See also Born on this Day On this day in: 1948 - 21:41 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee RTV-N-8. LV Configuration: Aerobee RTV-N-8 A6.
1957 - Launch Site: Cape Canaveral. Launch Complex: LC3. Launch Pad: -. Launch Vehicle: X-17. LV Configuration: X-17 VI-1 4-204-1A?. -
4-204-1A? re-entry vehicle test flight Nation: USA. Agency: USN. Apogee: 100 km (60 mi).
1959 - -
Mercury small-scale escape-tower combinations launched Nation: USA. Program: Mercury. Spacecraft: Mercury. Two small-scale spacecraft escape-tower combinations were launched successfully at Wallops Island. On the next day a full-scale spacecraft escape system was launched. The complete sequence of events - escape system firing, escape tower jettisoning, parachute deployment, landing, and helicopter recovery - was satisfactory.
1959 - 21:18 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Agena A. LV Configuration: Thor Agena A 170 / Agena A 1018. -
Discoverer 2 Nation: USA. Payload: KH-1 prototype / Agena A 1022. Mass: 743 kg (1,638 lb). Class: Surveillance. Type: Military. Spacecraft: KH-1. Agency: DARPA. Perigee: 239 km (148 mi). Apogee: 346 km (214 mi). Inclination: 89.90 deg. Period: 90.40 min. COSPAR: 1959-Gamma-1. USAF Sat Cat: 14. Decay Date: 1959-04-26. KH-1 prototype; tested capsule recovery techniques; did not carry camera; capsule recovery failed. Because of a timing error, the US believed that the capsule landed somewhere on the island of Spitsbergen, north of Norway, instead of landing in the recovery zone near Hawaii. The capsule was never found; and CIA officials suspect it may have been snatched by the Soviets. The search for this capsule formed the basis of the book and film 'Ice Station Zebra'. In the winter of 1960/1961, a US Discovery spy satellite capsule was found by loggers near Kalinin, 200 km north of Moscow. The loggers cracked it open with an axe. Sergei Khrushchev believed this to be the Discoverer 2 capsule. What was left was examined by Soviet engineers but didn’t reveal much information - it was a polished aluminium sphere, 30 cm in diameter, gilded on the exterior. Some said it was found as early as the winter of 1959.
1960 - 12:02 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Thor Ablestar. LV Configuration: Thor Ablestar 257 AB002?.
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Dummy subsatellite Nation: USA. Payload: GRAB dummy. Mass: 18 kg (39 lb). Class: Sigint. Spacecraft: GRAB. Agency: USAF. COSPAR: 1960-Gamma-3. USAF Sat Cat: 33. Decay Date: 1960-07-17.
1960 - 17:15 GMT - Launch Site: Rosamund Dry Lake DZ. Launch Complex: -. Launch Pad: 34.7 N x 118.1 W. Launch Vehicle: X-15. LV Configuration: X-15 1-4-9.
1962 - Launch Vehicle: N1.
1963 -
1963 -
1963 -
1963 - Launch Site: Kwajalein. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike Zeus. Model: Nike Zeus. LV Configuration: Nike Zeus-3. -
K-21 Titan Intercept Nation: USA. Agency: USA. Apogee: 200 km (120 mi).
1963 - Launch Site: Vandenberg. Launch Complex: 395-A3. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 1. LV Configuration: Titan I SM-1. -
NTMP K-21 Target mission Nation: USA. Agency: USAF SAC. Apogee: 1,000 km (600 mi).
1963 - 11:00 GMT - Launch Site: Kapustin Yar. Launch Complex: Mayak-2. Launch Pad: -. Launch Vehicle: Kosmos 2. Model: Kosmos 63S1.
1964 -
1964 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 1. LV Configuration: Dragon D-06. -
FU-104B Probe / Na Aeronomy mission Nation: France. Agency: CNES. Apogee: 425 km (264 mi).
1964 - Launch Site: Hammaguira. Launch Complex: Bacchus. Launch Pad: -. Launch Vehicle: Belier. Model: Centaure. LV Configuration: Centaure C59. -
Sodium / TMA release Aeronomy mission Nation: France. Agency: CNES. Apogee: 151 km (93 mi).
1964 - 19:00 GMT - Launch Site: Vandenberg. Launch Complex: LF07. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 734. -
Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1965 - 04:05 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 60.0 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.67UA.
1965 - 16:00 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 60.0 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.27UA.
1965 - 17:10 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 60.0 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.186UE.
1965 - 19:06 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 59.9 S x 78.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.101UA.
1965 - 21:00 GMT - Launch Site: Vandenberg. Launch Complex: LF08. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 1165. -
Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1965 - 21:00 GMT - Launch Site: Vandenberg. Launch Complex: LF02. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. LV Configuration: Minuteman 1B 851. -
Operational missile test Nation: USA. Agency: SAC 1STRAD. Apogee: 1,300 km (800 mi).
1966 - Launch Vehicle: Titan. Model: Titan 2.
1967 - Launch Site: Kagoshima. Launch Complex: L. Launch Pad: -. Launch Vehicle: Lambda. Model: Lambda 4S. LV Configuration: Lambda 4S L-4S-3. FAILURE: Fourth stage failed to ignite. -
Ohsumi 3 Nation: Japan. Payload: L-4S-3. Mass: 26 kg (57 lb). Class: Technology. Spacecraft: Ohsumi. Agency: ISAS. Apogee: 200 km (120 mi). COSPAR: F670413A. Decay Date: 1967-04-13.
1967 - 06:22 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun CRL AF6.561. -
Ion trap Ionosphere mission Nation: USA. Agency: AFCRL. Apogee: 116 km (72 mi).
