February 10

See also Born on this Day
On this day in:

1943 -

  • BI-1 Flight 3 Nation: USSR. Payload: BI-1 # 2 flight 2. Class: Manned. Type: Rocketplane. Spacecraft: BI-1. Crew: Gruzdev.

    Maximum Speed - 675 kph. Maximum Altitude - 2190 m. Date estimated.

1953 - 21:09 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Vehicle: Aerobee. Model: Aerobee RTV-N-10. LV Configuration: Aerobee RTV-N-10 NRL 12.
  • Aerobee Aeronomy/Chemical release mission Nation: USA. Agency: NRL. Apogee: 137 km (85 mi).

    Composition, cosmic radiation research. Launched at 1409 local time. Reached 137 km.

1954 - Launch Vehicle: Atlas A.
  • Teapot Report Nation: USA.

    The ICBM design feasible, as was acceleration of the program; Rand Corporation Report: Atlas ICBM could be operational by 1960-62 and should have crash project status

1958 -
  • Expanded NACA program of space flight research proposed Nation: USA. Program: Apollo.

    A greatly expanded NACA program of space flight research was proposed in a paper, "A Program for Expansion of NACA Research in Space Flight Technology," written principally by senior engineers of the Lewis Aeronautical Laboratory under the leadership of Abe Silverstein. The goal of the program would be "to provide basic research in support of the development of manned satellites and the travel of man to the moon and nearby planets." The cost of the program was estimated at $241 million per year above the current NACA budget.

1959 -
  • Wiind tunnel tests of Project Mercury configuration models were started. Nation: USA. Program: Mercury. Spacecraft: Mercury.

    By the end of the year, over 70 different models had been tested by facilities at the Air Force's Arnold Engineering Development Center and the NASA Langley, Ames, and Lewis Research Centers.

1960 - Launch Site: Cape Canaveral. Launch Complex: LC29. Launch Pad: LC29A. Launch Vehicle: Polaris A1. LV Configuration: Polaris A1 A1X-11.
  • Polaris A1 Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).

1961 -
  • Voice message sent by way of the moon Nation: USA. Program: Apollo.

    A voice message was sent from Washington, D.C., to Woomera, Australia, by way of the moon. NASA Deputy Administrator Hugh L. Dryden spoke by telephone to Goldstone, Calif., which "bounced" it to the deep-space instrumentation station at Woomera. The operation was conducted as part of the official opening ceremony of the Australian facility.

1961 - Launch Vehicle: Saturn V.
  • First static test of prototype F-1 thrust chamber Nation: USA. Program: Apollo.

    Rocketdyne Division's first static test of a prototype thrust chamber for the F-1 engine achieved a thrust of 1.550 million pounds in a few seconds at Edwards Air Force Base, Calif.

1961 -
  • Air Force interest in spacecraft similar to the Apollo Nation: USA. Program: Lunex.

    At the first meeting of the House Committee on Science and Astronautics, during the first session of the 87th Congress, Charles F. Ducander, Executive Director and Chief Counsel of the Committee staff, outlined a number of proposed subjects for study. One subject was the Air Force's interest in a three-man spacecraft similar to the Apollo spacecraft planned by NASA. A Committee staff member had been assigned to investigate this duplication of effort. On February 22, testifying before the Committee, Air Force Undersecretary Joseph V. Charyk stated that the Dyna-Soar program was a direct approach to manned military space applications. The Air Force interest in an Apollo-type spacecraft was part of the post-Dyna-Soar program, Charyk said.

1961 - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Vehicle: Titan 1. Model: Titan I. LV Configuration: Titan I AJ-11.
  • Titan 1 Mk 4 re-entry vehicle test mission Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi).

1962 -
  • Sever spacecraft trials Nation: USSR. Spacecraft: Sever.

    Two officers start a 15 day test aboard a mock-up of the Sever spacecraft, but without the participation of the IAKM. The whole thing was planned by Voronin's OKB in GKNII.

1964 - Launch Vehicle: Little Joe II.
  • Grumman to stop all work on the Apollo LEM Little Joe II program Nation: USA. Program: Apollo. Spacecraft: Apollo LM.

