See also Born on this Day On this day in: 1948 -
1950 -
1950 -
1950 - 01:11 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee XASR-SC-2. LV Configuration: Aerobee XASR-SC-2 SC 11.
1951 - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: Hermes. Model: Hermes A-1. LV Configuration: Hermes A-1 6. -
Test mission Nation: USA. Agency: USA. Apogee: 24 km (14 mi).
1954 - Launch Site: Kapustin Yar. Launch Complex: V-2. Launch Pad: -. Launch Vehicle: R-1. Model: R-1 8A11. LV Configuration: R-1 8A11 No 1912. -
Operational test Nation: USSR. Agency: NII-88. Apogee: 100 km (60 mi).
1957 - 20:12 GMT - Launch Site: Cape Canaveral. Launch Complex: LC5. Launch Pad: -. Launch Vehicle: Jupiter. LV Configuration: Jupiter IRBM AM-1B. FAILURE: Failure.
1960 - Launch Vehicle: Saturn I.
1960 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Nike Gosling. FAILURE: Failure. -
Porous re-entry vehicle test flight Nation: USA. Agency: NASA. Apogee: 43 km (26 mi).
1960 - 01:13 GMT - Launch Site: Cape Canaveral. Launch Complex: LC29A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1X-22. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1962 - Launch Site: Vandenberg. Launch Complex: -. Launch Pad: -. -
First West Coast launch of a Scout space booster. Nation: USA.
1962 - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-2. LV Configuration: Scout X-2 S111. FAILURE: Failure. -
Solrad 4B Nation: USA. Payload: GRAB 4B. Mass: 91 kg (200 lb). Class: Sigint. Spacecraft: GRAB. Agency: U.S. Navy. COSPAR: F620426A. Decay Date: 1962-04-26. Solar radiation monitor.
1962 - 10:02 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K. -
Cosmos 4 Nation: USSR. Payload: Zenit-2 11F61 s/n 2. Mass: 4,610 kg (10,160 lb). Class: Surveillance. Type: Military. Spacecraft: Zenit-2. Agency: RVSN. Perigee: 285 km (177 mi). Apogee: 317 km (196 mi). Inclination: 65.00 deg. Period: 90.50 min. COSPAR: 1962-Xi-1. USAF Sat Cat: 287. Duration: 3.00 days. Decay Date: 1962-04-29. Flight: Vostok 3, Vostok 4. Area survey photo reconnaissance satellite. Program partially completed. Failure of primary spacecraft orientation system. It was to spend four days in space, to be followed by another mission during 5-10 May. This meant that Vostok 3/4 could not be launched before 20-30 May. The cosmonaut prime crew returned from their in-suit parachute training at Fedosiya.
1962 - 16:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.110GI. -
Japan / US Ionosphere D-Reg Ionosphere mission Nation: USA. Agency: NASA/RRLJ. Apogee: 128 km (79 mi).
1962 - 18:00 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17A. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Delta. LV Configuration: Thor Delta 320/D9.
1962 - 18:56 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas Agena B. LV Configuration: Atlas Agena B 118D / Agena B SPS 2401.
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FTV 2401 RV Nation: USA. Payload: E-6 RV. Spacecraft: Samos. Agency: USAF. COSPAR: 1962-Pi-xx.
1963 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).
1963 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-04. FAILURE: Failure. -
Test mission Nation: France. Agency: CNES. Apogee: 58 km (36 mi).
1963 - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout X-2M. LV Configuration: Scout X-2M S121. FAILURE: Failure.
1963 - 18:31 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3X-20. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1963 - 20:13 GMT - Launch Site: Vandenberg. Launch Complex: SLC2E. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena D. LV Configuration: Thor Agena D 372 / Agena D 1411. FAILURE: Attitude sensors were misaligned. No orbit. -
KH-5 9055A Nation: USA. Payload: KH-5 s/n 9055A. Mass: 1,500 kg (3,300 lb). Class: Surveillance. Type: Military. Spacecraft: KH-5. Agency: U.S. Air Force. COSPAR: F630426AA. Decay Date: 1963-04-26. Mission failed.
1964 - Launch Site: Baikonur. Launch Complex: LC67/22. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. FAILURE: Failure. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 0 km ( mi).
1965 -
1965 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Operational test launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).
