Encyclopedia Astronautica
February 21


February 21 Chronology


1915 February 21 - .
  • Birth of Hugo H Woerdemann - . Nation: Germany; USA. Summary: German-American engineer in WW2. Member of the Rocket Team in the United States thereafter, arrived in America under Project Paperclip on 1945.11.16 aboard the Argentina from La Havre. Died at Temecula, Riverside, California..

1931 February 21 - . Launch Vehicle: HW-1.
  • Winkler HW-1 rocket - first liquid-fuel rocket in Europe. - . Nation: Germany. Related Persons: Winkler. Apogee: 0.0030 km (0.0019 mi). Funded by a Mr Hueckel, Winkler flies the first European liquid propellant rocket at Dessau, Germany. It is 60 cm high, weighs 5 kg, including 1.7 kg of liquid oxygen and methane propellants. The rocket consists of three tanks - one for the fuel, one for the oxygen, and one for the nitrogen gas that pressure-feeds the motor. The motor is a simple 18-inch long cylinder, housed at the centre of the prismatic rocket. The rocket reaches only 3 m in the first test due to a malfunction.

1944 February 21 - .
1944 February 21 - . Launch Site: Peenemuende. LV Family: V-2. Launch Vehicle: V-2. LV Configuration: V-2 17006.
1945 February 21 - . Launch Site: V-2 Battery 836. Launch Pad: 1./836. LV Family: V-2. Launch Vehicle: V-2.
  • V-2 Battery 1./836 begins operations near Hillscheid - . Nation: Germany. Agency: Wehrmacht. Summary: Battery 1./836 begins operations in the forest near Hillscheid and Hachenburg - Target: Antwerp..

1946 February 21 - . Launch Site: White Sands. LV Family: V-2. Launch Vehicle: V-2.
  • Peenenmuende team arrives in White Sands - . Nation: USA. Related Persons: von Braun.

1947 February 21 - .
  • XS-1 Flight 26 - . Crew: Goodlin. Payload: XS-1 # 2 flight 16. Nation: USA. Related Persons: Goodlin. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: Bell flight 16. Flight aborted after drop because of low engine-chamber pressure..

1950 February 21 - .
  • XS-1 Flight 131 - . Crew: Everest. Payload: XS-1 # 1 flight 77. Nation: USA. Related Persons: Everest. Class: Manned. Type: Manned rocketplane. Spacecraft: XS-1. Summary: AF flight 55. Wing-and-tail-loads investigation..

1953 February 21 - .
  • X-1A Flight 3 - . Crew: Ziegler. Payload: X-1A flight 3. Nation: USA. Related Persons: Ziegler. Class: Manned. Type: Manned rocketplane. Spacecraft: X-1A. Summary: Bell flight 3. First powered flight. False fire warning..

1954 February 21 - . Launch Site: Hammaguira. Launch Complex: Hammaguira Bechar. LV Family: Veronique. Launch Vehicle: Veronique. LV Configuration: Veronique NA14.
  • Test mission - . Nation: France. Agency: LRBA. Apogee: 135 km (83 mi).

1955 February 21 - . 18:25 GMT - . Launch Site: White Sands. Launch Complex: White Sands LC35. LV Family: Aerobee. Launch Vehicle: Aerobee RTV-N-10c. LV Configuration: Aerobee RTV-N-10c NRL 29.
  • Sunfollower / UVS Solar mission - . Nation: USA. Agency: NRL. Apogee: 115 km (71 mi). Summary: Solar spectrum research. Launched at 1125 local time. Reached 115 km..

1956 February 21 - . Launch Site: Wallops Island. LV Family: Deacon. Launch Vehicle: Deacon.
  • E42 model test flight - . Nation: USA. Agency: NASA. Apogee: 10 km (6 mi).

1958 February 21 - .
  • Russian sounding rocket launch. - . Nation: USSR. Summary: U.S.S.R. fired a single-stage rocket to 294-mile altitude with 3,340 pounds of experiments for measuring ion composition of the atmosphere, pressure, temperature, micrometeorites, etc., according to the Soviet IGY Committee..

1958 February 21 - . 07:40 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5A.
  • Ionosphere / biology mission - . Nation: USSR. Agency: AN. Apogee: 470 km (290 mi).

1958 February 21 - . 08:42 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5A.
  • Aeronomy / ionosphere mission - . Nation: USSR. Agency: AN. Apogee: 400 km (240 mi). Some reports say that one of the four launches this day carried the dogs Palma and Pushok. The dogs were said to have died due to cabin decompression. Rumors of the death of a 'cosmonaut Shiborin' can perhaps be attributed to this incident, if indeed it did occur.

1958 February 21 - . 09:40 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: V-2. Launch Vehicle: R-1. LV Configuration: A-1.
  • Ionosphere-solar mission Ionosphere-solar mission - . Nation: USSR. Agency: MVS. Apogee: 206 km (128 mi).