    MSC directed Grumman to stop all work on the LEM Little Joe II program. This action followed the ASPO Manager's decision against a testing program for the LEM comparable to that for the CSM.

1964 -
  • Death of Eugen Saenger Nation: Germany.

    Saenger dies of a heart attack in Berlin while lecturing to his students at the Technical University in Berlin

1964 - Launch Site: Green River. Launch Complex: Pad 2. Launch Vehicle: Athena. LV Configuration: Athena A001. FAILURE: Failure.
  • Athena USAF A001 re-entry vehicle test flight Nation: USA. Agency: USAF.

    This was the first of several hundred launches from Green River, Utah, to impact points in the US Army's White Sands Missile Range in New Mexico. The Athena was designed to simulate the re-entry environment of an intercontinental ballistic missile and was one of the few examples of sustained interstate missile tests within the United States.

1964 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Vehicle: Dragon. LV Configuration: Dragon D-07.
  • Dragon Test mission Nation: France. Agency: CNES. Apogee: 470 km (290 mi).

1965 - Launch Vehicle: N1.
  • L3 single-launch spacecraft draft project approved. Nation: USSR. Program: Lunar L3. Spacecraft: LK, Soyuz 7K-LOK.

    Interdepartmental Scientific-Technical Council on Space Research (MNTS-KI) Decree 'On approval of the L3 draft project' was issued. The decree followed a review by a Keldysh-led Academy of Sciences state commission the previous December. The decree moved the first flight of the N1 to the end of 1966. - Additional details.

1966 - Launch Vehicle: Titan 2.
  • Gemini launch vehicle 8 and spacecraft 8 were electrically mated; the Electrical Interface Integrated Validation and Joint Guidance and Control Test was completed February 14. Nation: USA. Flight: Gemini 8.

    After data from this test were reviewed (February 15), the Joint Combined Systems Test was run February 16.

1966 -
  • State Commission Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3, Voskhod 4, Voskhod 5.

    The commission, chaired by Tyulin, with attendance by Mishin, Tsybin, Shabarov, Kerimov, and others considers manned flight plans for 1966. The 20-day dog flight of Voskhod s/n 5 is expected to launch on 22-23 February. Kamanin notes that although he is not against the flight, it has no interest to the military. Launch of Voskhod 3 is set for 20-23 March. Kamanin names his crews for the flight - Volynov/Shonin and Beregovoi/Shatalov as back-ups. Only Pravetskiy objects to these selections, pushing Katys for the prime crew. This settled, Mishin announces he still intends to pursue the artificial gravity experiment on the flights of Voskhod s/n 7 and/or 8. Kamanin informs Mishin that he has requested for more than a year that this experiment be moved to a Soyuz flight - there are 700 kg of new military scientific equipment that has to be flown aboard Voskhod, leaving little room for nothing else.

    It is decided that the flights of Voskhod s/n 5 and 6 will be run from Moscow rather than from the cosmodrome. The state commission will return to Moscow immediately after launch for this purpose. Four groups of staff will follow the flight on four-hour shifts.

    Tyulin, Keldysh, and Mishin want engineer and scientist cosmonauts to be trained for early Soyuz flights. Kamanin agrees, telling them he will submit suitable candidates. The meeting goes well, possibly since in the absence of Korolev the commission is stacked with military representatives - of 17 members, 9 are military.

1966 - 00:55 GMT - Launch Site: Wallops Island. Launch Complex: LA3. Launch Pad: LA3A. Launch Vehicle: Scout X-4. Model: Scout X-4A. LV Configuration: Scout X-4A S141C.
  • Reentry 4B Nation: USA. Class: Technology. Type: RV. Agency: NASA. Apogee: 175 km (108 mi). Decay Date: 1966-02-09.

1966 - 05:42 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.188GE.
  • Nike Apache Plasma mission Nation: USA. Agency: NASA. Apogee: 178 km (110 mi).

1966 - 07:09 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.187GM.
  • Nike-Cajun Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi).

1966 - 07:48 GMT - Launch Site: Wallops Island. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.148GM.
  • Nike-Cajun Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi).

