Encyclopedia Astronautica
January 17


January 17 Chronology


1943 January 17 - .
1944 January 17 - . Launch Site: Heidelager. LV Family: V-2. Launch Vehicle: V-2.
1945 January 17 - . Launch Site: Peenemuende. Launch Complex: Peenemuende SK. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 20832. FAILURE: Failed 20 m above pad.
  • V-2 Ma390 V7 - . Nation: Germany. Summary: Planned range 320 km. 'Kitz' launch - listed under Heidekraut launches, but actually made from Karlshagen or railhead area of Peenemuende..

1947 January 17 - .
  • XS-1 Flight 18 - . Crew: Goodlin. Payload: XS-1 # 2 flight 8. Nation: USA. Related Persons: Goodlin. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: Bell flight 8. Buffet boundary investigation. Full-power climb. Plane reached mach 0.82..

1955 January 17 - . Launch Site: Wallops Island.
  • Rocket-towed model. - . Nation: USA. Summary: First launching of a test model towed by a rocket vehicle with a flexible towline, by Langley Laboratory's PARD at Wallops Island, Va..

1956 January 17 - . Launch Site: Hammaguira. Launch Complex: Hammaguira CB. LV Family: Monica. Launch Vehicle: Monica I. LV Configuration: Monica I I.
  • Campaign 5 to Feb 2 Test / release mission - . Nation: France. Agency: CASDN. Apogee: 40 km (24 mi).

1958 January 17 - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC3. LV Family: Polaris. Launch Vehicle: Polaris TV. LV Configuration: Polaris TV 1-204-10.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1961 January 17 - . 21:25 GMT - . Launch Site: Wallops Island. LV Family: Asp. Launch Vehicle: Nike Asp. LV Configuration: Nike Asp NASA 03.36GT.
  • Test mission - . Nation: USA. Agency: NASA. Apogee: 209 km (129 mi).

1962 January 17 - . 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 17 - . 20:00 GMT - . Launch Site: Mud Lake DZ. Launch Pad: 37.9 N x 117.1 W. Launch Platform: NB-52 003. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3-2-3.
  • X-15A MH-96. Mach 5 test - . Nation: USA. Agency: NASA; USAF. Apogee: 40 km (24 mi). Summary: Maximum Speed - 6058 kph. Maximum Altitude - 40690 m..

1962 January 17 - . 21:02 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B2. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 123D.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).

1963 January 17 - .
  • Department of Defense (DOD) and NASA management responsibilities in the Cape Canaveral area. - . Nation: USA. Related Persons: McNamara; Webb. NASA Administrator James E. Webb and Secretary of Defense Robert S. McNamara signed a new agreement on Department of Defense (DOD) and NASA management responsibilities in the Cape Canaveral area. The Air Force would continue as single manager of the Atlantic Missile Range and host agency at the 15,000-acre Cape Canaveral launch area. NASA's Launch Operations Center would manage and serve as host agency at the Merritt Island Launch Area, north and west of existing DOD installations. DOD and NASA would each be responsible for their own logistics and administration in their respective areas. Specific mission functions - e.g., preparation, checkout, launch, test evaluation - would be performed by each agency in its own behalf, regardless of location. DOD retained certain fundamental range functions, including scheduling, flight safety, search and rescue operations, and downrange airlift and station operation.

1963 January 17 - .
  • Mercury MA-10 a possibility. - . Nation: USA. Related Persons: Seamans. Program: Mercury. Flight: Mercury MA-9. Spacecraft: Mercury. Asked by a Congressional committee if NASA planned another Mercury flight after MA-9, Dr Robert C. Seamans stated, in effect, that schedules for the original Mercury program and the 1-day orbital effort were presumed to be completed in fiscal year 1963. If sufficient test data were not accumulated in the MA-9 flight, backup launch vehicles and spacecraft were available to fulfill requirements.

1963 January 17 - . 18:59 GMT - . Launch Site: Delamar Dry Lake DZ. Launch Pad: 37.3 N x 114.9 W. Launch Platform: NB-52 008. LV Family: X-15. Launch Vehicle: X-15. LV Configuration: X-15 3-14-24.
  • X-15A VO Alt, IR expt Test/Technology mission - . Nation: USA. Agency: NASA; USAF. Apogee: 82 km (50 mi). Summary: First civilian flight above 80 km. Maximum Speed - 5917 kph. Maximum Altitude - 82810 m. Second astronaut wings flight (USAF definition)..