1958 February 21 - . 15:20 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. LV Family: R-5. Launch Vehicle: R-5A.
  • Ionosphere / solar ultraviolet / meteorites mission - . Nation: USSR. Agency: AN. Apogee: 473 km (293 mi).

1961 February 21 - .
  • First Mercury crews selected. - . Nation: USA. Related Persons: Shepard; Grissom; Glenn. Program: Mercury. Summary: NASA Space Task Group selected John H. Glenn, Jr., Virgil I. Grissom, and Alan B. Shepard, Jr., to begin special training for first manned Mercury space flight..

1961 February 21 - . 14:12 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC14. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 67D.
  • Mercury MA-2 - . Nation: USA. Agency: USAF. Program: Mercury. Spacecraft: Mercury. Apogee: 182 km (113 mi). Mercury-Atlas 2 (MA-2) was launched from Cape Canaveral in a test to check maximum heating and its effects during the worst reentry design conditions. The flight closely matched the desired trajectory and attained a maximum altitude of 114.04 statute miles and a range of 1,431.6 statute miles. Inspection of the spacecraft aboard the recovery ship some 55 minutes after launch (actual flight time was 17.56 minutes) indicated that test objectives were met, since the structure and heat protection elements appeared to be in excellent condition. The flight control team obtained satisfactory data; and the complete launch computing and display system, operating for the first time in a flight, performed satisfactorily.

1962 February 21 - . Launch Site: Wallops Island. LV Family: RAM. Launch Vehicle: RAM A. LV Configuration: RAM A RAM A-2.
  • RAM A-2 re-entry vehicle test flight - . Nation: USA. Agency: NASA. Apogee: 1,000 km (600 mi).

1962 February 21 - . 18:44 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg SLC1E. LV Family: Delta. Launch Vehicle: Thor Agena B. LV Configuration: Thor Agena B 332 / Agena B 2301. FAILURE: Partial failure. Agena failed to restart to circularize orbit.. Failed Stage: 2.
  • Ferret 1 - . Payload: Ferret 1 / Agena B 2301. Mass: 1,500 kg (3,300 lb). Nation: USA. Agency: USAF. Class: Military. Type: Military naval signals reconnaisance satellite. Spacecraft: Ferret. Decay Date: 1962-03-04 . USAF Sat Cat: 242 . COSPAR: 1962-Delta-1. Apogee: 219 km (136 mi). Perigee: 169 km (105 mi). Inclination: 81.9000 deg. Period: 88.30 min.

1962 February 21 - . 22:30 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg 576B3. LV Family: Atlas. Launch Vehicle: Atlas D. LV Configuration: Atlas D 52D. FAILURE: Failure. Failed Stage: 1.
  • Operational missile test - . Nation: USA. Agency: USAF SAC. Apogee: 1,800 km (1,100 mi).

1963 February 21 - . 17:58 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 618. LV Family: Polaris. Launch Vehicle: Polaris A2. LV Configuration: Polaris A2P-117.
  • Operational test - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1963 February 21 - . 23:16 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.39CA.
  • Grenades Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 172 km (106 mi).

1964 February 21 - . LV Family: Titan. Launch Vehicle: Titan 2.
  • Gemini launch vehicle 1 Subsystem Functional Verification Tests (SSFVT) began on complex 19. - . Nation: USA. Summary: These repeated the SSFVT performed at Martin-Baltimore in the vertical test facility. Their purpose was to verify the vehicle's readiness to begin systems tests. SSFVT were completed on March 3..

1964 February 21 - .
  • Birth of Scott Joseph Kelly - . Nation: USA. Summary: American test pilot astronaut. Flew on STS-103, STS-118. Twin brother of astronaut Mark Kelly..

1964 February 21 - .
  • Birth of Mark Edward Kelly - . Nation: USA. Summary: American test pilot astronaut. Flew on STS-108, STS-121, STS-124. Twin brother of astronaut Scott Kelly..

1965 February 21 - . 11:00 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC41/15. LV Family: Kosmos 3. Launch Vehicle: Kosmos 65S3. LV Configuration: Kosmos 65S3 03L.
  • Cosmos 54 - . Mass: 50 kg (110 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1. Decay Date: 1968-09-15 . USAF Sat Cat: 1089 . COSPAR: 1965-011A. Apogee: 1,839 km (1,142 mi). Perigee: 269 km (167 mi). Inclination: 56.1000 deg. Period: 106.30 min.
  • Cosmos 55 - . Mass: 50 kg (110 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1. Decay Date: 1968-02-02 . USAF Sat Cat: 1090 . COSPAR: 1965-011B. Apogee: 1,752 km (1,088 mi). Perigee: 261 km (162 mi). Inclination: 56.0000 deg. Period: 105.30 min.
  • Cosmos 56 - . Mass: 50 kg (110 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-1. Decay Date: 1967-11-02 . USAF Sat Cat: 1091 . COSPAR: 1965-011C. Apogee: 1,687 km (1,048 mi). Perigee: 259 km (160 mi). Inclination: 56.0000 deg. Period: 104.60 min.