1966 - 08:52 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: LC31. Launch Vehicle: Vostok 8A92. Model: Vostok 8A92.
  • Cosmos 107 Nation: USSR. Payload: Zenit-2 11F61 s/n 34. Mass: 4,720 kg (10,400 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: MOM. Perigee: 216 km (134 mi). Apogee: 313 km (194 mi). Inclination: 65.00 deg. Period: 89.70 min. COSPAR: 1966-010A. USAF Sat Cat: 1998. Duration: 8.00 days. Decay Date: 1966-02-18.

    Area survey photo reconnaissance satellite.

1966 - 09:48 GMT - Launch Site: Vandenberg. Launch Complex: ABRES. Launch Pad: ABRESA1. Launch Vehicle: Atlas D. LV Configuration: Atlas D 305D.
  • Atlas D NTMP KX-38 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,800 km (1,100 mi).

1966 - 18:00 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.145GM.
  • Nike-Cajun Aeronomy mission Nation: USA. Agency: NASA. Apogee: 122 km (75 mi).

1966 - 18:41 GMT - Launch Site: Wallops Island. Launch Vehicle: Nike-Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.149GM.
  • Nike-Cajun Aeronomy mission Nation: USA. Agency: NASA. Apogee: 114 km (70 mi).

1967 - Launch Vehicle: Saturn V.
  • Apollo S-IVB stage explosion accident cause Nation: USA. Program: Apollo.

    The Board of Inquiry into the January 20 S-IVB-503 explosion at the Douglas Sacramento Test Facility identified the probable cause as the failure of a pressure vessel made with titanium-alloy parent-metal fusion welded with commercially pure titanium. The combination, which was in violation of specifications, formed a titanium hydride intermetallic that induced embrittling in the weld nugget, thus significantly degrading the capabilities of a weldment to withstand sustained pressure loads. The Board recommended pressure limitations for titanium-alloy pressure vessels.

1968 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2307.
  • Minuteman 2 Research and technology/modification Test mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1969 -
  • Soyuz plans Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz s/n 15+16, Soyuz s/n 14, Soyuz 6, Soyuz 7, Soyuz 8.

    Meeting with TsKBEM Deputy Chief Designer Tregub on manned space flight plans. Soyuz s/n 14 is set for a solo seven day mission in April-May. 15 and 16 with 5 cosmonauts aboard will fly a 7 day mission in August-September, remaining docked for three days. Soyuz s/n 17 through 20 will not fly until after May 1970 - there are no definite plans for them at this time. - Additional details.

1970 - Launch Site: Fort Churchill. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.442UI.
  • Nike Apache Ionosphere mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1970 - 05:25 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.16UE.
  • Nike Tomahawk Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1970 - 12:00 GMT - Launch Site: Plesetsk. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57.
  • Cosmos 323 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4. Agency: MOM. Perigee: 201 km (124 mi). Apogee: 314 km (195 mi). Inclination: 65.40 deg. Period: 89.70 min. COSPAR: 1970-010A. USAF Sat Cat: 4328. Duration: 8.00 days. Decay Date: 1970-02-18.

    High resolution photo reconnaissance satellite; returned film capsule

1970 - 14:10 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC S72. FAILURE: Failure.
  • Skylark ESRO S72 Ultraviolet Astronomy mission Nation: UK. Agency: BAC/ESRO. Apogee: 244 km (151 mi).

1972 - 17:02 GMT - Launch Site: Wallops Island. Launch Vehicle: Javelin. LV Configuration: Javelin NASA 8.60AE.
  • Javelin Plasma mission Nation: USA. Agency: NASA. Apogee: 851 km (528 mi).

1974 - 1975 - 05:28 GMT - Launch Site: Fort Churchill. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.536UA.
  • Nike Apache Aeronomy mission Nation: USA. Agency: NASA. Apogee: 142 km (88 mi).

1975 -
  • Landing of Soyuz 17 Nation: USSR. Program: Salyut. Flight: Soyuz 17.

    Soyuz 17 landed at 11:03 GMT, 110 km NE of Tselinograd.

