March 3

See also Born on this Day
On this day in:

1915 -

  • National Advisory Committee for Aeronautics (NACA) founded.

1943 - Launch Site: Peenemuende. Launch Complex: P7. Launch Vehicle: V-2. Model: V-2. LV Configuration: A-4 16. FAILURE: Explosion in the aft compartment.
  • V-2 Test mission Nation: Germany. Agency: Wehrmacht.

    Vertical flight interrupted by an explosion in the aft compartment. The engine burned for 33 seconds, and total flight was 128 seconds.

1945 - Launch Site: V-2 Gruppe Nord. Launch Vehicle: V-2.
  • Several V-2's launched after 56 Allied B-25 bombers mount an attack on V-2 headquarters units. Nation: Germany. Agency: Wehrmacht. Apogee: 90 km (55 mi).

    Due to a navigation error, many Dutch civilians were killed instead. After the attacks the Germans fired several rockets to show the Allies that the bombers missed their target.

1947 - Launch Site: White Sands. Launch Complex: LC33. Launch Vehicle: WAC. LV Configuration: WAC B 30B.
  • WAC Test mission Nation: USA. Agency: USA OR. Apogee: 63 km (39 mi).

1959 - Launch Site: Wallops Island. Launch Vehicle: Trailblazer 1. LV Configuration: Trailblazer 1 TB I alpha?.
  • Trailblazer 1 D58 re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 260 km (160 mi).

1959 - 05:10 GMT - Launch Site: Cape Canaveral. Launch Complex: LC5. Launch Pad: LC5. Launch Vehicle: Jupiter. Model: Juno II. LV Configuration: Jupiter AM-14.
  • Pioneer 4 Nation: USA. Program: Pioneer. Mass: 6.00 kg (13.20 lb). Class: Planetary. Type: Lunar. Spacecraft: Pioneer 3-4. Agency: NASA. COSPAR: 1959-Nu-1. USAF Sat Cat: 113.

    The fourth U.S.-IGY lunar probe effort, Pioneer IV, a joint project of the Army Ballistic Missile Agency and Jet Propulsion Laboratory under the direction of NASA, was launched by a Juno II rocket from the Atlantic Missile Range. Intended to impact on the lunar surface, Pioneer IV achieved earth-moon trajectory, passing within 60,200 km of the moon before going into permanent orbit around the sun.

1960 -
  • Korolev-Khruschev meeting on space plans. Nation: USSR. Spacecraft: Kosmoplan.

    Korolev believed it would be truly possible with backing from the very top to have a large rocket in the USSR in a very short span of time. Unfortunately at the meeting Korolev made a slip of the tongue he would always regret, admitting that his plan had not been agreed among all of the Chief Designers. This resulted in Khrushchev throwing the matter back for a consensus plan.

1960 - 22:50 GMT - Launch Site: Wallops Island. Launch Vehicle: Nike-Asp. Model: Nike Asp. LV Configuration: Nike Asp NASA 03.02GS.
  • Nike-Asp Solar mission Nation: USA. Agency: NASA. Apogee: 212 km (131 mi).

1961 - Launch Vehicle: Atlas D.
  • Mercury Atlas launch vehicle No. 100-D rolled out. Nation: USA. Program: Mercury.

    Factory roll-out inspection of Atlas launch vehicle No. 100-D was conducted at Convair-Astronautics. This launch vehicle was allocated for the Mercury-Atlas 3 (MA-3) mission.

1961 - Launch Site: Cape Canaveral. Launch Complex: LC18. Launch Pad: LC18B. Launch Vehicle: Blue Scout 2. Model: Blue Scout II. LV Configuration: Blue Scout II D-4.
  • Blue Scout 2 HETS A2-1 Plasma mission Nation: USA. Class: Earth. Type: Magnetosphere. Agency: USAF. Apogee: 2,540 km (1,570 mi).

1961 - Launch Site: Ile du Levant. Launch Vehicle: Antares. LV Configuration: Antares 010.
  • Antares Re-entry Vehicle Test mission Nation: France. Agency: ONERA. Apogee: 150 km (90 mi).