1966 February 21 - .
  • Death of Donald D Williams - . Nation: USA. Related Persons: Williams, Donald D. Summary: American engineer, instrumental in the development of the Early Bird and Syncom communications satellites. Commited suicide in 1966..

1966 February 21 - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar LC86/1. LV Family: Kosmos 2. Launch Vehicle: Kosmos 63S1. FAILURE: First stage failed 83 seconds after launch.. Failed Stage: 1.
  • DS-K-40 s/n 2 - . Payload: DS-K-40. Nation: USSR. Agency: RVSN. Program: DS. Class: Technology. Type: Navigation technology satellite. Spacecraft: DS-K-40. COSPAR: F660221A. Summary: Development of systems for the later operational Tselina satellites..

1966 February 21 - . 13:10 GMT - . Launch Site: Eglin. LV Family: Black Brant. Launch Vehicle: Black Brant 3. LV Configuration: Black Brant III NC7.181.
  • Aeronomy mission - . Nation: USA. Agency: NRL. Apogee: 175 km (108 mi).

1966 February 21 - . 19:57 GMT - . Launch Site: Eglin. LV Family: Black Brant. Launch Vehicle: Black Brant 3. LV Configuration: Black Brant III NC7.180.
  • Aeronomy mission - . Nation: USA. Agency: NRL. Apogee: 188 km (116 mi).

1966 February 21 - . 20:23 GMT - . Launch Site: Fort Churchill. LV Family: Black Brant. Launch Vehicle: Black Brant 3. LV Configuration: Black Brant III NC7.178.
  • O2 density Aeronomy mission - . Nation: USA. Agency: NRL. Apogee: 196 km (121 mi).

1967 February 21 - . 22:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF03. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 700.
  • Follow-on operational missile test - ripple launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1967 February 21 - . 22:40 GMT - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF09. Launch Pad: LF09?. LV Family: Minuteman. Launch Vehicle: Minuteman 1B. LV Configuration: Minuteman 1B 1263.
  • Follow-on operational missile test - ripple launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1968 February 21 - .
  • Further development of Lox/LH2 rocket engines authorised. - . Nation: USSR. Summary: Decree 'On Introduction of Hydrogen in Rocket Space Technology' --future of liquid hydrogen stages' was issued..

1968 February 21 - . LV Family: Proton. Launch Vehicle: Proton-K/D.
  • L1 Launch Commission. - . Nation: USSR. Related Persons: Glushko; Konopatov; Mishin. Program: Lunar L1; Soyuz. Spacecraft: Soyuz 7K-L1; Soyuz 7K-OK. The booster failure on the previous launch was found to be due to premature fuel injection during engine start, causing initial chamber temperatures to rise 200 degrees above normal. Glushko and Konopatov both guarantee their engines for the next launch. The next L1 flight will use the 'Kruga' landing predictor. This will predict the landing point to within a 150 x 150 km area two to three hours before re-entry. Landing points on the three previous flights would have been 2000 km from Madagascar and India, Novosibirsk, and the North Pole... Mishin plans the next dual Soyuz flight for 5-10 April. Kamanin protests that the parachute and sea trials of the redesigned capsule are not yet complete. Mishin, as usual, dismisses his concerns.

1968 February 21 - . 19:40 GMT - . Launch Site: Thumba. LV Family: Belier. Launch Vehicle: Centaure.
  • ISRO 25.02 Aeronomy mission - . Nation: India. Agency: ISRO. Apogee: 136 km (84 mi).

1968 February 21 - . 23:17 GMT - . Launch Site: Wallops Island. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.284CA.
  • TMA? Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 150 km (90 mi).

1969 February 21 - . 03:01 GMT - . Launch Site: Fort Churchill. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache NASA 14.307UI. FAILURE: Failure.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

1969 February 21 - . 09:18 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC110R. LV Family: N1. Launch Vehicle: N1. LV Configuration: N-1 11A52 3L. FAILURE: First stage failure.. Failed Stage: 1.
  • N1 3L launch - . Payload: Soyuz 7K-L1S s/n 3. Nation: USSR. Related Persons: Kirillov; Dorofeyev; Afanasyev, Sergei; Mishin. Agency: RVSN. Program: Lunar L3. Class: Manned. Type: Manned spacecraft. Spacecraft: Soyuz 7K-L1A. Decay Date: 1969-02-21 . COSPAR: F690221A. Apogee: 30 km (18 mi). N-1 serial number 3L was the first N-1 launched. The vehicle ran into trouble immediately at lift-off. A fire developed in the tail compartment. The engine monitoring system detected the fire, but then gave an incorrect signal, shutting down all engines at 68.7 seconds into the flight. British intelligence detected the launch attempt, but the CIA's technical means for some reason missed it and they denied for years that it had ever occurred. In retrospect the launch team at Baikonur pointed to a grave mistake - at the christening of the first N1, the champagne bottle broke against the crawler-transporter rather than the hull of the rocket. After the 3L failure everyone knew there was no chance at all of beating the Americans to the moon. Additional Details: N1 3L launch.

