Encyclopedia Astronautica
January 13


January 13 Chronology


1918 January 13 - .
  • Birth of Walter Jacobi - . Nation: Germany; USA. Summary: German engineer in WW2, member of the Rocket Team in the United States thereafter..

1923 January 13 - .
  • Birth of John W Paup - . Nation: USA. Summary: American North American engineer who managed their winning Apollo proposal and was the company's Apollo program manager 1961-1964. Replaced under NASA pressure, he died in 1968 before his spacecraft made it to the moon..

1934 January 13 - .
1945 January 13 - . Launch Site: Peenemuende. Launch Complex: Peenemuende SK. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 20840.
  • V-2 Ma392 V4 - . Nation: Germany. Summary: Planned range 320 km. Launched into sea; accuracy 13.1 km to the right of the planned trajectory. Circular error 14.4 km from aim point. 'Kitz' launch - listed under Heidekraut launches, but actually made from Karlshagen or railhead area of Peenemuende..

1949 January 13 - .
  • Birth of Rakesh 'Rikki' Sharma - . Nation: India. Summary: Indian pilot cosmonaut. Flew on Salyut 7 EP-3. First Indian astronaut. Indian Air Force.

1949 January 13 - . 20:26 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC33. LV Family: Hermes. Launch Vehicle: Hermes B-1. LV Configuration: Hermes B-1 B-1 No. 1. FAILURE: Failure.
  • Hermes II test - . Nation: USA. Agency: USA. Apogee: 1.00 km (0.60 mi).

1953 January 13 - . Launch Site: White Sands. LV Family: Corporal. Launch Vehicle: Corporal. LV Configuration: Corporal 41R.
  • Test mission - . Nation: USA. Apogee: 30 km (18 mi).

1954 January 13 - . Launch Site: White Sands. LV Family: Nike. Launch Vehicle: Nike. LV Configuration: Nike 1186A.
  • Test mission - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1955 January 13 - . Launch Site: White Sands. LV Family: Nike Hercules. Launch Vehicle: Nike Hercules.
  • Test launch - . Nation: USA. Agency: USA. Apogee: 10 km (6 mi).

1956 January 13 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC1. Launch Pad: LC1/2?. LV Family: Snark. Launch Vehicle: Snark.
  • Snark Missile test. - . Nation: USA. Summary: USAF Northrop Snark launched from Cape Canaveral on 2,000-mile flight..

1959 January 13 - . Launch Site: Hammaguira. Launch Vehicle: SE.4400. LV Configuration: SE4400 F87.
  • Test mission - . Nation: France. Agency: STA. Apogee: 40 km (24 mi).

1960 January 13 - . 21:07 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC29A. LV Family: Polaris. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1X-8.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1961 January 13 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • USAF changes Dynasoar launch vehicle to Titan II - . Nation: USA. Class: Manned. Type: Manned spaceplane. Spacecraft: Dynasoar.

1961 January 13 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5. LV Configuration: R-5 V-1000 target.
  • Target mission - . Nation: USSR. Agency: OKB-30. Apogee: 300 km (180 mi).

1962 January 13 - . Launch Vehicle: Spiral 50-50.
  • VVS Military-Scientific Conference at Monino - . Nation: USSR. Spacecraft: Spiral OS. Recommendations made by Kamanin's space unit included:
    • A KLA aerospace vehicle should be developed. This could be flown in a sub-orbital version at altitudes of 60 to 150 km and as an orbital aero-spaceplane at altitudes of 1000 to 3000 km.
    • An aircraft-launcher should be developed to allow air-launch of the KLA as well as air-to-space and space-to-earth missiles
    • Navigation, reconnaissance, guidance, and environmental control systems should be developed for the KLA suitable for flights of up to 30 days duration
    To achieve this it will be necessary to conduct research and development in air-launch and landing of the KLA, and train cosmonauts in engineering, medicine, and other specialties. The IAKM and TsPK would both need improvements.

1962 January 13 - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/4. LV Family: R-16. Launch Vehicle: R-16U.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1962 January 13 - . 16:15 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.68GT.
  • Attitude control test - . Nation: USA. Agency: NASA. Apogee: 209 km (129 mi).