1964 January 17 - . 05:01 GMT - . Launch Site: Wallops Island. LV Family: Javelin. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.31DA.
  • Composition / Airglow Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 925 km (574 mi).

1966 January 17 - . 16:42 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 641. LV Family: Polaris. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3P-393.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 January 17 - . 17:56 GMT - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bacchus. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C127.
  • Ionosphere mission - . Nation: France. Agency: CNES. Apogee: 124 km (77 mi).

1966 January 17 - . 22:39 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.262CM.
  • Sodium release Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 206 km (128 mi).

1967 January 17 - .
1967 January 17 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Blandine. LV Family: Veronique. Launch Vehicle: Veronique 61. LV Configuration: Veronique 61 VA85.
  • FU-145B astronomy Test / ultraviolet astronomy mission - . Nation: France. Agency: CNES. Apogee: 205 km (127 mi). Summary: FU145b X-ray and UV astronomy / Stab mission..

1967 January 17 - . Launch Site: Tonopah. LV Family: Sandhawk. Launch Vehicle: Sandhawk. LV Configuration: Sandhawk Sandia 281-3.
  • Test / aeronomy mission - . Nation: USA. Agency: Sandia. Apogee: 188 km (116 mi).

1967 January 17 - . 19:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee 150. LV Configuration: Aerobee 150 CRL AG3.526.
  • Extreme ultraviolet Mon Solar extreme ultraviolet mission - . Nation: USA. Agency: AFCRL. Apogee: 243 km (150 mi).

1968 January 17 - .
  • Afanasyev inspects the TsPK. - . Nation: USSR. Related Persons: Afanasyev, Sergei; Mishin. Program: Lunar L1; Lunar L3. Spacecraft: Soyuz 7K-L1; Soyuz 7K-LOK. He is shown the Volga and L1 trainers, takes a seat in the trainer, and is given a simulated space flight. At the air base he reviews the aircraft and the TBK-60 altitude chamber. Throughout the tour, Mishin constantly wore a soft expression and used coarse language. Afanasyev was briefed on and recognised problems with development and delivery of the Salyut digital computer needed for the L1 guidance system. But he was not told that cooperation had broken down totally on the L3 simulator development and crew selection.

1968 January 17 - . Launch Site: Vandenberg. LV Family: Delta. Launch Vehicle: Thor Agena D.
  • Final launch of a Thrust-Augmented-Thor/Agena - . Nation: USA. Summary: Final launch of a Thrust-Augmented-Thor/Agena space booster from Vandenberg (first launch on 28 February 1963)..

1968 January 17 - . 10:12 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC2W. LV Family: Delta. Launch Vehicle: Thor Agena D SLV-2A/D. LV Configuration: Thor SLV-2A Agena D 498 / Agena D 2733.
  • OPS 1965 - . Payload: Ferret 12 / Agena D 2733. Mass: 1,500 kg (3,300 lb). Nation: USA. Agency: NRO; USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Ferret. Decay Date: 1970-07-07 . USAF Sat Cat: 3097 . COSPAR: 1968-004A. Apogee: 536 km (333 mi). Perigee: 462 km (287 mi). Inclination: 75.1000 deg. Period: 94.60 min.

1968 January 17 - . 23:08 GMT - . Launch Site: Fort Churchill. LV Family: Nike. Launch Vehicle: Nike Iroquois. LV Configuration: Nike Iroquois CRL AG07.634.
  • Atmospheric / TMA Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 193 km (119 mi).

1969 January 17 - . 18:34 GMT - . Launch Site: Kiruna. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.313IM.
  • RTG SNC 2A / 1 Aeronomy mission - . Nation: Sweden. Agency: NASA; RTG. Apogee: 117 km (72 mi).

1969 January 17 - . 21:32 GMT - . Launch Site: Wallops Island. LV Family: Cajun. Launch Vehicle: Nike Cajun. LV Configuration: Nike Cajun NASA 10.306GM.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 112 km (69 mi).