1970 February 21 - .
  • Cosmonaut book - . Nation: USSR. Summary: Riabchikov conducts further interviews at the Gagarin Centre for his book..

1970 February 21 - . 12:35 GMT - . Launch Site: South Uist. LV Family: Petrel. Launch Vehicle: Petrel 1. LV Configuration: Petrel P53H.
  • UK-4 instrumented prototype Ionosphere mission - . Nation: UK. Agency: SRC. Apogee: 148 km (91 mi).

1972 February 21 - . 12:55 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy mission - . Nation: USSR. Apogee: 165 km (102 mi).

1972 February 21 - . 13:35 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy/Plasma mission - . Nation: USSR. Apogee: 187 km (116 mi).

1973 February 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC101. LV Family: R-36M. Launch Vehicle: R-36M.
  • Phase 1 state trials flight - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 February 21 - . Launch Site: Baikonur. Launch Complex: Baikonur LC104. LV Family: R-36M. Launch Vehicle: R-36M.
  • POR state trials missile launch - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 February 21 - . Launch Site: Baikonur. LV Family: UR-100N. Launch Vehicle: UR-100N.
  • State trials missile test - . Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).

1974 February 21 - . 09:16 GMT - . Launch Site: Poker Flat. LV Family: Black Brant. Launch Vehicle: Black Brant 5C. LV Configuration: Black Brant VC CRL A18.116-1.
  • HIRIS Aeronomy mission - . Nation: USA. Agency: AFCRL. Apogee: 180 km (110 mi).

1975 February 21 - . 16:00 GMT - . Launch Site: Kheysa. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 82 km (50 mi).

1976 February 21 - . 19:42 GMT - . Launch Site: Kiruna. LV Family: Apache. Launch Vehicle: Nike Apache. LV Configuration: Nike Apache SSC S18-2.
  • SSC S18 / 2 D-Layer Ionosphere mission - . Nation: Sweden. Agency: SSC. Apogee: 105 km (65 mi).

1977 February 21 - . 01:37 GMT - . Launch Site: Kheysa. LV Family: MR-12. Launch Vehicle: MR-12.
  • Aeronomy/Fields mission - . Nation: USSR. Apogee: 153 km (95 mi).

1977 February 21 - . 14:30 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Aerobee. Launch Vehicle: Aerobee 200A. LV Configuration: Aerobee 200A NASA 26.51UG.
  • JHU UVT F9 (Alpha Centauri) Astronomy mission - . Nation: USA. Agency: NASA. Apogee: 174 km (108 mi).

1977 February 21 - . 17:20 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 47182-428.
  • Cosmos 894 - . Mass: 810 kg (1,780 lb). Nation: USSR. Agency: MO. Class: Navigation. Type: Navigation satellite. Spacecraft: Parus. USAF Sat Cat: 9846 . COSPAR: 1977-013A. Apogee: 1,010 km (620 mi). Perigee: 963 km (598 mi). Inclination: 82.9000 deg. Period: 104.80 min. Summary: Military navigation satellite..

1977 February 21 - . 21:06 GMT - . Launch Site: Woomera. Launch Complex: Woomera LA8. LV Family: Aerobee. Launch Vehicle: Aerobee 170. LV Configuration: Aerobee 170 NASA 13.123IS.
  • Ultraviolet Extinction Aeronomy mission - . Nation: USA. Agency: NASA. Apogee: 177 km (109 mi).

1978 February 21 - . 11:20 GMT - . Launch Site: Kapustin Yar. Launch Complex: Kapustin Yar V-2. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 87 km (54 mi).

1979 February 21 - . 05:00 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-3C. LV Configuration: Mu-3C M-3C-4.
  • SS-04 Hakucho - . Payload: Corsa B. Mass: 100 kg (220 lb). Nation: Japan. Agency: ISAS. Class: Earth. Type: Magnetosphere satellite. Spacecraft: SS. Decay Date: 1985-04-15 . USAF Sat Cat: 11272 . COSPAR: 1979-014A. Apogee: 566 km (351 mi). Perigee: 543 km (337 mi). Inclination: 29.8000 deg. Period: 95.70 min. Soft X-ray telescope. Launching organization: Institute of Space and Aeronautical Science, University of Tokyo. Function: Observation of X-ray radiation of celestial bodies with good time resolution over a wide spectrum range. Characterstics: weight 96 kg, configuration regula r octagonal prism, height 0.66 m, diameter 0.76m, spin stabilized. Expected life 2 years.