1961 - Launch Site: Cape Canaveral. Launch Complex: LC20. Launch Vehicle: Titan 1. Model: Titan I. LV Configuration: Titan I AJ-12. FAILURE: Failure.
  • Titan 1 Mk 4 re-entry vehicle test mission Nation: USA. Agency: USAF.

1961 - 13:59 GMT - Launch Site: Baikonur. Launch Complex: LC41. Launch Vehicle: R-16. LV Configuration: R-16 4L-6T.
  • R-16 Test mission Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1962 -
  • Aerojet-General named for the Apollo service module propulsion system Nation: USA. Program: Apollo. Spacecraft: Apollo CSM.

    The Aerojet-General Corporation was named by NAA as a subcontractor for the Apollo service module propulsion system.

1964 - Launch Site: Baikonur. Launch Vehicle: R-16. Model: R-16U.
  • R-16 State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1965 - 00:09 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Vehicle: Aerobee 150. Model: Aerobee 150. LV Configuration: Aerobee 150 AE3.516.
  • Aerobee 150 Solar Ultraviolet mission Nation: USA. Agency: USAF. Apogee: 241 km (149 mi).

1965 - 04:42 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3. LV Configuration: Skylark 3 SL87B.
  • Skylark Test mission Nation: Australia. Agency: WRE/RAE. Apogee: 216 km (134 mi).

1965 - 14:15 GMT - Launch Site: White Sands. Launch Vehicle: Aerobee 150. Model: Aerobee 150. LV Configuration: Aerobee 150 AE3.517.
  • Aerobee 150 Solar Ultraviolet mission Nation: USA. Agency: USAF. Apogee: 252 km (156 mi).

1966 -
  • Landing rocket system for Apollo. Nation: USA. Spacecraft: Apollo CSM, Apollo X.

    Associate Administrator for Manned Space Flight George E. Mueller acknowledged receipt from Joseph F. Shea, the Apollo Spacecraft Program Manager at MSC, of a detailed technical description of MSC's plans and development progress toward developing a landing rocket system for Apollo. (MSC had undertaken this effort some months earlier at Mueller's specific request.) Mueller advised Shea that he had asked AAP Deputy Director John H. Disher to work closely with Shea's people to devise a land landing system for AAP built on Houston's effort for Apollo.

1966 - Launch Site: Cape Canaveral. Launch Complex: ETR. Launch Pad: SLBM Launch Area. Launch Vehicle: Polaris A3. LV Configuration: Polaris A3 A3P-135.
  • Polaris A3 Operational Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1966 -
  • Voskhod 3 ECS Nation: USSR. Program: Voskhod. Spacecraft: Voskhod. Flight: Voskhod 3.

    Today the trials at Voronin's OKB-124 had to be halted after a 16 day run, when the cabin oxygen level went out of limits. It seems the cosmonauts could control it in flight by closely monitoring the cabin atmosphere composition and changing cartridges as necessary (typically after 5.5 days), but this is not a reliable basis for a flight. For a 20 day flight, a 22-day endurance run on earth should be a minimum, but neither the IMBP or OKB-124 have been able to make the system run longer than 14-16 days before it breaks down. Later the State Commission meets. Cosmos 110 continues in normal flight, the dogs and other life forms are alive. The only minus is that data received is complete due to the failure of the antennae to deploy.

1966 - 21:54 GMT - Launch Site: Wallops Island. Launch Vehicle: Aerobee 150. Model: Aerobee 150A. LV Configuration: Aerobee 150A NASA 04.100DS.
  • Aerobee 150 Solar mission Nation: USA. Agency: NASA. Apogee: 219 km (136 mi).

1966 - 22:26 GMT - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Vehicle: Centaure. LV Configuration: Centaure C77.
  • Centaure Solar mission Nation: France. Agency: CNES. Apogee: 125 km (77 mi).

