| astronautix.com | Chronology - 1992 - Quarter 1 |
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- 1992 During the Year - Nation: Russia. Launch Vehicle: Burlak.
The design was studied by Germany in 1992-1994. Development estimated to cost only DM 50 million, but not proceeded with.
- 1992 During the Year - Nation: USSR.
The original Spektr design was to be armed with Oktava interceptor rockets and equipped with sensors to identify and track ballistic missile re-entry vehicles as well as discriminate decoys. In 1992, as directed by the Soviet Union's military and political leadership, all work on such projects was discontinued. The Spektr module was mothballed, then later converted into a civilian platform, partially funded by the United States.
- 1992 Jan 21 - - 15:07 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 Jan 22 - - 14:52 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC39A. Launch Vehicle: Shuttle. LV Configuration: STS-42.
Manned seven crew. Carried International Microgravity Laboratory-1. Payloads: International Microgravity Laboratory (lML)-1, getaway special (GAS) bridge with 10 getaway specials, IMAX camera, Gelation of Sols: Applied Microgravity Research (GOSAMR)-1, Investigations Into Polymer Mem-brane Processing (IPMP), Radiation Monitoring Equipment (RME)-lll, Student Experiment 81-09: Convection in Zero Gravity, Student Experiment 83-02: Capillary Rise of Liquid Through Granular Porous Media. Additional Details: STS-42. References: 1 , 2 , 5 , 6 , 7 .
- 1992 Jan 24 - - 00:14 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC43/4. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / 2BL.
Covered Oko constellation plane 6 - 119 degree longitude of ascending node. References: 1 , 2 , 5 , 6 , 100 .
- 1992 Jan 25 - - 05:16 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 s/n R15000-058.
Unmanned resupply vessel to Mir. Docked with Mir on 27 Jan 1992 09:30:43 GMT. Undocked on 13 Mar 1992 08:43:40 GMT. Destroyed in reentry on 13 Mar 1992 15:47:00 GMT. Total free-flight time 2.36 days. Total docked time 45.97 days. References: 1 , 2 , 6 , 275 .
- 1992 Jan 30 - - 22:19 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC81L. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 372-02 / 11S861 s/n 59L.
Glonass navigational satellite. Testing of components and apparatus of the Glonass global space navigation system being set up to determine the position of civil aircraft and vessels of the merchant marine and fishing fleet. References: 1 , 2 , 5 , 6 , 67 , 274 .
Glonass navigational satellite. Testing of components and apparatus of the Glonass global space navigation system being set up to determine the position of civil aircraft and vessels of the merchant marine and fishing fleet. References: 1 , 2 , 5 , 6 , 67 , 274 .
Glonass navigational satellite. Testing of components and apparatus of the Glonass global space navigation system being set up to determine the position of civil aircraft and vessels of the merchant marine and fishing fleet. References: 1 , 2 , 5 , 6 , 67 , 274 .
- 1992 Feb 5 - Nation: Russia. Launch Site: Baikonur . Launch Complex: LC45L. Launch Vehicle: Zenit-2. FAILURE: Second stage malfunction due to heating problems in main engine.
- 1992 Feb 11 - - 01:50 GMT. Nation: Japan. Launch Site: Tanegashima . Launch Complex: O. Launch Vehicle: H-1. LV Configuration: H-1(2) s/n H-24(F).
Japanese Research Satellite-1. JERS-1 (FUYO-1). To verify functions and performance of optical sensors and a Synthetic Aperture Radar and to establish an integrated system for observing the Earth's resources; to perform observations and measurements for land survey, agriculture, forest ry, fishery, environmental preservation, disaster prevention and coastal surveillance. Launch time 0150 GMT. Launching organization NASDA. The Japanese Fuyo-1 (ERS-1) satellite failed on Oct 12, 1998 after six years of operation. References: 1 , 2 , 5 , 6 .
- 1992 Feb 11 - - 00:41 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC36A. Launch Vehicle: Atlas II. LV Configuration: Atlas II (3) s/n AC-101 / Centaur II s/n 8101.
Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). Launch vehicle put payload into geosynchronous transfer orbit with GCS trajectory option. References: 1 , 2 , 5 , 6 , 278 .
- 1992 Feb 18 - - 22:04 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 65078-418.
Military navigation satellite. Positioned in plane 6 of constellation. References: 1 , 2 , 5 , 6 , 107 .
- 1992 Feb 20 - Nation: Russia.
Dismantled equipment. References: 66 .
- 1992 Feb 23 - - 22:29 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17B. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 / Delta s/n 207.
Global Positioning System. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 1 , 2 , 5 , 6 .
- 1992 Feb 26 - - 23:45 GMT. Nation: Arab States. Launch Site: Kourou . Launch Complex: ELA2. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L s/n V49.
Stationed at 31 deg E. References: 1 , 2 , 5 , 6 .
Stationed at 162 deg E. Domestic communications. Launching organization Arianespace. Launch time 2358 GMT. References: 1 , 2 , 5 , 6 .
- 1992 Mar 4 - - 04:27 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / ML.
Operation of the long-range telephone and telegraph radio-communications system and transmission of Central Television programmes. References: 1 , 2 , 5 , 6 .
- 1992 Mar 10 - - 22:33 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53778-423.
Civilian navigation satellite. Positioned in plane 11 of constellation. Tsikada type spacecraft. Determination of the position of ships of the merchant marine and fishing fleet in the world's oceans and seas as part of the Tsikada space navigation system. References: 1 , 2 , 5 , 6 , 107 .
- 1992 Mar 13 - Nation: USA. Launch Vehicle: ERIS.
Second test against a Minuteman I was considered successful enough that no further tests were planned. Further develoment of the technology was to be accomplished by the Orbital Sciences' Aries test vehicle with spectacularly poor results.
- 1992 Mar 14 - - 00:00 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC36B. Launch Vehicle: Atlas I. LV Configuration: Atlas I MPF s/n AC-72 / Centaur I s/n 5052.
Geostationary at 125 deg W. Spent boosters, spent maneuvering stages, shrouds and other non-functional objects (US Cat D). Launch vehicle put payload into geosynchronous transfer orbit with GCS trajectory option. References: 1 , 2 , 5 , 6 , 278 .
- 1992 Mar 17 - - 10:54 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U2.
Mir Expedition EO-11. Joint flight with Germany. Docked at the Kvant rear port at 12:33 GMT on March 19. The Soyuz TM-14 crew, Aleksandr Viktorenko and Aleksandr Kaleri, returned to Earth together with French astronaut Michel Tognini. The Soyuz TM-14 undocked from Mir at 21:47 GMT on Aug 9, and landed in Kazakhstan at 01:07 GMT on August 10. References: 1 , 2 , 6 , 51 .
- 1992 Mar 24 - - 13:14 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 .
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