1979 February 21 - . 07:49 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/40. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 294-01.
  • Ekran 3 - . Payload: Ekran s/n 16L. Mass: 1,970 kg (4,340 lb). Nation: USSR. Agency: MOM. Class: Communications. Type: Military communications satellite. Spacecraft: Ekran . Completed Operations Date: 1981-05-01 . USAF Sat Cat: 11273 . COSPAR: 1979-015A. Apogee: 35,919 km (22,318 mi). Perigee: 35,623 km (22,135 mi). Inclination: 14.6000 deg. Period: 1,435.30 min. Transmission of color and black-and-white USSR central television programmes to a network of receivers for collective use. Positioned in geosynchronous orbit over the Indian Ocean at 99 deg E in 1979-1981 As of 3 September 2001 located at 51.81 deg E drifting at 0.088 deg W per day. As of 2007 Mar 11 located at 98.64E drifting at 0.060E degrees per day.

1980 February 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT72GB Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1980 February 21 - . 00:53 GMT - . Launch Site: Andoya. LV Family: Tomahawk Sandia. Launch Vehicle: Nike Tomahawk. LV Configuration: Nike Tomahawk Ferdinand 49.
  • PULSAUR I Test / aurora / ionosphere mission - . Nation: Norway. Agency: NTNF. Apogee: 196 km (121 mi).

1980 February 21 - . 12:00 GMT - . Launch Site: Plesetsk. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Cosmos 1165 - . Mass: 6,300 kg (13,800 lb). Nation: USSR. Agency: MOM. Class: Surveillance. Type: Military surveillance satellite. Spacecraft: Zenit-4MKM. Duration: 13.00 days. Decay Date: 1980-03-05 . USAF Sat Cat: 11713 . COSPAR: 1980-017A. Apogee: 350 km (210 mi). Perigee: 170 km (100 mi). Inclination: 72.9000 deg. Period: 89.70 min. Summary: High resolution photo reconnaissance satellite; returned film capsule.

1981 February 21 - . Launch Site: Vandenberg. Launch Complex: Vandenberg LF26. Launch Pad: LF26?. LV Family: Minuteman. Launch Vehicle: Minuteman 3.
  • FOT GT81GB Follow-on Test launch - . Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).

1981 February 21 - . 00:30 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. LV Family: Mu. Launch Vehicle: Mu-3S. LV Configuration: Mu-3S M-3S-2.
  • SS-07 Hinotori - . Payload: Astro A. Mass: 185 kg (407 lb). Nation: Japan. Agency: ISAS. Class: Astronomy. Type: X-ray astronomy satellite. Spacecraft: Astro. Decay Date: 1991-07-11 . USAF Sat Cat: 12307 . COSPAR: 1981-017A. Apogee: 279 km (173 mi). Perigee: 274 km (170 mi). Inclination: 31.3000 deg. Period: 90.10 min. Summary: Hinotori (ASTRO-A). Launching organisation: Institute of Space and Aeronautical Science, University of Tokyo. Investigation of solar flare by X-ray telescope and spectrograph. .

1981 February 21 - . 23:23 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36A. LV Family: Atlas. Launch Vehicle: Atlas Centaur SLV-3D. LV Configuration: SLV-3D Centaur AC-42 / Centaur D-1AR 5023.
  • Comstar 4 - . Payload: Comstar 1D. Mass: 1,520 kg (3,350 lb). Nation: USA. Agency: Comsat. Program: Comstar. Class: Communications. Type: Civilian communications satellite. Spacecraft: Intelsat 4A. USAF Sat Cat: 12309 . COSPAR: 1981-018A. Apogee: 35,792 km (22,240 mi). Perigee: 35,783 km (22,234 mi). Inclination: 7.2000 deg. Period: 1,436.20 min. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). Launch vehicle put payload into geosynchronous transfer orbit Positioned in geosynchronous orbit at 142 deg W in 1981; 127 deg W in 1981-1985; 76 deg W in 1985-on. As of 31 August 2001 located at 25.65 deg W drifting at 1.067 deg E per day. As of 2007 Mar 11 located at 78.95E drifting at 0.039W degrees per day.

1982 February 21 - . 07:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: PASSAT. Launch Vehicle: MMR-06.
  • Aeronomy mission - . Nation: USSR. Agency: GMS. Apogee: 58 km (36 mi).

1983 February 21 - . 19:00 GMT - . Launch Site: Sea-launched. Launch Pad: UNKO. Launch Platform: SHIR. LV Family: M-100. Launch Vehicle: M-100.
  • - . Nation: USSR. Apogee: 91 km (56 mi).