1969 January 17 - .
  • Landing of Soyuz 4 - . Return Crew: Khrunov; Shatalov; Yeliseyev. Nation: USSR. Related Persons: Khrunov; Shatalov; Yeliseyev. Program: Soyuz. Flight: Soyuz 4; Soyuz 4/5. Soyuz 4 landed at 06:51 GMT 48 km south-west of Karaganda, 40 km from the planned point, with the crew of Khrunov, Shatalov and Yeliseyev aboard. Shatalov's performance has been outstanding -- all manoeuvres were made correctly with minimal expenditure of propellant. The soft landing system performed well, in temperatures of -30 deg C and in 60 to 80 cm of snow. The first recovery helicopter reached the capsule only five minutes after touchdown. 25 minutes later the crew is on a helicopter, on their way to the airfield at Karaganda. The crew is given a medical examination at the Hotel Chaika and then taken downstairs for a press conference. At 16:45 they board an An-24, bound for Tyuratam.

1970 January 17 - . Launch Site: Baikonur. Launch Complex: Baikonur LC161/35. LV Family: Tsiklon. Launch Vehicle: R-36 8K67M.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1970 January 17 - . 01:20 GMT - . Launch Site: Kagoshima. LV Family: S. Launch Vehicle: S-210. LV Configuration: S-210-3.
  • X-ray astronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 119 km (73 mi).

1970 January 17 - . 03:03 GMT - . Launch Site: Fort Churchill. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.65UE.
  • Aurora mission - . Nation: USA. Agency: NASA. Apogee: 252 km (156 mi).

1971 January 17 - . 14:48 GMT - . Launch Site: Kiruna. Launch Complex: Kiruna C. LV Family: Belier. Launch Vehicle: Centaure. LV Configuration: Centaure C37/2.
  • ESRO C37 / 2 MPE Ba Ionosphere / barium release mission - . Nation: Europe. Agency: ESRO. Apogee: 215 km (133 mi).

1971 January 17 - . 15:33 GMT - . Launch Site: Andoya. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk DLR A-NT-39.
  • MPE Barium release / Brigitte Ionosphere / fields mission - . Nation: Germany. Agency: DLR. Apogee: 328 km (203 mi).

1972 January 17 - . 10:00 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 90 km (55 mi).

1973 January 17 - . 09:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 93 km (57 mi).

1974 January 17 - .
  • Kamanin sees Comet Kohoutek. - . Nation: USSR.

1974 January 17 - . 02:37 GMT - . Launch Site: Poker Flat. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.160GE.
  • Plasma mission - . Nation: USA. Agency: NASA. Apogee: 298 km (185 mi).

1974 January 17 - . 10:07 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/2. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53753-208.
  • Cosmos 628 - . Mass: 550 kg (1,210 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Tsiklon. USAF Sat Cat: 7094 . COSPAR: 1974-001A. Apogee: 1,008 km (626 mi). Perigee: 952 km (591 mi). Inclination: 83.0000 deg. Period: 104.70 min. Summary: Military navigation satellite..

1975 January 17 - . 09:07 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. Launch Pad: LC1 or LC31. LV Family: R-7. Launch Vehicle: Voskhod 11A57.
  • Cosmos 702 - . Mass: 6,000 kg (13,200 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-2M. Duration: 12.00 days. Decay Date: 1975-01-29 . USAF Sat Cat: 7606 . COSPAR: 1975-002A. Apogee: 313 km (194 mi). Perigee: 205 km (127 mi). Inclination: 71.3000 deg. Period: 89.70 min. Summary: Area survey photo reconnaissance satellite; returned film capsule..

1975 January 17 - . 09:35 GMT - . Launch Site: Kagoshima. LV Family: Kappa. Launch Vehicle: Kappa 9M. LV Configuration: Kappa 9M K-9M-49.
  • Airglow Aeronomy / ionosphere mission - . Nation: Japan. Agency: ISAS. Apogee: 363 km (225 mi).

1975 January 17 - . 22:43 GMT - . Launch Site: Wallops Island. LV Family: Tomahawk Sandia. Launch Vehicle: Ute Tomahawk. LV Configuration: Ute Tomahawk CRL A09.301-9.
  • Aladdin 75 Sphere Aeronomy / plasma mission - . Nation: USA. Agency: USAF CRL. Apogee: 190 km (110 mi).