1976 - 07:00 GMT - Launch Vehicle: MMR-06. LV Configuration: MMR-06 MMR-06.
  • MMR-06 Aeronomy mission Nation: USSR. Apogee: 57 km (35 mi).

1977 -
  • Midfuselage on dock, Palmdale, Columbia (OV-102) Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Columbia.

1977 - 00:22 GMT - Launch Site: Syowa Base. Launch Vehicle: S-310. LV Configuration: S-310 S-310JA-2.
  • S-310 Aeronomy mission? Nation: Japan. Agency: NIPR. Apogee: 212 km (131 mi).

1977 - 03:15 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12.
  • MR-12 Aeronomy/Ionosphere/Plasma mission Nation: USSR. Apogee: 152 km (94 mi).

1978 -
  • Complete final assembly, STA-099, Palmdale Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Challenger.

1978 - 05:30 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Vehicle: Black Brant. Model: Black Brant VB. LV Configuration: Black Brant VB NASA 21.56UG.
  • Black Brant WOT 2 Astronomy mission Nation: USA. Agency: NASA. Apogee: 238 km (147 mi).

1983 - 07:15 GMT - Launch Site: Plesetsk. Launch Complex: LC41. Launch Pad: LC41/1. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
  • Cosmos 1440 Nation: USSR. Program: Resurs. Mass: 6,300 kg (13,800 lb). Class: Earth. Type: Landsat. Spacecraft: Resurs F1-17F41. Agency: MOM. Perigee: 208 km (129 mi). Apogee: 272 km (169 mi). Inclination: 82.40 deg. Period: 89.30 min. COSPAR: 1983-009A. USAF Sat Cat: 13793. Duration: 14.00 days. Decay Date: 1983-02-24.

    High resolution photo surveillance; film capsule; maneuverable; also performed earth resources tasks. Investigation of the natural resources of the earth in the interests of various branches of the national economy of the USSR and international cooperation.

1984 - 02:40 GMT - Launch Site: Andoya. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR A-NO-126.
  • Nike Orion Ferdinand 69 M-T 6 Ionosphere mission Nation: Norway. Agency: NTNF/DLR. Apogee: 117 km (72 mi).

1984 - 03:05 GMT - Launch Site: Andoya. Launch Vehicle: Nike Orion.
  • Nike Orion Ferdinand 72 M-M 2 Aeronomy mission Nation: Norway. Agency: NTNF. Apogee: 115 km (71 mi).

1984 - 03:44 GMT - Launch Site: Andoya. Launch Vehicle: Viper. LV Configuration: Viper 3A MAP/WINE.
  • Viper M-F 44 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 109 km (67 mi).

1984 - 04:12 GMT - Launch Site: Kiruna. Launch Complex: S. Launch Vehicle: Skylark. Model: Skylark 6. LV Configuration: Skylark 6 DLR K-GR-130.
  • Skylark MAP/WINE M-I 1 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 180 km (110 mi).

1984 - 05:29 GMT - Launch Site: Andoya. Launch Vehicle: Viper. LV Configuration: Viper 3A MAP/WINE.
  • Viper M-F 45 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 114 km (70 mi).

1984 - 20:00 GMT - Launch Site: Andoya. Launch Vehicle: Viper. LV Configuration: Viper 3A MAP/WINE.
  • Viper M-F 46 Aeronomy mission Nation: Germany. Agency: DFVLR. Apogee: 111 km (68 mi).

1985 - 02:11 GMT - Launch Site: Sonde Stromfjord. Launch Vehicle: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.15UE.
  • Terrier Malemute ARCS 3 Plasma mission Nation: USA. Agency: NASA. Apogee: 406 km (252 mi).

1985 - 02:13 GMT - Launch Site: Sonde Stromfjord. Launch Vehicle: Black Brant. Model: Black Brant X. LV Configuration: Black Brant X NASA 35.012UE.
  • Black Brant TOPAZ I Plasma mission Nation: USA. Agency: NASA. Apogee: 816 km (507 mi).

1986 - Launch Site: Biscarosse. Launch Complex: BLB. Launch Vehicle: SSBS. LV Configuration: SSBS S3 2607.
  • SSBS Operational test mission Nation: France. Agency: DMA. Apogee: 1,000 km (600 mi).