1984 February 21 - . 06:46 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC31. LV Family: R-7. Launch Vehicle: Soyuz 11A511U.
  • Progress 19 - . Payload: Progress s/n 120. Mass: 7,020 kg (15,470 lb). Nation: USSR. Agency: MOM. Program: Salyut 7. Class: Manned. Type: Manned logistics spacecraft. Flight: Salyut 7 EO-3. Spacecraft: Progress. Duration: 40.48 days. Completed Operations Date: 1984-04-01 18:17:55 . Decay Date: 1984-04-01 18:17:55 . USAF Sat Cat: 14757 . COSPAR: 1984-018A. Apogee: 245 km (152 mi). Perigee: 186 km (115 mi). Inclination: 51.6000 deg. Period: 88.80 min. Transport of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 23 Feb 1984 08:21:00 GMT. Undocked on 31 Mar 1984 09:40:00 GMT. Destroyed in reentry on 1 Apr 1984 18:18:00 GMT. Total free-flight time 3.43 days. Total docked time 37.05 days.

1984 February 21 - . 15:36 GMT - . Launch Site: Plesetsk. Launch Complex: Plesetsk LC132/1. LV Family: Kosmos 3. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 65039-537.
  • Cosmos 1538 - . Mass: 700 kg (1,540 lb). Nation: USSR. Agency: MO. Program: Strela. Class: Communications. Type: Military store-dump communications satellite. Spacecraft: Strela-2M. USAF Sat Cat: 14759 . COSPAR: 1984-019A. Apogee: 800 km (490 mi). Perigee: 769 km (477 mi). Inclination: 74.0000 deg. Period: 100.60 min. Summary: Replaced Cosmos 1420..

1985 February 21 - . 07:57 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC200/39. LV Family: Proton. Launch Vehicle: Proton-K/DM. LV Configuration: Proton-K/DM 327-01.
  • Cosmos 1629 - . Payload: SPRN No. 3. Mass: 2,000 kg (4,400 lb). Nation: USSR. Agency: MOM. Class: Military. Type: Early warning satellite. Spacecraft: Prognoz SPRN. Completed Operations Date: 1986-10-01 . USAF Sat Cat: 15574 . COSPAR: 1985-016A. Apogee: 35,773 km (22,228 mi). Perigee: 35,738 km (22,206 mi). Inclination: 6.5000 deg. Period: 1,434.50 min. Geosynchronous ballistic missile early warning satellite. Positioned in geosynchronous orbit at 35 deg E in 1985; 24 deg W in 1985-1986 As of 5 September 2001 located at 151.95 deg W drifting at 0.251 deg E per day. As of 2007 Mar 3 located at 24.42W drifting at 0.038E degrees per day.

1986 February 21 - . 17:15 GMT - . Launch Site: ETR Launch Area. Launch Platform: SSBN 732. LV Family: Trident. Launch Vehicle: Trident C-4.
  • Demonstration and shakedown operations launch - . Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).

1987 February 21 - . 16:15 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K. LV Family: S. Launch Vehicle: S-520. LV Configuration: S-520-8.
  • GUV Ultraviolet astronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 286 km (177 mi).

1989 February 21 - . 23:30 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M. Launch Pad: M1. LV Family: Mu. Launch Vehicle: Mu-3S-II. LV Configuration: Mu-3S-II M-3S2-4.
  • Akebono - . Payload: Exos D. Mass: 295 kg (650 lb). Nation: Japan. Agency: ISAS. Class: Earth. Type: Ionosphere satellite. Spacecraft: EXOS. USAF Sat Cat: 19822 . COSPAR: 1989-016A. Apogee: 8,554 km (5,315 mi). Perigee: 272 km (169 mi). Inclination: 75.1000 deg. Period: 185.90 min. Summary: Studied aurora borealis, auroral australis. EXOS-D (Akebono). Observation in high precision of behaviour and acceleration mechanism of aurora particles in Earth magnetosphere. Launching organization ISAS. Launch time 2330 GMT. .

1990 February 21 - . Launch Site: Alcantara. LV Family: Sonda. Launch Vehicle: Sonda 2. LV Configuration: Sonda 2 XV-53.
  • Alcantara Ionosphere mission - . Nation: Brazil. Agency: INPE; IAE. Apogee: 101 km (62 mi).

1990 February 21 - . 16:00 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima L. Launch Pad: K. LV Family: S. Launch Vehicle: S-520. LV Configuration: S-520-11.
  • CIR Infrared astronomy mission - . Nation: Japan. Agency: ISAS. Apogee: 317 km (196 mi).

1991 February 21 - . 14:06 GMT - . Launch Site: Scud Batteries. Launch Pad: IRAQ-S. LV Family: R-17. Launch Vehicle: Al Hussein.
  • Combat launch - target: King Khalid Military City - . Nation: Iraq. Apogee: 100 km (60 mi).

1991 February 21 - . 14:06 GMT - . Launch Site: Scud Batteries. Launch Pad: IRAQ-S. LV Family: R-17. Launch Vehicle: Al Hussein.
  • Combat launch - target: King Khalid Military City - . Nation: Iraq. Apogee: 100 km (60 mi).