1962 January 13 - . 21:41 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1W. LV Family: Delta. Launch Vehicle: Thor Agena B. LV Configuration: Thor Agena B 327 / Agena B 1120. FAILURE: Failure. Failed Stage: U.
  • Discoverer 37 - . Payload: KH-3 s/n 9030. Mass: 1,150 kg (2,530 lb). Nation: USA. Agency: USAF. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: KH-3. Decay Date: 1962-01-13 . COSPAR: F620113A. Summary: KH-3. Mission failed. Last attempted flight of KH-3 series..
  • SRV 571 - . Nation: USA. Agency: USAF. Spacecraft: KH-3. COSPAR: F620113B.

1963 January 13 - . Launch Site: Cuxhaven.
  • DRG launches at Cuxhaven - . Nation: Germany. Summary: The DRG (German Rocket Society) launched three model rockets but they fell in the flats and were not recovered..

1964 January 13 - . 16:30 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 623. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2P-243. FAILURE: Failure.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 100 km (60 mi).

1964 January 13 - . 21:50 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 623. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2P-244.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1965 January 13 - .
  • OKB-1 program review - . Nation: USSR. Related Persons: Leonov; Gorbatko; Zaikin. Program: Voskhod. Flight: Voskhod 2. Spacecraft: Voskhod; Berkut. All systems development is complete, and the two boosters for Vykhod are ready. The launch of the pathfinder spacecraft with mannequins aboard will take place at the end of January, with the manned mission scheduled for March. Leonov's spacesuit is complete, but Zaikin's will not be finished until 5 February, and there will exist only the metal detail parts for Gorbatko's suit.

1965 January 13 - . 05:02 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC80/17. LV Family: Tsiklon. Launch Vehicle: R-36 8K67. FAILURE: Failure.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

1965 January 13 - . 15:49 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 KP3.9.
  • Dayglow Aeronomy mission - . Nation: USA. Agency: KPNO. Apogee: 228 km (141 mi).

1965 January 13 - . 17:12 GMT - . Launch Site: Wallops Island. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.28UI.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 1,006 km (625 mi).

1965 January 13 - . 18:51 GMT - . Launch Site: Hidden Hills DZ. Launch Pad: 36.1 N x 116.0 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3-39-62. FAILURE: Control system problems..
  • X-15A 3D,HT,Fric,BLN test - . Nation: USA. Agency: NASA; USAF. Apogee: 30 km (18 mi). Summary: Maximum Speed - 5973 kph. Maximum Altitude - 30297 m. Immediately after burnout aircraft gyrated around all 3 axes for 7 seconds..

1965 January 13 - . 23:48 GMT - . Launch Site: Wallops Island. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.111NA.
  • Airglow Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 178 km (110 mi).

1966 January 13 - . LV Family: Saturn I. Launch Vehicle: Saturn IB.
  • Land impact program for the Apollo CM Block I deleted - . Nation: USA. Program: Apollo. Spacecraft: Apollo CSM; CSM Block II. A decision made at a Program Management Review eliminated the requirement for a land impact program for the CM to support Block I flights. Post-abort CM land impact for Saturn IB launches had been eliminated from Complex 37 by changes to the sequence timers in the launch escape system abort mode. The Certification Test Specification and related Certification Test Requirements would reflect the new Block II land impact requirements.

1966 January 13 - . Launch Site: White Sands. Launch Vehicle: HIBEX. LV Configuration: HIBEX 10.
  • 10 test - . Nation: USA. Agency: USA; DARPA. Apogee: 20 km (12 mi).

1966 January 13 - . Launch Site: Kwajalein. LV Family: Nike Zeus. Launch Vehicle: Nike Zeus. LV Configuration: Nike Zeus-3.
  • Interceptor mission - . Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1967 January 13 - . 10:00 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. LV Family: Veronique. Launch Vehicle: Veronique AGI. LV Configuration: Veronique AGI AGI 63.
  • FU-160 Solar corona Solar ultraviolet mission - . Nation: France. Agency: CNES. Apogee: 123 km (76 mi). Summary: FU160 Solar corona (UV) / Ptr mission..

1968 January 13 - . Launch Site: Biscarosse. Launch Complex: Biscarosse BLB. LV Family: MSBS. Launch Vehicle: MSBS M012. LV Configuration: MSBS M012 A1.
  • A1 test - . Nation: France. Agency: DMA. Apogee: 500 km (310 mi).

