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On this day in:

1909 -

  • Goddard Lox/LH2 rocket concept Nation: USA.

    Goddard realises his earlier nested gun concept is not practical - he calculates it will take 56 tons of explosive to launch a 500 pound payload to an altitude of 2,000 miles. He realises Lox/LH2 will make the ideal rocket fuel, although he is still thinking in terms of explosive pulses.

1931 - Launch Vehicle: Schmiedl.
  • First rocket-mail. Nation: Austria. Apogee: 1.00 km (0.60 mi).

    Schmiedl launches his V7 post rocket with 100 letters aboard from Schoeckel bei Graz to Sankt Radegund, a distance of two kilometres. The 880 cm long rocket descended as planned by parachute .

1951 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-1. Model: R-1. LV Configuration: R-1 IIIA-3.
  • Nation: USSR. Agency: NII-88. Apogee: 100 km (60 mi).

    Last launch in winter test series.

1954 - 18:35 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee RTV-N-10. LV Configuration: Aerobee RTV-N-10 NRL 20.
  • Sunfollower UVS Solar ultraviolet mission Nation: USA. Agency: NRL. Apogee: 101 km (62 mi).

    Solar ultraviolet research. Launched at 1135 local time. Reached 101 km.

1956 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-5. Model: R-5M.
  • BAYKAL Nuclear test Nation: USSR. Agency: MVS. Apogee: 500 km (310 mi).

    The R-5M successfully launched an 80 kiloton (300 kiloton according to some sources) warhead over a 1200 km range - from Kaputsin Yar Area 4N to a point near Priaralsk Karakum, 150 km north-east of the Aral Sea.

1957 - 08:05 GMT - Launch Site: Holloman. Launch Complex: A. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee AJ10-34. LV Configuration: Aerobee AJ10-34 USAF 76.
  • Firefly (Ethelyne) Aeronomy / chemical release mission Nation: USA. Agency: ARDC. Apogee: 143 km (88 mi).

    Ethylene gas release (Firefly). Launched at 0105 local time. Reached 140.6 km.

1959 - Launch Vehicle: Saturn I.
  • Booster name changed from Juno V to Saturn Nation: USA. Program: Apollo.

    The Army proposed that the name of the large clustered-engine booster be changed from Juno V to Saturn, since Saturn was the next planet after Jupiter. Roy W. Johnson, Director of the Advanced Research Projects Agency, approved the name on February 3.

1960 - 18:08 GMT - Launch Site: Cape Canaveral. Launch Complex: LC19. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I B-7A.
  • Test mission Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi).

1961 - Launch Vehicle: Saturn C-3, Saturn I, Saturn V.
  • NERVA Request for Proposal. Nation: USA. Program: NERVA.

    NASA-AEC Space Nuclear Propulsion Office invited industry to submit proposals for participation in development of Nerva (nuclear engine for rocket vehicle application), a part of Project Rover initiated in 1955 by USAF-AEC.

1961 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-11. Model: R-11A.
  • Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 200 km (120 mi).

1961 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-11. Model: R-11A.
  • Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 200 km (120 mi).

1961 - 19:00 GMT - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: LC41/pad?. Launch Vehicle: R-16. LV Configuration: R-16 3L-5T. FAILURE: Failure.
  • First successful R-16 launch. Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).

    The missile was supposed to be launched at 18:00, but is then delayed to 24:00 due to technical problems. It is a clear night, illuminated by the moon, and the missile takes off at midnight. The first three minutes of flight are successful, but then the second stage fails to ignite. The missiles impacts 520 km downrange from the launch pad.

1963 - 06:56 GMT - Launch Site: Vandenberg. Launch Complex: LC-A. Launch Pad: -. Launch Vehicle: Scout. Model: Blue Scout Jr SLV-1C. LV Configuration: Blue Scout Jr SLV-1C 202.
  • ERCS 279L Communications mission Nation: USA. Agency: USAF. Apogee: 1,000 km (600 mi).

1964 - Launch Site: Baikonur. Launch Complex: LC60/8. Launch Pad: LC60/8?. Launch Vehicle: R-16. Model: R-16U.
  • Military training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).

1965 -
  • Cosmonaut organisation Nation: USSR. Program: Lunar L1, Lunar L3. Spacecraft: Soyuz A, Soyuz B, Soyuz V, LK-1, Soyuz PPK, Soyuz R.

    Kamanin will organise the cosmonauts into two groups: the first group will be commanded by Nikolayev, and the latest group by Beregovoi. They will be assigned to support and train seven missions: military space (reconnaissance, interceptor, and combat spacecraft); space navigation; life support and rescue systems; communications and telemetry systems; scientific orbital stations; lunar fly-by; and lunar landing expeditions. All of this may be for nought, since Marshall Malinovskiy has said that heavy launch vehicles and lunar flights have no military utility and should be funded and handled by the Academy of Science.