1966 - Launch Site: Baikonur. Launch Complex: LC41/4. Launch Pad: -. Launch Vehicle: R-16. Model: R-16U. -
Military training launch Nation: USSR. Agency: RVSN. Apogee: 1,210 km (750 mi).
1966 - Launch Site: Baikonur. Launch Complex: PU32. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1966 - 00:12 GMT - Launch Site: Sonmiani. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.249IM. -
Rehbar 13 (Gren / TMA) Aeronomy mission Nation: USA. Agency: NASA. Apogee: 190 km (110 mi).
1966 - 10:04 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/1. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1967 -
1967 - 04:15 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5B. LV Configuration: Black Brant VB AFF-VB-06. -
Test / ionosphere / plasma mission Nation: Canada. Agency: NRCC. Apogee: 396 km (246 mi).
1967 - 10:06 GMT - Launch Site: San Marco. Launch Complex: -. Launch Pad: -. Launch Vehicle: Scout. Model: Scout B. LV Configuration: Scout B S153C.
1967 - 18:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC4W. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3B. LV Configuration: Titan IIIB 3B-5. FAILURE: Stage 2 engine lost thrust. -
OPS 4243 Nation: USA. Payload: KH-8 no. 05 / Agena D. Mass: 3,000 kg (6,600 lb). Class: Surveillance. Type: Military. Spacecraft: KH-8. Agency: U.S. Air Force. COSPAR: F670426A. Decay Date: 1967-04-26. KH-8 type satellite.
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SRV-1 Nation: USA. Payload: SRV-1. Spacecraft: KH-8. Agency: USAF. COSPAR: F670426B.
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SRV-2 Nation: USA. Payload: SRV-2. Spacecraft: KH-8. Agency: USAF. COSPAR: F670426C.
1967 - 19:20 GMT - Launch Site: Silver Lake DZ. Launch Complex: -. Launch Pad: 35.3 N x 116.1 W. Launch Vehicle: X-15. LV Configuration: X-15 3-58-87. FAILURE: Emergency landing at Silver Lake.
1968 -
1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1968 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3P. -
Follow-on operational missile test Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1968 - 04:42 GMT - Launch Site: Kapustin Yar. Launch Complex: LC86/4. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 11K63.
1968 - 19:51 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 1-76-134.
1969 - -
Soyuz program review Nation: USSR. Program: Soyuz. Spacecraft: Soyuz 7K-OK, Soyuz Kontakt. Flight: Soyuz 5, Soyuz 6, Soyuz 7, Soyuz 8, Soyuz n 17, Soyuz n 18, Soyuz n 19, Soyuz n 20. The commission considers plans for the rest of the Soyuz production. Spacecraft s/n 14, 15, and 16 are to fly in August 1969, 17 and 18 in November 1969, and 19 and 20 in February-March 1970. Crews selected for the August flights are: for spacecraft 14, Shonin and Kubasov; for 15, Filipchenko, Volkov, and Gorbatko; for 16, Nikolayev and Sevastyanov. Back-ups will be Kuklin, Grechko, and Kolodin. All of the spacecraft will fly 4 to 5 day missions. Spacecraft 15 and 16 will dock and remain together 2 or 3 days to form an 'orbital station'. Experiments planned for the flight are: - Visual observation of rocket launch plumes using the Svinets device
- Film and photography of the spacecraft 15-16 docking from spacecraft 14
- Demonstration of welding in weightless vacuum conditions using the Vulkan device
- Demonstration of autonomous navigation by the cosmonauts using a sextant
- Medium wave radio communications
- Test of new television sensors for the Soyuz orientation system
Spacecraft 17 through 20 will fly 15 to 16 day missions to demonstrate the new SZhO life support system for the L3, and conduct rendezvous and docking operations using the L3's Kontakt system.
- Additional details.
1969 - Launch Site: Kourou. Launch Complex: ALFS. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 3. LV Configuration: Dragon 3 D-302. -
FU-188 Technology test Nation: France. Agency: CNES. Apogee: 410 km (250 mi).
1969 - 17:00 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.403IG. -
ISRO 40.04 X-ray astronomy mission Nation: USA. Agency: NASA. Apogee: 144 km (89 mi).
1970 - 13:05 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12. -
Aeronomy mission Nation: USSR. Apogee: 175 km (108 mi).
