , 2 , 6 , 102 , 106 .
- 1992 Dec 22 - - 12:14 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC32. Launch Vehicle: Tsyklon 3.
Investigation of outer space. References: 1 , 2 , 5 , 6 , 114 .
- 1992 Dec 25 - - 07:12 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC45L. Launch Vehicle: Zenit-2.
- 1992 Dec 25 - - 20:09 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC32. Launch Vehicle: Tsyklon 3.
Investigation of outer space. References: 1 , 2 , 5 , 6 .
- 1992 Dec 29 - - 13:40 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC43/3. Launch Vehicle: Soyuz 11A511U.
Biological research; carried monkeys Ivasha and Krosha. International study of the adaptation of living organisms to conditions of space flight. After 12 days in Earth orbit, the capsule was recovered 50 deg 46 min N, 73 deg 08 min E, about 100 kilometers north of the city of Karaganda. The Cosmos 2229 mission was also referred to as Bion 10, because it was the tenth in a series of Soviet/Russian unmanned satellites carrying biological experiments. Additional Details: Cosmos 2229. References: 1 , 2 , 6 , 104 , 297 .
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