1969 January 13 - .
  • Soyuz 4 launch scrubbed - . Nation: USSR. Related Persons: Mishin; Shatalov. Program: Soyuz. Flight: Soyuz 4; Soyuz 4/5. Spacecraft: Soyuz 7K-OK. The 'unlucky' Shatalov entered the spacecraft at 10:30. But the -24 deg C weather was below the limits of the booster's gyroscopes. The launch was scrubbed. The launch was made successfully the next day. Later in the day Mishin discussed the N1/L3 project with Afanasyev.

1969 January 13 - .
  • Soyuz 4/5 profile still not settled - . Nation: USSR. Program: Soyuz. Flight: Soyuz 4; Soyuz 5; Soyuz 4/5. Spacecraft: Soyuz 7K-OK. In the evening Afanasyev hosts 100 guests - the leadership of the space program - to watch the big Army-Dinamo football game. Space plans are discussed. The State Commission still needs to confirm the crews for Soyuz 4/5. The issue of automatic versus manual rendezvous is again argued. Kamanin believes this reliance on automated systems has cost the Soviet Union the moon race.

1969 January 13 - .
  • Soyuz 4 scrub - . Nation: USSR. Program: Soyuz. Flight: Soyuz 4; Soyuz 5; Soyuz 4/5. Spacecraft: Soyuz 7K-OK. The launch of the 13th Soviet cosmonaut into space aboard Soyuz 4 is scrubbed - the first launch scrub in the history of Soviet manned launch attempts. Despite -24 deg C temperatures and 8 to 10 m/s winds, the fuelling of the rocket proceeds successfully. Voice communications are lost with Shatalov whenever the television camera is turned on, but it is decided just to leave the camera off and proceed with the launch. Then at T - 9 minutes a problem is detected with the gyro platform of the rocket. It takes three hours to fix, pushing the launch back to 15:00, meaning the landing will have to be in darkness at the end of the mission. It is decided this is too risky, and the launch is cancelled. As Shatalov exits from the spacecraft, he jokes that he has set a new record: shortest space flight, and first to return to its exact point of lift-off. The engineers are concerned with the internal temperature of the SAS abort system solid rockets if left on the pad for 24 hours in these temperatures. The internal temperature of the fuel cannot go below -2 deg C at night. Any lower, the loss of specific impulse of the fuel would reduce the thrust by more than 5%, the limit established for safe operation.

1969 January 13 - . LV Family: N1. Launch Vehicle: N1.
  • N1 payload preparation and fuelling are underway. - . Nation: USSR. Program: Lunar L3. Four N1 launches are planned in 1969: The launch of 3L will be followed by 5L, 6L, and 7L in April, June, and November. But this is probably much too optimistic due to delays in delivery of critical systems needed to complete the boosters. But at least 4L, 5L, and 6L should be launched this year.

1969 January 13 - . 23:43 GMT - . Launch Site: Eglin. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AH07.673.
  • AFGL Barium release Aeronomy mission - . Nation: USA. Agency: USAF. Apogee: 220 km (130 mi).

1970 January 13 - . 05:32 GMT - . Launch Site: Tonopah. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk-12 Sandia 152-137.
  • LRL ROX-3 X-ray astronomy mission - . Nation: USA. Agency: Sandia. Apogee: 180 km (110 mi).

1970 January 13 - . 23:50 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.384UM.
  • UM Pitot 42 Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 171 km (106 mi).

1971 January 13 - . 20:10 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 2. LV Configuration: Black Brant II ADD-2-124.
  • O2 profile Aeronomy mission - . Nation: Canada. Agency: NRCC. Apogee: 146 km (90 mi).

1972 January 13 - . 20:04 GMT - . Launch Site: Andoya. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.135IE.
  • Ferdinand 29 / Electra Plasma mission - . Nation: USA. Agency: NASA. Apogee: 192 km (119 mi).

1973 January 13 - . 21:45 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 645. Launch Vehicle: Poseidon.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1974 January 13 - . 02:10 GMT - . Launch Site: White Sands. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.24UG-UP. FAILURE: Failure.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 82 km (50 mi).

1975 January 13 - . 20:50 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 87 km (54 mi).

1976 January 13 - . 13:36 GMT - . Launch Site: Ascension. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 65 km (40 mi).

1977 January 13 - . 04:22 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 5A. LV Configuration: Black Brant VA AAD-VA-45.
  • Auroral UV / infrared Aurora / ionosphere mission Aurora / ionosphere mission - . Nation: Canada. Agency: NRCC. Apogee: 152 km (94 mi).