1976 January 17 - . 23:27 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17B. LV Family: Delta. Launch Vehicle: Delta 2914. LV Configuration: Delta 2914 606/D119.
  • CTS 1 - . Payload: Hermes. Mass: 500 kg (1,100 lb). Nation: Canada. Agency: CRCSS. Class: Communications. Type: Civilian communications satellite. Spacecraft: CTS. Completed Operations Date: 1979-12-08 . USAF Sat Cat: 8585 . COSPAR: 1976-004A. Apogee: 35,840 km (22,260 mi). Perigee: 35,704 km (22,185 mi). Inclination: 12.8000 deg. Period: 1,435.40 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Positioned in geosynchronous orbit over the Americas at 116 deg W in 1976-79; over the Pacific Ocean 142 deg W in 1979 As of 5 September 2001 located at 135.36 deg W drifting at 0.161 deg W per day. As of 2007 Mar 10 located at 131.55W drifting at 0.190W degrees per day.

1977 January 17 - . 07:30 GMT - . Launch Site: Koroni. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 85 km (52 mi).

1978 January 17 - . 03:26 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53716-327.
  • Cosmos 985 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 10599 . COSPAR: 1978-007A. Apogee: 1,015 km (630 mi). Perigee: 938 km (582 mi). Inclination: 82.9000 deg. Period: 104.60 min. Summary: Military navigation satellite..

1978 January 17 - . 20:21 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC25C. LV Family: Trident. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 C4X-13.
  • Test mission - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1979 January 17 - . 20:00 GMT - . Launch Site: White Sands. LV Family: Astrobee. Launch Vehicle: Astrobee F. LV Configuration: Astrobee F NASA 25.10AS.
  • Solar mission - . Nation: USA. Agency: NASA. Apogee: 226 km (140 mi).

1980 January 17 - . 15:24 GMT - . Launch Site: Wallops Island. Launch Vehicle: Rocketsonde. LV Configuration: AN/DMQ-9.
  • - . Nation: USA. Agency: MRN. Apogee: 90 km (55 mi).

1981 January 17 - . LV Family: Shuttle. Launch Vehicle: Shuttle.
  • Shuttle MPTA-098 625-second firing. - . Nation: USA. Summary: This firing used the three flight engines, which had been removed from Columbia..

1982 January 17 - . 14:11 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 726. LV Family: Trident. Launch Vehicle: Trident C-4.
  • DASO-9 demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1983 January 17 - . 19:48 GMT - . Launch Site: Point Mugu. Launch Vehicle: Rocketsonde.
  • Arcasonde - . Nation: USA. Agency: MRN. Apogee: 67 km (41 mi).

1984 January 17 - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K?. LV Family: SB-735. Launch Vehicle: ST-735. LV Configuration: ST-735-1 ST-735-1.
  • SRB Sep test - . Nation: Japan. Agency: ISAS. Apogee: 50 km (31 mi).

1984 January 17 - . 20:00 GMT - . Launch Site: Andoya. LV Family: Viper. Launch Vehicle: Viper 3A. LV Configuration: Viper 3A MAP/WINE.
  • M-F 26 Aeronomy mission - . Nation: Germany. Agency: DFVLR. Apogee: 116 km (72 mi).

1985 January 17 - . 15:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. Launch Pad: LC35 L-21B. LV Family: Aerobee. Launch Vehicle: Aerobee 150 MI. LV Configuration: Aerobee 150 MI-20 NASA 04.342UG.
  • JHU Airglow 14 (HUT) Airglow mission - . Nation: USA. Agency: NASA. Apogee: 169 km (105 mi).

1985 January 17 - . 17:46 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65034-138.
  • Cosmos 1624 - . Mass: 700 kg (1,540 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-2M. USAF Sat Cat: 15482 . COSPAR: 1985-006A. Apogee: 797 km (495 mi). Perigee: 777 km (482 mi). Inclination: 74.0000 deg. Period: 100.60 min. Summary: Replaced Cosmos 1570..