1971 - -
Quarantine for crew members who would go to the moon on future Apollo flights was discontinued Nation: USA. Program: Apollo. Flight: Apollo 15. Acting NASA Administrator George M. Low discontinued the quarantine for future Apollo flights to the moon beginning with the Apollo 15 mission. The decision was based on a recommendation of the Interagency Committee on Back Contamination (ICBC). The ICBC would continue as an active body, however, at least until the results of the last Apollo lunar mission were reviewed. Biomedical characterization of returned lunar samples would also be continued.
1971 - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
FOT GT93B Follow-on Test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).
1971 - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.388II. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).
1971 - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.387II. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).
1971 - 19:34 GMT - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C136. -
INTA C-7101 Aeronomy mission Nation: France. Agency: CNES. Apogee: 129 km (80 mi).
1971 - 19:34 GMT - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.386II. -
Ionosphere mission Nation: USA. Agency: NASA. Apogee: 100 km (60 mi).
1971 - 22:15 GMT - Launch Site: El Arenosillo. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.319II. -
INTA NC-7101 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 154 km (95 mi).
1973 - 06:20 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 27.0 N x 125.0 W. Launch Vehicle: Sandhawk. Model: Hydra Sandhawk. -
LRL BOX-18 X-ray astronomy mission Nation: USA. Agency: USN NMC. Apogee: 262 km (162 mi).
1974 - 14:23 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M.
1975 - 15:10 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A3. LV Configuration: Polaris A3T. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1977 - 14:45 GMT - Launch Site: Plesetsk. Launch Complex: LC43/3. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U. -
Cosmos 905 Nation: USSR. Payload: Yantar-2K s/n 6. Mass: 6,600 kg (14,500 lb). Class: Surveillance. Type: Military. Spacecraft: Yantar-2K. Agency: MOM. Perigee: 170 km (100 mi). Apogee: 413 km (256 mi). Inclination: 67.10 deg. Period: 90.30 min. COSPAR: 1977-030A. USAF Sat Cat: 9937. Duration: 30.00 days. Decay Date: 1977-05-26. Sixth Yantar second generation reconnaissance test flight and first completely successful flight. Both small SpK film capsules successfully recovered during course of flight, as was the main OSA cabin with its camera, computer, and main film cannisters. First full duration Yantar flight.
1978 - Launch Site: Natal. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sonda. Model: Sonda 3. LV Configuration: Sonda 3 XV-05. -
Ionosphere mission Nation: Brazil. Agency: IAE. Apogee: 615 km (382 mi).
1978 - 10:20 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1 S201C.
1980 - 22:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC3E. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F/SVS. LV Configuration: Atlas F/SVS 34F.
1983 - 10:00 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1984 - 02:40 GMT -
1985 - 05:48 GMT - Launch Site: Baikonur. Launch Complex: LC31. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-SOL.
1986 - Launch Site: Baikonur. Launch Complex: Jubilee. Launch Pad: -.
1986 - -
Major nuclear accident at Soviet Union's Chernobyl power station alarms world Nation: USSR.
1988 - 01:57 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout G. LV Configuration: Scout G-1 S211C.
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Transit O-32 Nation: USA. Program: Transit. Mass: 64 kg (141 lb). Class: Navigation. Spacecraft: Transit. Agency: USN. Perigee: 1,017 km (631 mi). Apogee: 1,298 km (806 mi). Inclination: 90.40 deg. Period: 108.50 min. COSPAR: 1988-033B. USAF Sat Cat: 19071.
1988 - 03:15 GMT - Launch Site: Baikonur. Launch Complex: LC200/39. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2. LV Configuration: Proton-K/DM-2 332-01. -
Cosmos 1940 Nation: USSR. Payload: SPRN No. 5. Mass: 2,000 kg (4,400 lb). Type: Weather. Spacecraft: Prognoz SPRN. Agency: MOM. Perigee: 35,590 km (22,110 mi). Apogee: 35,764 km (22,222 mi). Inclination: 9.00 deg. Period: 1,430.50 min. COSPAR: 1988-034A. USAF Sat Cat: 19073. Completed Operations Date: 1988-09-01. Given on Western lists as a geosynchronous ballistic missile early warning satellite. However not listed as such in Russian lists, and officially ...'conducted atmospheric, ocean studies. Investigation of the seas and oceans and the processes occurring in the earth's atmosphere'. So may have carried test instruments for second generation SPRN or had other purposes. Stationed initially at 12 deg E; Positioned in geosynchronous orbit at 24 deg W in 1988 As of 1 September 2001 located at 49.66 deg W drifting at 1.409 deg E per day. As of 2007 Mar 9 located at 70.52W drifting at 1.424E degrees per day.