1967 - 03:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Vehicle: Aerobee 150. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.160GG.
  • Aerobee 150 Ultraviolet Astronomy mission Nation: USA. Agency: NASA. Apogee: 157 km (97 mi).

1967 - 04:20 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Vehicle: Aerobee 150. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.84UG.
  • Aerobee 150 Infrared Astronomy mission Nation: USA. Agency: NASA. Apogee: 158 km (98 mi).

1967 - 06:44 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86. Launch Pad: LC86/1. Launch Vehicle: Kosmos 11K63. Model: Kosmos 11K63.
  • Cosmos 145 Nation: USSR. Program: DS. Payload: DS-U2-M s/n 2. Mass: 250 kg (550 lb). Class: Technology. Spacecraft: DS-U2-M. Agency: MO SSSR. Perigee: 226 km (140 mi). Apogee: 2,107 km (1,309 mi). Inclination: 48.40 deg. Period: 108.70 min. COSPAR: 1967-019A. USAF Sat Cat: 2697. Completed Operations Date: 1967-04-30. Decay Date: 1968-03-08.

    Development tests of atomic clocks.

1967 - 23:58 GMT - Launch Site: Andoya. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache Ferdinand 14.
  • Nike Apache Ferdinand 14 Ionosphere/Plasma mission Nation: Norway. Agency: NDRE. Apogee: 190 km (110 mi).

1968 -
  • Zond 4 first midcourse fails. Nation: USSR. Program: Lunar L1. Spacecraft: Soyuz 7K-L1.

    At 07:35 the first midcourse manoeuvre for Zond 4, then 225,000 km from earth, was cancelled due to an orientation system problem. The sun tracker worked, but the star tracker could not acquire Sirius. The first and second midcourse manoeuvres are not strictly necessary. However if the third midcourse fails, when the spacecraft is 167,000 km from earth on the return leg, the spacecraft will miss the atmosphere and head back out into space. A meeting is held on cosmonaut training. The simulators are still not adequate. Feoktistov is still demanding that he be trained for the first Soyuz docking mission.

1969 -
  • Soviet/Chinese troops clash on Ussuri River Nation: USSR. Program: Lunar L3. Class: Manned.

    Military on full alert; Tyuratam preempted by military through June

1969 - 10:00 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Vehicle: Aerobee 150. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.199GE.
  • Aerobee 150 XR background X-ray Astronomy mission Nation: USA. Agency: NASA. Apogee: 163 km (101 mi).

1969 - 16:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39. Launch Pad: LC39A. Launch Vehicle: Saturn V. Model: Saturn V. LV Configuration: Saturn V SA-504.
  • Apollo 9 Nation: USA. Program: Apollo. Payload: Apollo CSM 104 / Apollo LM 3 / Saturn S-IVB-504N. Mass: 36,511 kg (80,492 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo CSM. Location of Spacecraft: San Diego Aerospace Museum, San Diego, CA. Agency: NASA MSC. Perigee: 185 km (114 mi). Apogee: 187 km (116 mi). Inclination: 32.60 deg. Period: 88.60 min. COSPAR: 1969-018A. USAF Sat Cat: 3769. Duration: 10.04 days. Decay Date: 1969-03-13. Crew: McDivitt, Schweickart, Scott. Flight: Apollo 9.

    Apollo 9 (AS-504), the first manned flight with the lunar module (LM-3), was launched from Pad A, Launch Complex 39, KSC, on a Saturn V launch vehicle at 11:00 a.m. EST March 3. Originally scheduled for a February 28 liftoff, the launch had been delayed to allow crew members James A. McDivitt, David R. Scott, and Russell L. Schweickart to recover from a mild virus respiratory illness. Following a normal launch phase, the S-IVB stage inserted the spacecraft into an orbit of 192.3 by 189.3 kilometers. After post-insertion checkout, CSM 104 separated from the S-IVB, was transposed, and docked with the LM. At 3:08 p.m. EST, the docked spacecraft were separated from the S-IVB, which was then placed on an earth-escape trajectory. On March 4 the crew tracked landmarks, conducted pitch and roll yaw maneuvers, and increased the apogee by service propulsion system burns.