1965 - Launch Site: Larson AFB. Launch Complex: -. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1.
  • Last Titan I ICBM taken off alert status at Larson AFB Nation: USA.

1965 - Launch Site: Tonopah. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. LV Configuration: Tomahawk Sandia 152-17.
  • Magnus Test / aeronomy mission Nation: USA. Agency: Sandia. Apogee: 106 km (65 mi).

1965 - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1041.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1965 - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 714.
  • Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1965 - 06:30 GMT - Launch Site: Green River. Launch Complex: Pad 2. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena D003. FAILURE: Failure.
  • USAF D003 re-entry vehicle test flight Nation: USA. Agency: USAF. Apogee: 50 km (31 mi).

1965 - 09:57 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: -. Launch Vehicle: HAD. LV Configuration: HAD 152.
  • Aeronomy mission Nation: Australia. Agency: WRE. Apogee: 123 km (76 mi).

1965 - 20:50 GMT - Launch Site: Delamar Dry Lake DZ. Launch Complex: -. Launch Pad: 37.3 N x 114.9 W. Launch Vehicle: X-15. LV Configuration: X-15 3-40-63.
  • X-15A MA-25S TPS,MH-96,BLN Test/Technology mission Nation: USA. Agency: NASA/USAF. Apogee: 29 km (18 mi).

    Maximum Speed - 6253 kph. Maximum Altitude - 29931 m.

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

    Smirnov again questions the chief designers about the reliability of the parachute systems developed by Tkachev. The VVS remains troubled as to the reliability of these systems. Recently the system has been tested at Fedosiya to increase its rating to 2900 to 3200 kg for use on Voskhod-3. Three parachutes in these tests suffered rips during deployment. The Voskhod-3 capsule will weigh 3000 kg. Tkachev says he will guarantee its safety, but VVS and LII specialists do not share this optimism. Leonov, Gagarin, and various cosmonauts ask Kamanin to stop further showings of the new film comedy "30-3", which they say denigrates Soviet cosmonauts. However a showing to the leadership is enjoyed by all, and they see no grounds for surpressing it.

1966 - 02:02 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.186GM.
  • Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 118 km (73 mi).

1966 - 10:04 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.50UG.
  • Spica ultraviolet spectra Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 175 km (108 mi).

1966 - 21:32 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 450 / Agena D SS-01B 1623.
  • KH-4A 1029 Nation: USA. Payload: KH-4A s/n 1029 / Agena D 1623. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-4A. Agency: NRO/CIA. Perigee: 182 km (113 mi). Apogee: 428 km (265 mi). Inclination: 75.00 deg. Period: 90.60 min. COSPAR: 1966-007A. USAF Sat Cat: 1968. Decay Date: 1966-02-27.

    KH-4A. Both panoramic cameras were operational throughout.

1966 - 23:15 GMT - Launch Site: Woomera. Launch Complex: LA2. Launch Pad: LA2 SL. Launch Vehicle: Skylark. Model: Skylark 3 AC. LV Configuration: Skylark 3 AC SL307.
  • LUX Solar AC5 Solar x-ray and ultraviolet mission Nation: Australia. Agency: WRE/RAE. Apogee: 216 km (134 mi).

1967 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2087.
  • ERCS 2 Communications mission Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).

1967 - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3 Agena D. LV Configuration: SLV-3 Agena D 7126 / Agena D 7126.
  • Agena D Nation: USA. Spacecraft: KH-7. Agency: USAF. Perigee: 126 km (78 mi). Apogee: 285 km (177 mi). Inclination: 102.70 deg. Period: 88.61 min. COSPAR: 1967-007B. USAF Sat Cat: 2665. Decay Date: 1967-02-15.

  • KH 7-36 Nation: USA. Payload: KH-7 no. 36. Mass: 2,000 kg (4,400 lb). Class: Surveillance. Type: Military. Spacecraft: KH-7. Agency: NRO/USAF. Perigee: 136 km (84 mi). Apogee: 357 km (221 mi). Inclination: 103.00 deg. Period: 89.50 min. COSPAR: 1967-007A. USAF Sat Cat: 2664. Decay Date: 1967-02-12.

    KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).

1968 - 05:30 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.261GG.
  • X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 139 km (86 mi).

1968 - 06:10 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.220GG.
  • Stellar astronomy Ultraviolet astronomy mission Nation: USA. Agency: NASA. Apogee: 149 km (92 mi).