1978 January 13 - . 15:15 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 984 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 13.00 days. Decay Date: 1978-01-26 . USAF Sat Cat: 10592 . COSPAR: 1978-006A. Apogee: 291 km (180 mi). Perigee: 206 km (128 mi). Inclination: 62.8000 deg. Period: 89.50 min. Summary: Area survey photo reconnaissance satellite; returned film capsule..

1979 January 13 - . 15:30 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1071 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MKM. Duration: 13.00 days. Decay Date: 1979-01-26 . USAF Sat Cat: 11233 . COSPAR: 1979-002A. Apogee: 339 km (210 mi). Perigee: 179 km (111 mi). Inclination: 62.8000 deg. Period: 89.70 min. Summary: High resolution photo reconnaissance satellite; returned film capsule; maneuverable..

1980 January 13 - .
  • Discovery of EETA 79001 (Mars Meteorite) - . Nation: USA.

1981 January 13 - . 20:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 89 km (55 mi).

1982 January 13 - . 18:10 GMT - . Launch Site: White Sands. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 98 km (60 mi).

1983 January 13 - . 16:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1984 January 13 - . 14:40 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1532 - . Mass: 6,600 kg (14,500 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Yantar-4K1. Duration: 44.00 days. Decay Date: 1984-02-26 . USAF Sat Cat: 14634 . COSPAR: 1984-004A. Apogee: 357 km (221 mi). Perigee: 163 km (101 mi). Inclination: 67.1000 deg. Period: 89.70 min. Summary: High resolution photo reconnaissance; returned film in two small SpK capsules during the mission and with the main capsule at completion of the mission..

1984 January 13 - . 18:57 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 19 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 120 km (70 mi).

1984 January 13 - . 19:30 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-77.
  • CIR Infrared astronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 317 km (196 mi).

1984 January 13 - . 19:31 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 20 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 117 km (72 mi).

1984 January 13 - . 20:00 GMT - . Launch Site: Andoya. LV Family: Hawk. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-123.
  • Ferdinand 68 M-T 3 Ionosphere mission - . Nation: Norway. Agency: NTNF; DLR. Apogee: 122 km (75 mi).

1984 January 13 - . 20:50 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 21 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 119 km (73 mi).

1984 January 13 - . 21:22 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 22 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 116 km (72 mi).

1984 January 13 - . 22:12 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 23 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 121 km (75 mi).

1984 January 13 - . 22:44 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 24 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 115 km (71 mi).

1986 January 13 - .
  • Stephen Synnott's Discovery of Uranus Moons Desdemona, Rosalind & Belinda - . Nation: USA.

1987 January 13 - . 20:05 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1988 January 13 - . 13:00 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 81 km (50 mi).

1989 January 13 - . 11:51 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: PRILIV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 56 km (34 mi).

1990 January 13 - . 10:10 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: PRILIV. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 58 km (36 mi).

1993 January 13 - . 01:49 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC43/3. LV Family: R-7. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
  • Molniya 1-85 - . Payload: Molniya-1T. Mass: 1,600 kg (3,500 lb). Nation: Russia. Agency: MOM. Program: Molniya. Class: Communications. Type: Military communications satellite. Spacecraft: Molniya-1T. Decay Date: 2005-11-15 . USAF Sat Cat: 22309 . COSPAR: 1993-002A. Apogee: 39,822 km (24,744 mi). Perigee: 528 km (328 mi). Inclination: 63.4000 deg. Period: 717.70 min. Summary: Operation of the long-range telephone and telegraph radio communications system, transmission of television programmes to stations in the Orbita network. Replaced Molniya 1-78..