    On March 5 McDivitt and Schweickart entered the LM through the docking tunnel, evaluated the LM systems, transmitted the first of two series of telecasts, and fired the LM descent propulsion system. They then returned to the CM.

    McDivitt and Schweickart reentered the LM on March 6. After transmitting a second telecast, Schweickart performed a 37-minute extravehicular activity (EVA), walking between the LM and CSM hatches, maneuvering on handrails, taking photographs, and describing rain squalls over KSC.

    On March 7, with McDivitt and Schweickart once more in the LM, Scott separated the CSM from the LM and fired the reaction control system thrusters to obtain a distance of 5.5 kilometers between the two spacecraft. McDivitt and Schweickart then performed a lunar-module active rendezvous. The LM successfully docked with the CSM after being up to 183.5 kilometers away from it during the six-and-one-half-hour separation. After McDivitt and Schweickart returned to the CSM, the LM ascent stage was jettisoned.

    During the remainder of the mission, the crew tracked Pegasus III, NASA's meteoroid detection satellite that had been launched July 30, 1965; took multispectral photos of the earth; exercised the spacecraft systems; and prepared for reentry.

  • Apollo 9 LM Nation: USA. Program: Apollo. Payload: Apollo LM 3. Mass: 14,530 kg (32,030 lb). Class: Manned. Type: Lunar spacecraft. Spacecraft: Apollo LM. Agency: NASA MSC. Perigee: 185 km (114 mi). Apogee: 187 km (116 mi). Inclination: 32.60 deg. Period: 88.60 min. COSPAR: 1969-018x. USAF Sat Cat: 3769. Duration: 10.04 days. Decay Date: 1969-03-13. Flight: Apollo 9.

1970 - 14:53 GMT - Launch Site: Poker Flat. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.108GE.
  • Nike Tomahawk Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1970 - 21:15 GMT - Launch Site: Woomera. Launch Complex: LA5. Launch Pad: LA5B. Launch Vehicle: Black Arrow. LV Configuration: Black Arrow BA0 R-1.
  • Black Arrow Test mission Nation: UK. Agency: RAE. Apogee: 550 km (340 mi).

    Successful suborbital research and development flight

1971 -
  • Soviet of Chief Designers. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1, Soyuz 7KT-OK. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1.

    DOS-7K #1 completed its factory testing on 3 March. Checkout at Baikonur is to be completed by 9 April, and launch is scheduled for 15 April. The first crew to the station will be launched aboard a Soyuz on 18-20 April. Remaining items to be cleared:

    • Vibration qualification test of the station test article are not complete. They will only begin on 5 March and will take two months using 3-shift work. Mishin wants the preliminary results on 20 March.
    • Four complete Igla systems are required. Five have been completed and are working satisfactorily.
    • The expiration date on the parachute installed in the Soyuz 10 capsule is 15 April. It will have to be repacked before the flight.
    • There were numerous failures in the first phase of environmental control system qualification tests. They have to be repaired before the second phase can even be started.
    • Mishin wants the first crew to stay on the station for 30 days, the second crew 45 days. Glushko and the doctors say this is a grave risk.
1971 - Launch Site: Woomera. Launch Complex: LA2. Launch Vehicle: Aero High. LV Configuration: Aero High AH4.
  • Aero High Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 178 km (110 mi).

1971 - Launch Site: Woomera. Launch Complex: LA2. Launch Vehicle: Aero High. LV Configuration: Aero High AH5.
  • Aero High Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 178 km (110 mi).

1971 - 06:52 GMT - Launch Site: Fort Churchill. Launch Vehicle: Black Brant. Model: Black Brant VB. LV Configuration: Black Brant VB AAF-VB-32.
  • Black Brant Auroral mission Nation: Canada. Agency: NRCC. Apogee: 275 km (170 mi).