1991 February 21 - . 18:00 GMT - . Launch Site: Scud Batteries. Launch Pad: IRAQ-S. LV Family: R-17. Launch Vehicle: Al Hussein.
  • Combat launch - target: King Khalid Military City - . Nation: Iraq. Apogee: 100 km (60 mi).

1991 February 21 - . 23:31 GMT - . Launch Site: Scud Batteries. Launch Pad: IRAQ-S. LV Family: R-17. Launch Vehicle: Al Hussein.
  • Bahrain - . Nation: Iraq. Apogee: 100 km (60 mi).

1992 February 21 - .
  • Death of Milton B Ames - . Nation: USA. Related Persons: Ames. Summary: American engineer, at NASA in leadership positions, 1936-1972..

1992 February 21 - . 20:09 GMT - .
1993 February 21 - . 18:32 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U2. LV Configuration: Soyuz 11A511U2 U15000-068.
  • Progress M-16 - . Payload: Progress M s/n 216. Mass: 7,338 kg (16,177 lb). Nation: Russia. Agency: MOM. Program: Mir. Class: Manned. Type: Manned logistics spacecraft. Flight: Mir EO-13. Spacecraft: Progress M. Duration: 33.65 days. Completed Operations Date: 1993-03-27 10:05:12 . Decay Date: 1993-03-27 10:05:12 . USAF Sat Cat: 22530 . COSPAR: 1993-012A. Apogee: 234 km (145 mi). Perigee: 189 km (117 mi). Inclination: 51.7000 deg. Period: 88.70 min. Unmanned resupply vessel to Mir. Docked with Mir on 23 Feb 1993 20:17:57 GMT. Undocked on 26 Mar 1993 06:50:00 GMT. Redocked with Mir on 1993-03-26 07:06:03 GMT. Final undocking on 1993-03-27 04:21:00 GMT. Destroyed in reentry on 27 Mar 1993 10:25:00 GMT. Total free-flight time 2.33 days. Total docked time 31.32 days.

1996 February 21 - . 12:34 GMT - . Launch Site: Baikonur. Launch Complex: Baikonur LC1. LV Family: R-7. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U 651.
  • Soyuz TM-23 - . Call Sign: Skif (Roman-age tribe). Crew: Onufrienko; Usachyov. Backup Crew: Lazutkin; Tsibliyev. Payload: Soyuz TM 11F732 s/n 72. Mass: 7,150 kg (15,760 lb). Nation: Russia. Related Persons: Onufrienko; Usachyov; Lazutkin; Tsibliyev. Agency: MOM. Program: Mir. Class: Manned. Type: Manned spacecraft. Flight: Mir EO-21; Mir EO-20. Spacecraft: Soyuz TM. Duration: 193.80 days. Decay Date: 1996-09-02 . USAF Sat Cat: 23798 . COSPAR: 1996-011A. Apogee: 390 km (240 mi). Perigee: 375 km (233 mi). Inclination: 51.7000 deg. Period: 92.20 min. Summary: Mir Expedition EO-21. Soyuz TM-23 docked with Mir at 14:20:35 on February 23..

1997 February 21 - .
1998 February 21 - . 07:55 GMT - . Launch Site: Tanegashima. Launch Complex: Tanegashima Y. LV Family: H-2. Launch Vehicle: H-II. LV Configuration: H-II H-II-5F.
  • Kakehashi - . Payload: COMETS. Nation: Japan. Agency: NASDA. Manufacturer: Toshiba; NEC. Class: Communications. Type: Civilian communications satellite. Spacecraft: Kakehashi. USAF Sat Cat: 25175 . COSPAR: 1998-011A. Apogee: 17,727 km (11,015 mi). Perigee: 1,033 km (641 mi). Inclination: 30.1000 deg. Period: 328.10 min. Kakehashi, meaning 'Bridge', was called Communuications and Broadcasting Experimental Test Satellite (COMETS) before launch. It contained Ka-band communications and inter-satellite data relay payloads. Premature shutdown 44 seconds into the H-II second stage second burn put the satellite into a much lower than planned orbit. The on-board Unified Propulsion System was used to raise it to a more useful orbit.

2000 February 21 - .
2000 February 21 - .
  • Death of Kenneth D Nichols - . Nation: USA. Related Persons: Nichols. Summary: American manager, involved in directing the guided missile research and development effort for the Secretary of Defense in the early 1950's..

2002 February 21 - . 09:55 GMT - . Launch Site: Poker Flat. LV Family: Black Brant. Launch Vehicle: Black Brant 5B. LV Configuration: Black Brant VB NASA 21.128UE.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 250 km (150 mi).

2002 February 21 - . 09:57 GMT - . Launch Site: Poker Flat. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.069UE.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

2002 February 21 - . 09:59 GMT - . Launch Site: Poker Flat. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.070UE.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

2002 February 21 - . 10:01 GMT - . Launch Site: Poker Flat. LV Family: Honest John. Launch Vehicle: Taurus Orion. LV Configuration: Taurus Orion NASA 33.073UE.
  • Ionosphere mission - . Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).