1986 January 17 - . 07:21 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC32. Launch Pad: LC32/pad?. LV Family: Tsiklon. Launch Vehicle: Tsiklon-3.
  • Cosmos 1726 - . Payload: Tselina-D no. 53. Mass: 2,000 kg (4,400 lb). Nation: USSR. Agency: MO. Program: Tselina. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Tselina-D. USAF Sat Cat: 16495 . COSPAR: 1986-006A. Apogee: 618 km (384 mi). Perigee: 590 km (360 mi). Inclination: 82.5000 deg. Period: 96.80 min.

1986 January 17 - . 10:20 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 331-02.
  • Raduga 18 - . Payload: Raduga s/n 29L. Mass: 1,940 kg (4,270 lb). Nation: USSR. Agency: MOM. Class: Communications. Type: Military communications satellite. Spacecraft: Raduga . Completed Operations Date: 1991-12-04 . USAF Sat Cat: 16497 . COSPAR: 1986-007A. Apogee: 36,493 km (22,675 mi). Perigee: 35,909 km (22,312 mi). Inclination: 5.8000 deg. Period: 1,457.30 min. Stationed at 335 deg. E. Provision of telephone and telegraph radiocommunications and television broadcasting. Positioned in geosynchronous orbit at 25 deg W in 1986-1989; 170 deg W in 1989-1991 As of 28 August 2001 located at 163.25 deg W drifting at 5.255 deg W per day. As of 2007 Mar 10 located at 22.49E drifting at 5.257W degrees per day.

1987 January 17 - . 17:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100B.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1989 January 17 - . 19:00 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC36. LV Family: Black Brant. Launch Vehicle: Black Brant 9. LV Configuration: Black Brant IX NASA 36.47GU.
  • Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).

1990 January 17 - .
  • NASA Astronaut Training Group 13 selected. - . Nation: USA. Related Persons: Bursch; Chiao; Clifford; Cockrell; Collins, Eileen; Currie; Gregory, William; Halsell; Harris; Helms; Jones; McArthur; Newman; Ochoa; Precourt; Searfoss; Sega; Thomas; Voss, Janice; Walz; Wilcutt; Wisoff; Wolf. The group was selected to provide pilot, engineer, and scientist astronauts for space shuttle flights.. Qualifications: Pilots: Bachelor's degree in engineering, biological science, physical science or mathematics. Advanced degree desirable. At least 1,000 flight-hours of pilot-in-command time. Flight test experience desirable. Excellent health. Vision minimum 20/50 uncorrected, correctable to 20/20 vision; maximum sitting blood pressure 140/90. Height between 163 and 193 cm.

    Mission Specialists: Bachelor's degree in engineering, biological science, physical science or mathematics and minimum three years of related experience or an advanced degree. Vision minimum 20/150 uncorrected, correctable to 20/20. Maximum sitting blood pressure of 140/90. Height between 150 and 193 cm.. Reported to the Johnson Space Center in late July 1990 to begin their year long training. Chosen from 1945 qualified applicants, then 106 finalists screened between September and November 1989.


1990 January 17 - . 14:45 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2055 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 12.00 days. Decay Date: 1990-01-29 . USAF Sat Cat: 20426 . COSPAR: 1990-003A. Apogee: 260 km (160 mi). Perigee: 248 km (154 mi). Inclination: 62.8000 deg. Period: 89.60 min. Summary: Military cartographic satellite; returned film capsule..

1991 January 17 - . 10:30 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC16/2. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 2121 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Earth. Type: Earth resources satellite. Spacecraft: Zenit-8. Duration: 24.00 days. Decay Date: 1991-02-10 . USAF Sat Cat: 21059 . COSPAR: 1991-004A. Apogee: 247 km (153 mi). Perigee: 165 km (102 mi). Inclination: 82.6000 deg. Period: 88.60 min. Summary: Military cartographic satellite; returned film capsule..

1992 January 17 - . Launch Site: White Sands. Launch Complex: White Sands SULF. Launch Vehicle: Storm. LV Configuration: Storm S1.
  • BTTV-1 Validation test - . Nation: USA. Agency: USA. Apogee: 200 km (120 mi).

1993 January 17 - .
  • EVA STS-54-1 - . Crew: Harbaugh; Runco. EVA Type: Extra-Vehicular Activity. EVA Duration: 0.18 days. Nation: USA. Related Persons: Harbaugh; Runco. Program: STS. Class: Manned. Type: Manned spaceplane. Flight: STS-54. Spacecraft: Endeavour. Summary: Tested tools and techniques for extravehicular activity..