1993 January 13 - . 13:59 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC39B. LV Family: Shuttle. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-54.
  • STS-54 - . Call Sign: Endeavour. Crew: Casper; Harbaugh; Helms; McMonagle; Runco. Payload: Endeavour F03 / TDRS 6 [IUS]. Mass: 21,156 kg (46,640 lb). Nation: USA. Related Persons: Casper; Harbaugh; Helms; McMonagle; Runco. Agency: NASA Houston. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-54. Spacecraft: Endeavour. Duration: 5.98 days. Decay Date: 1993-01-19 . USAF Sat Cat: 22313 . COSPAR: 1993-003A. Apogee: 309 km (192 mi). Perigee: 302 km (187 mi). Inclination: 28.5000 deg. Period: 90.60 min. Manned five crew. Deployed TDRSS 6. Payloads: Tracking and Data Relay Satellite (TDRS)-F/Inertial Upper Stage (IUS); Diffuse X-ray Spectrometer (DXS); Chromosome and Plant Cell Division in Space (CHROMEX); Commercial Generic Bioprocessing Apparatus (CGBA) A; Physiological and Anatomical Rodent Experiment (PARE) 02; Solid Surface Combustion Experiment (SSCE).
  • TDRS 6 - . Payload: TDRS F. Mass: 2,530 kg (5,570 lb). Nation: USA. Agency: NASA Greenbelt. Program: STS. Class: Communications. Type: Civilian communications satellite. Spacecraft: TDRS. USAF Sat Cat: 22314 . COSPAR: 1993-003B. Apogee: 35,792 km (22,240 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.7000 deg. Period: 1,436.10 min. NASA communications; deployed from STS-54 1/13/93. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). Positioned in geosynchronous orbit at 150 deg W in 1993; 138 deg W in 1993; 46 deg W in 1994-1999 As of 5 September 2001 located at 46.99 deg W drifting at 0.017 deg W per day. As of 2007 Mar 8 located at 173.51W drifting at 0.006E degrees per day.

1994 January 13 - . 02:00 GMT - . Launch Site: Ryori. LV Family: MT-135. Launch Vehicle: MT-135P. LV Configuration: MT-135P-R877.
  • Meteorological mission - . Nation: Japan. Agency: JMA. Apogee: 50 km (31 mi).

1997 January 13 - . 02:00 GMT - . Launch Site: Kagoshima. LV Family: MT-135. Launch Vehicle: MT-135. LV Configuration: MT-135-65.
  • NNP-O3 Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 55 km (34 mi).

1998 January 13 - .
1999 January 13 - .
  • ISS Status Report: ISS 99-02 - . Nation: USA. Program: ISS. Summary: International Space Station flight controllers in Houston and Moscow continued to monitor the new outpost this week as it awaits a visit by the Space Shuttle Discovery, planned for launch in May on mission STS-96.. Additional Details: ISS Status Report: ISS 99-02.

2000 January 13 - .
  • ISS Status Report: ISS 00-02 - . Nation: USA. Program: ISS. Managers continue to manage electrical power through four of six batteries inside the Zarya module, with battery number one currently in full restoration mode through Monday. Following its restoration, which is conducted on all batteries every six months to maximize charging capacity, battery one will be available for use periodically, if necessary. Additional Details: ISS Status Report: ISS 00-02.

2003 January 13 - . 00:45 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Delta 7320-10. LV Configuration: Delta 7320-10 D294.
  • ICESat - . Payload: EOS-LAM. Mass: 1,000 kg (2,200 lb). Nation: USA. Agency: NASA. Manufacturer: Ball. Class: Earth. Type: Sea satellite. Spacecraft: ICESat. Decay Date: 2010-08-30 . USAF Sat Cat: 27642 . COSPAR: 2003-002A. Apogee: 610 km (379 mi). Perigee: 593 km (368 mi). Inclination: 94.0089 deg. Period: 96.56 min. Summary: Oceanography, gravimetry, altimetry mission. Delayed from March 30, May 12, August 30, September 10, December 15 and 20, 2002; and Jan. 11 and 12, 2003..
  • CHIPSat - . Payload: CHIPSat BD 2. Mass: 85 kg (187 lb). Nation: USA. Agency: NASA. Manufacturer: SpaceDev. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: CHIPSat. USAF Sat Cat: 27643 . COSPAR: 2003-002B. Apogee: 601 km (373 mi). Perigee: 585 km (363 mi). Inclination: 94.0070 deg. Period: 96.39 min. Summary: Astrophysics mission. Delayed from March 30, May 12, August 30, September 10, December 15 and 20, 2002; and Jan. 11 and 12, 2003..

2006 January 13 - .
  • International Space Station Status Report: SS06-002 - . Nation: USA. Related Persons: Tokarev; McArthur. Program: ISS. Flight: ISS EO-12. Summary: This past week, Expedition 12 Commander Bill McArthur and Flight Engineer Valery Tokarev completed an important upgrade to the station's spacewalk preparation systems, and installed the Recharge Oxygen Orifice Bypass Assembly.. Additional Details: International Space Station Status Report: SS06-002.

2008 January 13 - .
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