1971 - 09:30 GMT - Launch Site: Baikonur. Launch Vehicle: Voskhod 11A57. Model: Voskhod 11A57.
  • Cosmos 399 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-4M. Agency: MOM. Perigee: 200 km (120 mi). Apogee: 285 km (177 mi). Inclination: 64.90 deg. Period: 89.30 min. COSPAR: 1971-017A. USAF Sat Cat: 5003. Duration: 14.00 days. Decay Date: 1971-03-17.

    High resolution photo reconnaissance satellite; returned film capsule; maneuverable.

1971 - 12:15 GMT - Launch Site: Jiuquan. Launch Complex: LA2. Launch Pad: LA2A. Launch Vehicle: CZ-1. Model: Chang Zheng 1.
  • SJ-1 Nation: China. Payload: Shi Jian 1. Mass: 221 kg (487 lb). Class: Technology. Type: Comsat. Spacecraft: DFH-1. Agency: MAI. Perigee: 265 km (164 mi). Apogee: 1,833 km (1,138 mi). Inclination: 69.80 deg. Period: 106.10 min. COSPAR: 1971-018A. USAF Sat Cat: 5007. Decay Date: 1979-06-17.

    Similar in appearance to the American Telstar and conducted communications technology tests.

1972 - 01:49 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36. Launch Pad: LC36A. Launch Vehicle: Atlas Centaur SLV-3C. Model: SLV-3C Centaur. LV Configuration: SLV-3C Centaur AC-27 / Centaur D-1A 5007C.
  • Pioneer 10 Nation: USA. Program: Pioneer. Payload: Pioneer F. Mass: 259 kg (570 lb). Class: Planetary. Type: Outer Planets. Spacecraft: Pioneer 10-11. Agency: NASA ARC. COSPAR: 1972-012A. USAF Sat Cat: 5860.

    Jupiter flyby December 1973; first man-made object to leave solar system. The spacecraft achieved its closest approach to Jupiter on December 3, 1973, when it reached approximately 2.8 Jovian radii (about 200,000 km). As of Jan. 1, 1997 Pioneer 10 was at about 67 AU from the Sun near the ecliptic plane and heading outward from the Sun at 2.6 AU/year and downstream through the heliomagnetosphere towards the tail region and interstellar space. - Additional details.

1973 - 06:05 GMT - Launch Site: Thumba. Launch Vehicle: Centaure. Model: Centaure 2A. LV Configuration: Centaure 2A ISRO 5.19.
  • Centaure ISRO 5.19 Fields mission Nation: India. Agency: ISRO/CNES. Apogee: 125 km (77 mi).

1973 - 06:50 GMT - Launch Site: Thumba. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache ISRO 10.45.
  • Nike Apache ISRO 10.45 Aeronomy mission? Nation: India. Agency: ISRO. Apogee: 158 km (98 mi).

1976 -
  • Payload bay doors on dock, Palmdale, Enterprise Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise.

    Payload bay doors on dock, Palmdale, Enterprise (OV-101)

1976 - 00:10 GMT - Launch Site: Kheysa. Launch Vehicle: MR-12. LV Configuration: MR-12 MR-12.
  • MR-12 Aeronomy/Ionosphere/Chemical release/Plasma mission Nation: USSR. Apogee: 164 km (101 mi).

1976 - 17:44 GMT - Launch Site: Poker Flat. Launch Vehicle: Paiute Tomahawk. LV Configuration: Paiute Tomahawk GL A10.507-1.
  • Paiute Tomahawk ICECAP 76 Aeronomy mission Nation: USA. Agency: USAF GL. Apogee: 210 km (130 mi).

1977 - 10:30 GMT - Launch Site: Plesetsk. Launch Vehicle: Soyuz 11A511U. Model: Soyuz 11A511U.
  • Cosmos 896 Nation: USSR. Mass: 6,300 kg (13,800 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-6U. Agency: MOM. Perigee: 202 km (125 mi). Apogee: 206 km (128 mi). Inclination: 72.90 deg. Period: 88.60 min. COSPAR: 1977-016A. USAF Sat Cat: 9857. Duration: 13.00 days. Decay Date: 1977-03-16.