1996 January 17 - . 05:40 GMT - .
1997 January 17 - . 01:17 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 MSLS IFT-1.
  • IFT-1 EKV Target Target mission - . Nation: USA. Agency: USAF AFMC. Apogee: 1,300 km (800 mi). Summary: Minuteman launched an MSLS target vehicle for the EKV anti-ballistic missile interceptor launched from Kwajalein Atoll..

1997 January 17 - . 16:28 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC17A. LV Family: Delta. Launch Vehicle: Delta 7925. LV Configuration: Delta 7925 D241. FAILURE: T+12 sec GEM strap-on number 2 structural failure.. Failed Stage: 0.
  • GPS 42 - . Payload: GPS 2R-1 / GPS SVN 42. Mass: 2,030 kg (4,470 lb). Nation: USA. Agency: MDSSC. Manufacturer: Valley Forge. Program: Navstar. Class: Navigation. Type: Navigation satellite. Spacecraft: GPS Block 2R. COSPAR: F970117A. Summary: Destroyed in launch vehicle failure..

2001 January 17 - . 04:31 GMT - . Launch Site: Balasore. Launch Complex: Balasore IC4. LV Family: Agni. Launch Vehicle: Agni 2.
  • Agni RV Mk 2 Research and development launch - . Nation: India. Agency: IDRDL. Apogee: 1,000 km (600 mi).

2002 January 17 - .
  • Galileo, Io 33 Flyby - . Nation: USA. Spacecraft: Galileo.

2003 January 17 - . 13:00 GMT - . Launch Site: Kiruna. LV Family: Loki. Launch Vehicle: Super Loki.
  • SAGE-3 3 Aeronomy mission - . Nation: Germany. Agency: NASA. Apogee: 112 km (69 mi).

2004 January 17 - . 15:30 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K. LV Family: S. Launch Vehicle: S-310. LV Configuration: S-310-33.
  • WAVE2004 Aeronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 141 km (87 mi).

2007 January 17 - .
2008 January 17 - .
  • ISS On-Orbit Status 01/17/08 - . Nation: USA. Related Persons: Malenchenko; Tani; Whitson. Program: ISS. Flight: ISS EO-16. CDR Whitson and FE-2 Tani started out with the daily reading of SLEEP (Sleep-Wake Actigraphy and Light Exposure during Spaceflight) experiment data accumulated during the night, for logging and filling in questionnaire entries in the SLEEP session file on the HRF-1 laptop for downlink.

    (To monitor the crewmembers' sleep/wake patterns and light exposure, Dan and Peggy wear a special Actiwatch device which measures the light levels encountered by him as well as his patterns of sleep and activity throughout the Expedition. The log entries are done within 15 minutes of final awakening for seven consecutive days, as part of the crew's discretionary 'job jar' task list.)

    Preparatory to today's pump R&R (Removal & Replacement) of the EHS VOA (Environmental Health Systems/Volatile Organic Analyzer), CDR Whitson rotated the CHeCS rack down for some AAA(Avionics Air Assembly) fan/filter and smoke detector cleaning, before FE-2 Tani performed the VOA IFM (Inflight Maintenance), with filter inspection, preceded and followed by taking CSA-O2 (Compound Specific Analyzer-Oxygen) readings in the affected rack areas. (If the O2 percentage was between 15.7% - 24.1%, Dan was Go to proceed. If not, the ground had steps to be taken to ventilate the area. Ground analysis has shown that the secondary seals in QDs (Quick Disconnects) in the Nitrogen/Oxygen systems do not always seal properly, which can result in an increased N2/O2 concentration behind panels & racks with no ventilation. The CHeCS (LAB1D4) is one of these racks.) Additional Details: ISS On-Orbit Status 01/17/08.


2008 January 17 - .
  • Death of Werner Karl Dahm - . Nation: Germany; USA. Related Persons: Dahm. Summary: German-American aerodynamicist, worked at Peenemuende on A9/A10, A7, A4b, and Wasserfall winged missiles. Post-war completed studies, joined von Braun team in US as Head of Aerodynamics Analysis Branch, Aeroballistics Division, Huntsville..

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