1989 - 08:53 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1. Launch Vehicle: Soyuz 11A511U2. Model: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 Ye15000-032.
  • Progress 40 Nation: USSR. Program: Mir. Payload: Progress s/n 148. Mass: 7,022 kg (15,480 lb). Class: Manned. Type: Logistics. Spacecraft: Progress. Agency: MOM. Perigee: 187 km (116 mi). Apogee: 244 km (151 mi). Inclination: 51.60 deg. Period: 88.80 min. COSPAR: 1989-008A. USAF Sat Cat: 19783. Duration: 22.71 days. Completed Operations Date: 1989-03-05 01:59:08. Decay Date: 1989-03-05 01:59:08. Flight: Mir EO-4, Mir LD-2.

    Unmanned resupply vessel to Mir. Conducted third test of Buran ejection seat during ascent to orbit. The K-36M.11F35 seat was installed in an 'experimental droppable compartment' installed in place of the Launch Escape Tower engine on top of the shroud. Docked with Mir on 12 Feb 1989 10:29:38 GMT. Undocked on 3 Mar 1989 01:45:52 GMT. Unfurled experimental space mirror petal structure on undocking. Destroyed in reentry on 5 Mar 1989 01:59:00 GMT. Total free-flight time 4.08 days. Total docked time 18.64 days.

1989 - 15:13 GMT - Launch Site: Plesetsk. Launch Complex: LC32. Launch Pad: LC32. Launch Vehicle: Tsyklon 3. Model: Tsiklon-3.
  • Cosmos 1994 Nation: USSR. Program: Strela. Payload: Strela-3 no. 29. Mass: 220 kg (480 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-3. Agency: MO SSSR. Perigee: 1,394 km (866 mi). Apogee: 1,418 km (881 mi). Inclination: 82.60 deg. Period: 113.90 min. COSPAR: 1989-009A. USAF Sat Cat: 19785.

    Military store-dump communications satellite. Six satellites launched by a single carrier rocket.

  • Cosmos 1995 Nation: USSR. Program: Strela. Payload: Strela-3 no. 30. Mass: 220 kg (480 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-3. Agency: MO SSSR. Perigee: 1,411 km (876 mi). Apogee: 1,418 km (881 mi). Inclination: 82.60 deg. Period: 114.10 min. COSPAR: 1989-009B. USAF Sat Cat: 19786.

  • Cosmos 1996 Nation: USSR. Program: Strela. Payload: Strela-3 no. 31. Mass: 220 kg (480 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-3. Agency: MO SSSR. Perigee: 1,405 km (873 mi). Apogee: 1,413 km (877 mi). Inclination: 82.60 deg. Period: 114.00 min. COSPAR: 1989-009C. USAF Sat Cat: 19787.

  • Cosmos 1997 Nation: USSR. Program: Strela. Payload: Strela-3 no. 32. Mass: 220 kg (480 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-3. Agency: MO SSSR. Perigee: 1,399 km (869 mi). Apogee: 1,418 km (881 mi). Inclination: 82.60 deg. Period: 114.00 min. COSPAR: 1989-009D. USAF Sat Cat: 19788.

  • Cosmos 1998 Nation: USSR. Program: Strela. Payload: Strela-3 no. 33. Mass: 220 kg (480 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-3. Agency: MO SSSR. Perigee: 1,389 km (863 mi). Apogee: 1,413 km (877 mi). Inclination: 82.60 deg. Period: 113.80 min. COSPAR: 1989-009E. USAF Sat Cat: 19789.

  • Cosmos 1999 Nation: USSR. Program: Strela. Payload: Strela-3 no. 34. Mass: 220 kg (480 lb). Class: Communications. Type: Military Store-dump. Spacecraft: Strela-3. Agency: MO SSSR. Perigee: 1,383 km (859 mi). Apogee: 1,417 km (880 mi). Inclination: 82.60 deg. Period: 113.80 min. COSPAR: 1989-009F. USAF Sat Cat: 19790.