1968 - 10:17 GMT - Launch Site: Vandenberg. Launch Complex: LF24. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 2464.
  • ST Olympic Trials 8 operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1968 - 12:55 GMT - Launch Site: Vandenberg. Launch Complex: LF09. Launch Pad: LF09?. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1274. FAILURE: Failure.
  • ST Olympic T. B-1 operational test launch Nation: USA. Agency: SAC 1STRAD. Apogee: 10 km (6 mi).

1968 - 13:26 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.259IA.
  • INCOSPAR 10.13 ISRO Aeronomy / ionosphere mission Nation: India. Agency: ISRO. Apogee: 191 km (118 mi).

1968 - 13:40 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C90.
  • ISRO 15.06 Aeronomy mission Nation: India. Agency: ISRO. Apogee: 159 km (98 mi).

1969 - 08:25 GMT - Launch Site: Vandenberg. Launch Complex: LF04. Launch Pad: -. Launch Vehicle: Minuteman 2. LV Configuration: Minuteman 2 FTM-2208.
  • Giant Fist 5 demonstration and shakedown operations launch Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).

1970 -
  • Soyuz 9 experiment review Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK. Flight: Soyuz 9.

    Nikolayev visits the IMBP to review the modified ECS required for the long-duration Soyuz 9 mission. This will have to function reliably for 20 days. The biomedical experiments and objectives of the mission are also reviewed.

1970 - 23:07 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5A. LV Configuration: Black Brant VA A-BBVA-23.
  • DLR A-BBV-23 Synove Aeronomy / ionosphere / plasma mission Nation: Germany. Agency: DLR. Apogee: 202 km (125 mi).

1971 -
  • Military Soviet of the VVS considers manned space plans - Day 2. Nation: USSR. Spacecraft: Spiral OS.

    Kamanin waits and waits to give his speech on the second day of the VVS Military Soviet. It is constantly postponed. He spends 16 hours waiting 'on-call'. This demonstrates to him the poor organisation of the military leadership.

1971 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: UR-100. Model: UR-100M.
  • First State trials launch Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1971 - 15:35 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE R19.
  • QUINCE II (Probe A) Aeronomy / ionosphere / Fields mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi).

1971 - 15:36 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Terrier Tomahawk. LV Configuration: Terrier Tomahawk SECEDE R20.
  • QUINCE II (Probe E) Aeronomy / Fields mission Nation: USA. Agency: Sandia. Apogee: 300 km (180 mi).

1972 - 05:30 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P110T/C.
  • ISRO 18.06 Ionosphere mission Nation: UK. Agency: SRC. Apogee: 134 km (83 mi).

1972 - 11:25 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.111UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 173 km (107 mi).

1973 - 06:15 GMT - Launch Site: Gillam. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 3B. LV Configuration: Black Brant IIIB AAF-3B-67.
  • Auroral mission Nation: Canada. Agency: NRCC. Apogee: 200 km (120 mi).

1973 - 06:20 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AAF-VB-36.
  • Auroral substorm Aurora / aeronomy / plasma mission Nation: Canada. Agency: NRCC. Apogee: 335 km (208 mi).

1973 - 19:05 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure 2A. LV Configuration: Centaure 2A ISRO 5.18.
  • ISRO 5.18 CO.07 Ionosphere mission Nation: India. Agency: ISRO. Apogee: 147 km (91 mi).

1977 -
  • Burnup of the Salyut 4 Space Station (USSR) Nation: USSR. Spacecraft: Salyut 4.

1977 - 12:30 GMT - Launch Site: Plesetsk. Launch Complex: LC132/2. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53746-306.
  • Cosmos 891 Nation: USSR. Mass: 900 kg (1,980 lb). Class: Calibration. Spacecraft: Taifun-1. Agency: MO SSSR. Perigee: 472 km (293 mi). Apogee: 516 km (320 mi). Inclination: 65.80 deg. Period: 94.50 min. COSPAR: 1977-006A. USAF Sat Cat: 9801. Decay Date: 1981-02-04.

    Radar calibration mission.

1978 - 08:54 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.08UE.
  • Plasma mission Nation: USA. Agency: NASA. Apogee: 616 km (382 mi).

1978 - 13:04 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P199H.
  • Atomic oxygen Atmospheric mission Nation: UK. Agency: SRC. Apogee: 140 km (80 mi).

1978 - 13:33 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P203H.
  • Ion composition Ionosphere mission Nation: UK. Agency: SRC. Apogee: 112 km (69 mi).

1978 - 13:56 GMT - Launch Site: South Uist. Launch Complex: -. Launch Pad: -. Launch Vehicle: Petrel. Model: Petrel 1. LV Configuration: Petrel P112H.
  • Solar La Ionosphere / solar ultraviolet mission Nation: UK. Agency: SRC. Apogee: 135 km (83 mi).