1989 - 17:00 GMT - Launch Site: Plesetsk. Launch Complex: LC41/1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1990 - 01:37 GMT - Launch Site: Plesetsk. Launch Complex: -. Launch Pad: -. Launch Vehicle: Soyuz. Model: Molniya 8K78M. LV Configuration: Molniya 8K78M-ML.
1991 - 20:29 GMT -
1993 - 14:50 GMT - Launch Site: Cape Canaveral. Launch Complex: LC39A. Launch Pad: -. Launch Vehicle: Shuttle. LV Configuration: Space Shuttle STS-55. -
STS-55 Nation: USA. Program: STS. Payload: Columbia F14/USS/Spacelab D-2 LM. Mass: 12,185 kg (26,863 lb). Class: Manned. Type: Spaceplane. Spacecraft: Columbia. Agency: NASA JSC. Perigee: 304 km (188 mi). Apogee: 312 km (193 mi). Inclination: 28.50 deg. Period: 90.70 min. COSPAR: 1993-027A. USAF Sat Cat: 22640. Duration: 9.99 days. Decay Date: 1993-05-06. Crew: Harris, Henricks, Nagel, Precourt, Ross, Schlegel, Walter. Flight: STS-55. Manned seven crew. Carried German Spacelab-D2. Payloads: Spacelab D-2 with long module, unique support structure (USS), and Reaction Kinetics in Glass Melts (RKGM) getaway special, Shuttle Amateur Radio Experiment (SAREX) II.
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Spacelab D-2 LM Nation: USA. Program: Spacelab. Payload: Spacelab Long Module. Class: Manned. Type: Spacelab. Spacecraft: Spacelab. Agency: NASA. COSPAR: 1993-027xx.
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USS Nation: USA. Program: STS. Agency: NASA. COSPAR: 1993-027xx.
1994 - 02:14 GMT - Launch Site: Plesetsk. Launch Complex: LC133/3. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M.
1998 - -
Cassini Venus Flyby Nation: USA. Spacecraft: Cassini.
1999 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-21. -
84? Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1999 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Trident. Model: Trident D-5. LV Configuration: Trident D-5 FCET-21. -
Trident D-5 84? operational test launch Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
2002 - -
Starshine 2 Spacecraft Reenters Into Earth's Atmosphere Nation: USA. Spacecraft: Starshine.
2003 - Launch Site: Mojave. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tier One. -
White Knight Flight 22 Nation: USA. Program: X-Prize. Spacecraft: SpaceShipOne. Flight Time: 0.3 hours Pilot: Melvill Copilot: Binnie. Objectives: Airshow for the 'friends and family' unveiling Results: Good show for 1000+ guests. Broadcast media included CNN, ABC, PBS, Tech TV, Discovery & National Geographic TV.
2003 - 03:53 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG ?15000-006.
2004 - -
Opportunity Mars Rover, End of Primary Mission Nation: USA. Spacecraft: MER.
2004 - 20:37 GMT - Launch Site: Baikonur. Launch Complex: LC200/39. Launch Pad: -. Launch Vehicle: Proton. Model: Proton-K/DM-2M. LV Configuration: Proton-K/DM-2M 410-06.
2005 - 07:31 GMT - Launch Site: Kiritimati. Launch Complex: -. Launch Pad: 0.0 N x 154.0 W. Launch Vehicle: Zenit. Model: Zenit-3SL. LV Configuration: Zenit-3SL 15.
2006 - 22:48 GMT - Launch Site: Taiyuan. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: CZ. Model: CZ-4B. LV Configuration: Chang Zheng 4B CZ4B-9 (89).
2008 - 22:16 GMT - Launch Site: Baikonur. Launch Vehicle: Soyuz. Model: Soyuz FG. LV Configuration: Soyuz-FG/Fregat.
Born on this day in:
Died on this day in: - 1976 - Andrei Antonovich Grechko
. Russian Military Officer.
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