2002 February 21 - . 12:43 GMT - . Launch Site: Cape Canaveral. Launch Complex: Cape Canaveral LC36B. Launch Pad: SLC36B. LV Family: Atlas V. Launch Vehicle: Atlas 3B DEC. LV Configuration: Atlas 3B-DEC AC-204.
  • Echostar 7 - . Mass: 690 kg (1,520 lb). Nation: USA. Agency: PanAmSat. Manufacturer: Lockheed; Motorola. Program: Echostar. Class: Communications. Type: Civilian communications satellite. Spacecraft: LM 700. USAF Sat Cat: 27378 . COSPAR: 2002-006A. Apogee: 35,794 km (22,241 mi). Perigee: 35,779 km (22,231 mi). Inclination: 0.1000 deg. Period: 1,436.10 min. Direct Broasdcasting satellite. The first launch of the Atlas 3B, with the Common Centaur stretched two-engine upper stage. Launch delayed from December 19, 2001 and January 22. The Echostar 7 communications satellite was placed into geostationary transfer orbit. The first burn of the Centaur put the stack into a 185 x 193 km x 28.1 deg parking orbit. At 1305 UTC the Centaur burned again to achieve the final 245 x 57060 km x 22.6 deg transfer orbit and separated from Echostar. As of 2007 Mar 11 located at 118.92W drifting at 0.006W degrees per day.

2003 February 21 - .
  • International Space Station Status Report #03-8 - . Nation: USA. Related Persons: Bowersox; Budarin; Pettit. Program: ISS. Flight: ISS EO-6. Summary: The Expedition 6 crew marked its 90th day in orbit today. Commander Ken Bowersox, Flight Engineer Nikolai Budarin and NASA ISS Science Officer Don Pettit have been in orbit since their launch from the Kennedy Space Center in Florida on Nov. 23.. Additional Details: International Space Station Status Report #03-8.

2006 February 21 - .
  • Death of Jack Pendleton Monroe - . Nation: USA. Related Persons: Monroe. Summary: American career naval officer who became a rear admiral in 1956. He served as commander of the Pacific Missile Range from 1957-1961 before becoming the Director of Astronautics for the Chief of Naval Operations from 1961-1963..

2006 February 21 - . 21:28 GMT - . Launch Site: Kagoshima. Launch Complex: Kagoshima M-V. LV Family: M-V. Launch Vehicle: M-V. LV Configuration: M-V-1 M-V-8.
  • Astro F (Akari) - . Mass: 960 kg (2,110 lb). Nation: Japan. Agency: JAXA. Manufacturer: Toshiba. Program: Astro. Class: Astronomy. Type: Infrared astronomy satellite. Spacecraft: Akari. USAF Sat Cat: 28939 . COSPAR: 2006-005A. Apogee: 719 km (446 mi). Perigee: 705 km (438 mi). Inclination: 98.2000 deg. Period: 99.00 min. Summary: Carried a 0.67m-diameter liquid-helium-cooled infrared telescope with detectors ranging from the near infrared to 60 and 170 micron channels in the far IR. It was to carry out the first far infrared sky survey since IRAS in 1983..
  • Cute 1.7 - . Mass: 3.00 kg (6.60 lb). Nation: Japan. Agency: ISAS. Manufacturer: TIT. Class: Technology. Type: Navigation technology satellite. Spacecraft: Cute. Decay Date: 2009-10-25 . USAF Sat Cat: 28941 . COSPAR: 2006-005C. Apogee: 685 km (425 mi). Perigee: 297 km (184 mi). Inclination: 98.2000 deg. Period: 94.40 min. Summary: Student subsatellite ejected from the M-V-8 third stage at 21:45 GMT..

2008 February 21 - . 03:26 GMT - . Launch Site: Pacific Ocean. Launch Platform: Lake Erie. LV Family: Standard-ER. Launch Vehicle: Standard SM-3.
  • US shoots down failed USA 193 satellite. - . Nation: USA. Agency: USN. Decay Date: 2008-02-29 . USAF Sat Cat: 29651 . The classifed NRO USA 193 spacecraft, launched in 2006, suffered a complete failure of its on-board propulsion system, putting the satellite in a rapidly-decaying orbit. The Pentagon said that the hydrazine propellant aboard consituted a risk and announced they would shoot the satellite down. The real objective may have been to demonstrated US antisatellite capability after a Chinese test in 2007. In any case, on 21 February 2008 the satellite was down to a 242 km x 257 km orbit. At 03:26 GMT an SM-3 missile was fired from the Aegis cruiser USS Lake Erie stationed west of Hawaii, to intercept the satellite. The hit-to-kill warhead successfully rammed the satellite, breaking it up into 153 catalogued items of debris with perigees of 170-250 km and apogees of up to 2700 km.

Home - Browse - Contact
© / Conditions for Use