1980 - 08:47 GMT - Launch Site: Kagoshima. Launch Complex: -. Launch Pad: -. Launch Vehicle: S. Model: S-310. LV Configuration: S-310-8.
  • Aeronomy mission Nation: Japan. Agency: ISAS. Apogee: 179 km (111 mi).

1981 - 02:19 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
  • Cosmos 1243 Nation: USSR. Mass: 1,400 kg (3,000 lb). Class: Military. Type: ASAT. Spacecraft: IS-A. Agency: MO SSSR. Perigee: 294 km (182 mi). Apogee: 1,013 km (629 mi). Inclination: 65.80 deg. Period: 97.80 min. COSPAR: 1981-010A. USAF Sat Cat: 12160. Decay Date: 1981-02-02.

    ASAT interceptor. Approached within 50 m of target, but explosive charge did not go off as planned. Deorbited to destructive reentry in the atmosphere.

1984 - 15:36 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Super Chief. Model: Talos Sergeant Hydac.
  • HAVE SLED II Target mission Nation: USA. Agency: USAF BMO. Apogee: 500 km (310 mi).

1984 - 17:38 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47139-532.
  • Cosmos 1535 Nation: USSR. Mass: 810 kg (1,780 lb). Class: Navigation. Spacecraft: Parus. Agency: MO SSSR. Perigee: 953 km (592 mi). Apogee: 1,013 km (629 mi). Inclination: 83.00 deg. Period: 104.80 min. COSPAR: 1984-010A. USAF Sat Cat: 14679.

    Military navigation satellite. Replaced Cosmos 1428.

1991 - 21:41 GMT - Launch Site: Scud Batteries. Launch Complex: -. Launch Pad: IRAQ-S. Launch Vehicle: R-17. Model: Al Hussein.
  • Riyadh Nation: Iraq. Agency: IRAQ. Apogee: 100 km (60 mi).

1994 - Launch Site: Vandenberg. Launch Complex: LF26. Launch Pad: LF26?. Launch Vehicle: Minuteman 3.
  • FOT GT154GB Follow-on Test launch Nation: USA. Agency: USAF AFSPC. Apogee: 1,300 km (800 mi).

1995 - 15:27 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.138CE.
  • Aria-II Ionosphere mission Nation: USA. Agency: NASA. Apogee: 340 km (210 mi).

1995 - 15:51 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.230UE.
  • Ionosphere mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).

1999 - 01:30 GMT - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: K. Launch Vehicle: S. Model: S-310. LV Configuration: S-310-28.
  • SELENE RF / X-ray test Ionosphere / x-ray mission Nation: Japan. Agency: ISAS. Apogee: 184 km (114 mi).

2003 - 12:59 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. LV Configuration: Soyuz-U E15000-680.
  • Progress M-47 Nation: Russia. Program: ISS. Payload: Progress M s/n 247. Mass: 7,290 kg (16,070 lb). Class: Manned. Type: Logistics. Spacecraft: Progress M. Manufacturer: RKK Energia. Agency: Rosaviakosmos. Perigee: 195 km (121 mi). Apogee: 247 km (154 mi). Inclination: 51.65 deg. Period: 88.77 min. COSPAR: 2003-006A. USAF Sat Cat: 27681. Duration: 206.00 days. Decay Date: 2003-08-28. Flight: ISS EO-6.

    Launch delayed from original schedule of January 30, and was made just one day after the Columbia disaster resulted in a suspension of shuttle flights. Docked successfully with the ISS on 14:49 GMT on 4 February 2003. Undocked from Zvezda on August 27 and deorbited later the same day.

2007 - 16:28 GMT - Launch Site: Xichang. Launch Complex: LC2. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-3A. LV Configuration: Chang Zheng 3A CZ3A-12 (95).
  • Beidou 2A Nation: China. Payload: Beiduou 1D. Mass: 2,200 kg (4,800 lb). Class: Navigation. Spacecraft: Beidou. Perigee: 35,326 km (21,950 mi). Apogee: 36,248 km (22,523 mi). Inclination: 6.20 deg. Period: 1,436.10 min. COSPAR: 2007-003A. USAF Sat Cat: 30323.

    Fourth Beidou satellite. It did not reach geostationary orbit until early April following deployment problems with its solar panels and reports of US detection of a debris cloud at the time of the original expected apogee firing.


Born on this day in:
  • 1906 - Shen Qizhen.  Chinese Engineer. Birth City: Chongqing. Birth State: Sichuan. Birth Country: China.

Died on this day in:
  • 2001 - Otto Heinrich Hirschler.  German Rocket engineer.

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