1989 - 16:55 GMT - Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
  • Cosmos 2000 Nation: USSR. Program: Resurs. Mass: 6,300 kg (13,800 lb). Class: Earth. Type: Landsat. Spacecraft: Resurs F2. Agency: MOM. Perigee: 175 km (108 mi). Apogee: 243 km (150 mi). Inclination: 82.30 deg. Period: 88.70 min. COSPAR: 1989-010A. USAF Sat Cat: 19792. Duration: 20.00 days. Decay Date: 1989-03-02.

    Investigation of the natural resources of the Earth in the interests of various branches of the Soviet economy and international cooperation; space-based survey of the central part of Antarctica for purposes of mapping inaccessible regions of that continent.

1994 - 05:35 GMT - Launch Site: White Sands. Launch Vehicle: Black Brant. Model: Black Brant 9CM1. LV Configuration: Black Brant 9CM1 NASA 36.097IE.
  • Black Brant GEMINI Plasma/Aeronomy mission Nation: Canada. Agency: NASA/CSA. Apogee: 245 km (152 mi).

1997 - 05:17 GMT - Launch Site: Poker Flat. Launch Vehicle: Black Brant. Model: Black Brant XII. LV Configuration: Black Brant XII NASA 40.10UE.
  • Black Brant PHAZE 2 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 945 km (587 mi).

1997 - 06:30 GMT - Launch Site: Nevada Test Site. Launch Complex: Area 26. Launch Vehicle: Castor-Orbus. LV Configuration: Castor-Orbus Fusing Test.
  • Castor-Orbus Test mission Nation: USA. Agency: Sandia. Apogee: 100 km (60 mi).

1997 - 14:09 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
  • Soyuz TM-25 Nation: Russia. Program: Mir. Payload: Soyuz TM 11F732 s/n 74. Class: Manned. Type: Spacecraft. Spacecraft: Soyuz TM. Manufacturer: RKK Energiya im. S.P. Korolyov, Kaliningrad-Korolyov. Agency: RKA. Perigee: 385 km (239 mi). Apogee: 392 km (243 mi). Inclination: 51.70 deg. Period: 92.30 min. COSPAR: 1997-003A. USAF Sat Cat: 24717. Duration: 184.92 days. Decay Date: 1997-08-14. Crew: Tsibliyev, Lazutkin, Ewald. Flight: Mir EO-23, Mir 97, Mir NASA-3, Mir EO-22.

    Mir Expedition EO-23. Soyuz TM-25 docked with Mir at the forward port on February 12 at 15:51:13 GMT.

1998 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-49.
  • Trident C-4 Operational Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1998 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-49.
  • Trident C-4 Operational Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1998 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-49.
  • Trident C-4 Operational Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1998 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Trident C-4. LV Configuration: Trident C-4 FCET-49.
  • Trident C-4 Operational Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1998 -
  • Galileo, Europa 13 Flyby Spacecraft: Galileo.

1998 - 13:20 GMT - Launch Site: Vandenberg. Launch Complex: 576. Launch Pad: 576E. Launch Vehicle: Taurus. Model: Taurus 2210. LV Configuration: Taurus 2210 T2 2210.
  • GFO Nation: USA. Class: Earth. Type: Radarsat. Spacecraft: GFO. Manufacturer: Ball Aerospace, Boulder. Agency: USN. Perigee: 786 km (488 mi). Apogee: 788 km (489 mi). Inclination: 108.10 deg. Period: 100.60 min. COSPAR: 1998-007A. USAF Sat Cat: 25157.

    Altimeter.

  • Orbcomm G1 Nation: USA. Program: Orbcomm. Payload: Orbcomm s/n FM3. Class: Communications. Spacecraft: Microstar. Manufacturer: Orbital Sciences Corp., Germantown (formerly Fairchild). Agency: Orbcomm. Perigee: 781 km (485 mi). Apogee: 874 km (543 mi). Inclination: 107.99 deg. Period: 101.46 min. COSPAR: 1998-007B. USAF Sat Cat: 25158.

    Plane G. Ascending node 297.9 degrees.