    Photo surveillance; returned film capsule; maneuverable.

1978 -
  • Complete modification for mated vibe tests. Nation: USA. Program: STS. Class: Manned. Type: Spaceplane. Spacecraft: Enterprise.

    Complete modification for mated vertical ground vibration test, Edwards, Enterprise (OV-101)

1980 - Launch Site: Vandenberg. Launch Complex: SLC3. Launch Pad: SLC3W. Launch Vehicle: Atlas F. Model: Atlas F/MSD. LV Configuration: Atlas F/MSD 67F.
  • EP-2 (NOSS 3) Nation: USA. Payload: Plume shield. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS-Subsat. Agency: USN. Perigee: 1,048 km (651 mi). Apogee: 1,166 km (724 mi). Inclination: 63.50 deg. Period: 107.40 min. COSPAR: 1980-019E. USAF Sat Cat: 11733.

  • NOSS 3 Nation: USA. Payload: PARCAE 3. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS. Agency: USN. Perigee: 1,035 km (643 mi). Apogee: 1,150 km (710 mi). Inclination: 63.00 deg. Period: 107.10 min. COSPAR: 1980-019A. USAF Sat Cat: 11720.

    Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE.

  • EP 1 Nation: USA. Payload: SSU. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS-Subsat. Agency: USN. Perigee: 1,048 km (651 mi). Apogee: 1,166 km (724 mi). Inclination: 63.50 deg. Period: 107.40 min. COSPAR: 1980-019C. USAF Sat Cat: 11731.

    Deployed from NOSS 3.

  • EP 2 Nation: USA. Payload: SSU. Spacecraft: NOSS. Agency: USN. Perigee: 730 km (450 mi). Apogee: 1,484 km (922 mi). Inclination: 63.40 deg. Period: 107.41 min. COSPAR: 1980-019D. USAF Sat Cat: 11732.

  • EP 3 Nation: USA. Payload: SSU. Class: Sigint. Type: Naval reconnaisance. Spacecraft: NOSS-Subsat. Agency: USN. Perigee: 1,048 km (651 mi). Apogee: 1,166 km (724 mi). Inclination: 63.50 deg. Period: 107.40 min. COSPAR: 1980-019G. USAF Sat Cat: 11745.

    Deployed from NOSS 3.

1982 - 05:44 GMT - Launch Site: Plesetsk. Launch Complex: LC16. Launch Pad: LC16/2. Launch Vehicle: Molniya 8K78M. Model: Molniya 8K78M.
  • Cosmos 1341 Nation: USSR. Payload: Oko #24. Mass: 1,250 kg (2,750 lb). Class: Early Warning. Spacecraft: Oko. Agency: MOM. Perigee: 4,229 km (2,627 mi). Apogee: 36,092 km (22,426 mi). Inclination: 67.50 deg. Period: 717.10 min. COSPAR: 1982-016A. USAF Sat Cat: 13080.

    Replaced Cosmos 1247. Covered Oko constellation plane 5 - 79 degree longitude of ascending node.

1983 - 03:54 GMT - Launch Site: Punta Lobos. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.26UE.
  • Taurus Orion Project Condor plasma mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1984 - 04:40 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Vehicle: Black Brant. Model: Black Brant VB. LV Configuration: Black Brant VB NASA 21.85UG.
  • Black Brant Astronomy mission Nation: USA. Agency: NASA. Apogee: 206 km (128 mi).

1984 - 06:24 GMT - Launch Site: Fort Churchill. Launch Vehicle: Black Brant. Model: Black Brant 8C. LV Configuration: Black Brant 8C ADD-VIIIC-9.
  • Black Brant ARIES A Auroral/Aeronomy/Ionosphere mission Nation: Canada. Agency: Canada. Apogee: 206 km (128 mi).

1985 - 14:45 GMT - Launch Site: Natal. Launch Vehicle: Skylark. Model: Skylark 12. LV Configuration: Skylark 12 DLR N-GRC-137. FAILURE: Failure.
  • Skylark Interzodiak 1 Extreme ultraviolet Astronomy mission Nation: Germany. Agency: DFVLR.

1987 - 11:14 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1. Launch Vehicle: Soyuz 11A511U2. Model: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 I15000-016.
  • Progress 28 Nation: USSR. Program: Mir. Payload: Progress s/n 137. Mass: 7,246 kg (15,974 lb). Class: Manned. Type: Logistics. Spacecraft: Progress. Agency: MOM. Perigee: 185 km (114 mi). Apogee: 254 km (157 mi). Inclination: 51.60 deg. Period: 88.90 min. COSPAR: 1987-023A. USAF Sat Cat: 17564. Duration: 24.69 days. Completed Operations Date: 1987-03-28 03:48:55. Decay Date: 1987-03-28 03:48:55. Flight: Mir EO-2, Mir LD-1.

    Unmanned supply vessel to Mir. Orbit of station at time of rendezvous was 344 X 369 km, 51. 62 deg. Docked with Mir on 5 Mar 1987 12:42:36 GMT. Undocked on 26 Mar 1987 05:06:48 GMT. Destroyed in reentry on 28 Mar 1987 03:49:00 GMT. Total free-flight time 4.01 days. Total docked time 20.68 days.

1987 - 15:03 GMT - Launch Site: Plesetsk. Launch Complex: LC32. Launch Pad: LC32. Launch Vehicle: Tsyklon 3. Model: Tsiklon-3.
  • Cosmos 1825 Nation: USSR. Program: Tselina. Payload: Tselina-D no. 60. Mass: 1,600 kg (3,500 lb). Class: Sigint. Spacecraft: Tselina-D. Agency: MO SSSR. Perigee: 594 km (369 mi). Apogee: 621 km (385 mi). Inclination: 82.50 deg. Period: 96.80 min. COSPAR: 1987-024A. USAF Sat Cat: 17566.

    Ocean surveillance.

1989 - 18:17 GMT - Launch Site: Kiruna. Launch Vehicle: Black Brant. Model: Black Brant VB. LV Configuration: Black Brant VB NASA 21.100UU.
  • Black Brant Aeronomy mission Nation: USA. Agency: NASA. Apogee: 124 km (77 mi).

1992 -
  • Energia Engineer Cosmonaut Training Group 11 selected. Nation: USSR.

1998 -
  • EVA Mir EO-25-1 Nation: Russia. Program: Mir. Class: Manned. Type: Space station. Spacecraft: Mir. Crew: Musabayev, Budarin. Flight: Mir NASA-6, Mir EO-25. EVA Duration: 0.0658 days.

    Inner and outer airlocks of Kvant-2 module were depressurised for EVA. However the crew could not open the outer hatch, repaired on 2 January 1998 by Solovyov and Vinogradov. The planned EVA was cancelled.

1998 - 22:33 GMT - Launch Site: Kiruna. Launch Vehicle: Nike Orion. LV Configuration: Nike Orion DLR K-NO2-233.
  • Nike Orion NLTE-1 Atomic 2A Ionosphere mission Nation: Sweden. Agency: SSC. Apogee: 134 km (83 mi).


Born on this day in:
  • 1946 - James (Jim) Craig Adamson.  American Mission Specialist Astronaut. Birth City: Warsaw. Birth State: New York. Birth Country: USA.
  • 1949 - Dr Bonnie Jeanne Dunbar.  American Mission Specialist Astronaut. Birth City: Sunnyside. Birth State: Washington. Birth Country: USA.
  • 1949 - James Shelton (Jim) Voss.  American Mission Specialist Astronaut. Birth City: Cordova. Birth State: Alabama. Birth Country: USA.

Died on this day in:
  • 2003 - Gentry.  American Pilot Test Pilot.
 
 
 
 
 
 
 
 
 

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