  • Orbcomm G2 Nation: USA. Program: Orbcomm. Payload: Orbcomm s/n FM4. Class: Communications. Spacecraft: Microstar. Manufacturer: Orbital Sciences Corp., Germantown (formerly Fairchild). Agency: Orbcomm. Perigee: 783 km (486 mi). Apogee: 871 km (541 mi). Inclination: 107.99 deg. Period: 101.45 min. COSPAR: 1998-007C. USAF Sat Cat: 25159.

    Plane G. Ascending node 298.1 degrees.

  • Celestis-02 Nation: USA. Payload: Celestis-02/Orion 38. Class: Burial . Spacecraft: Celestis. Manufacturer: Orbital Sciences Corp., Germantown (formerly Fairchild). Agency: OSC. Perigee: 780 km (480 mi). Apogee: 876 km (544 mi). Inclination: 108.00 deg. Period: 101.50 min. COSPAR: 1998-007D. USAF Sat Cat: 25160.

1999 - 08:06 GMT - Launch Site: Vandenberg. Launch Complex: LF04. Launch Vehicle: Minuteman 3. LV Configuration: Minuteman 3 GT169GM.
  • Minuteman 3 FOT GT169GM Follow-on Test launch Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi).

2000 - 01:30 GMT - Launch Site: Kagoshima. Launch Complex: M-V. Launch Pad: M-V. Launch Vehicle: M-V. Model: M-V. LV Configuration: M-V M-V-4. FAILURE: First stage failure. An anomalous vibration was detected 25 seconds after launch. At 41 seconds ceramic heat shields in the first stage nozzle broke and fell off, and thrust vector control on the nozzle was lost.
  • ASTRO E Nation: Japan. Mass: 1,680 kg (3,700 lb). Class: Astronomy. Spacecraft: ASTRO E. Manufacturer: ISAS. Agency: ISAS. Apogee: 200 km (120 mi). COSPAR: F000210A.

    Spacecraft was injected in very low perigee orbit and reentered.. X-ray astronomy satellite. Stage 1 lost control, and separated with the rocket off-course at 75 seconds in the flight. Stage 2 burned correctly and separated at 218 seconds, followed by the third stage burn at 621 seconds. Last signals were received at 20 minutes after launch. ASTRO-E was to have separated from the third stage at 23 minutes, but ended in an orbit with a perigee of only 80 km and an apogee of 410 km. It probably reentered on the first orbit at around 0230 - 0300 GMT somewhere between East Africa and western China.

2001 -
  • EVA STS-98-1 Nation: USA. Program: ISS. Spacecraft: International Space Station. Crew: Jones, Curbeam. Flight: STS-98. EVA Duration: 0.32 days.

    Tom Jones and Bob Curbeam began the first STS-98 spacewalk from the ODS airlock on Atlantis, supervising the ISS/Destiny assembly operations. The airlock was depressurized at 1544 GMT. PMA-2 was berthed on Z1 at 1650 GMT; Destiny was unberthed from the payload bay at 1735 GMT and docked to Unity at 1900 GMT. At 1935 GMT Curbeam was connecting ammonia coolant lines when a leaking connector sprayed ammonia into space, contaminating his suit. He was ordered to stay in sunlight to bake off the ammonia. At around 2311 GMT the spacewalkers returned to the airlock, closing the hatch at 2318 GMT. A new depressurization for decontamination was begun at 2342 GMT, with the airlock fully depressurized at 2350 GMT. The hatch was then opened and closed quickly at 2351-2352 GMT, to flush the airlock of any ammonia residue. This last event was not counted as an EVA by NASA.


Born on this day in:
  • 1968 - Garrett Erin Reisman.  American Mission Specialist Astronaut. Birth City: Morristown. Birth State: New Jersey. Birth Country: USA.

Died on this day in:
  • 1964 - Eugen Albert Saenger.  German German Engineer.
  • 2004 - Lewis Emmerich.  American Engineer.
 
 
 
 
 
 
 
 
 

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2007 except where otherwise noted.

 
Encyclopedia Astronautica
topic index
0 - A - B - C - D - E - F - G - H - I - J - K - L - M - N - O - P - Q - Ra - Re - Sa - Sf - Sp - T - U - V - W - X - Y - Z