1967 - 07:24 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL AF08.647. -
Sphere / TMA Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 175 km (108 mi).
1969 - 00:33 GMT - Launch Site: Andoya. Launch Complex: -. Launch Pad: -. Launch Vehicle: Belier. Model: Dragon 2B. LV Configuration: Dragon 2B D-255. -
FU-182 Ions / Electric field Ionosphere mission Nation: France. Agency: CNES. Apogee: 399 km (247 mi).
1969 - 02:24 GMT - Launch Site: Cape Canaveral. Launch Complex: LC13. Launch Pad: -. Launch Vehicle: Atlas. Model: SLV-3A Agena D. LV Configuration: SLV-3A Agena D 5502A / Agena D 2802.
1969 - 14:04 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.326GE. -
Magnetospheric mission Nation: USA. Agency: NASA. Apogee: 155 km (96 mi).
1970 -
1970 - Launch Site: Baikonur. Launch Complex: LC162/36. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67P. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1970 - 12:34 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 NASA 04.321UA. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 200 km (120 mi).
1971 - -
Cosmodrome jammed for series of historic launches. Nation: USSR. Program: Salyut, Lunar L3. Spacecraft: Salyut 1. Flight: Soyuz 10. Nikolayev and others are flying to the cosmodrome. All of the cosmonauts except Volynov will be present for the historic launch of the first space station., the first crew to the station, and the N1 launch planned for 1 May. Kamanin has an argument with the cosmonauts on the necessity of working out on the KTF trainer during the mission.
1972 - Launch Site: Vandenberg. Launch Complex: LF05. Launch Pad: -. Launch Vehicle: Minuteman 2. -
OT GT88M operational test launch Nation: USA. Agency: USAF SAC. Apogee: 1,300 km (800 mi).
1972 - 01:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.107-1. -
Mass Spectrometer Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 120 km (70 mi).
1972 - 01:16 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL AT07.894. -
Mass Spectrometer Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 128 km (79 mi).
1972 - 01:30 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL A08.013-1. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 214 km (132 mi).
1972 - 01:45 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.217-2. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 190 km (110 mi).
1972 - 04:00 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.215-1. -
Sphere Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 219 km (136 mi).
1972 - 04:15 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.921-4. -
Release Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 164 km (101 mi).
1972 - 07:50 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.921-2. -
TMA / Grenade Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 160 km (90 mi).
1972 - 09:30 GMT - Launch Site: Eglin. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.921-6. -
TMA Aeronomy mission Nation: USA. Agency: AFCRL. Apogee: 175 km (108 mi).
1974 - 23:33 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 2914. LV Configuration: Delta 2914-C 588/D101.
1975 - 00:51 GMT - Launch Site: Vandenberg. Launch Complex: SLC3W. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 71F / Star-17A. FAILURE: First stage failure due to explosion in flame pit at lift-off.
1975 - 08:15 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.174GE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 299 km (185 mi).
1975 - 09:46 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Castor. LV Configuration: Castor DNA EX531.43-1. -
EXCEDE Active plasma mission Nation: USA. Agency: USAF. Apogee: 100 km (60 mi).
1975 - 10:38 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.173GE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 299 km (185 mi).
1976 - 17:16 GMT - Launch Site: Baikonur. Launch Complex: LC90/19. Launch Pad: LC90/pad?. Launch Vehicle: Tsiklon. Model: Tsiklon-2.
1978 - 19:22 GMT - Launch Site: Kiruna. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Orion. LV Configuration: Nike Orion NASA 31.06UE. -
SSC S27 TWILIGHT Test / aeronomy mission Nation: USA. Agency: NASA. Apogee: 153 km (95 mi).
1979 - 22:05 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 8C. LV Configuration: Black Brant 8C NASA 27.33AS-US. -
Solar mission Nation: USA. Agency: NASA. Apogee: 268 km (166 mi).
1983 - 09:06 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Sergeant. Model: Sounding Rocket. LV Configuration: Sergeant GL A30.276. -
FWIF VI Auroral mission Nation: USA. Agency: USAF GL. Apogee: 140 km (80 mi).
1984 - 13:14 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Loki. Model: Super Loki. LV Configuration: Super Loki T 1-0883. -
Aeronomy mission Nation: USA. Agency: NASA WFC. Apogee: 110 km (60 mi).
1984 -
1985 - Launch Site: Baikonur. Launch Complex: -. Launch Pad: -. Launch Vehicle: Zenit. Model: Zenit-2. FAILURE: Failure. -
R&D suborbital Zenit launch vehicle test failure Nation: USSR. Agency: UNKS.
1986 - 09:14 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 10. LV Configuration: Black Brant X NASA 35.016GE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 977 km (607 mi).
1990 - 18:53 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: LC1 or LC31. Launch Vehicle: Soyuz. Model: Soyuz 11A511U.
1990 - 22:28 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 6925-8. LV Configuration: Delta 6925-8 D194. -
Palapa B2R Nation: Indonesia. Program: Palapa. Mass: 1,200 kg (2,600 lb). Class: Communications. Spacecraft: HS 376. Agency: Perumtel. Perigee: 35,784 km (22,235 mi). Apogee: 35,795 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.30 min. COSPAR: 1990-034A. USAF Sat Cat: 20570. Refurbished Palapa B2 retrieved by STS-51A; 107.7 deg E. Communication services for Indonesia, the Association of South-East Asian Nations (ASEAN), and Papua New Guinea. Launch time 2227:59.719 Z. Launch complex 17, ETR. Positioned in geosynchronous orbit at 108 deg E in 1990-1999 As of 29 August 2001 located at 42.49 deg E drifting at 0.002 deg E per day. As of 2007 Mar 9 located at 163.55E drifting at 2.663W degrees per day.
1991 - 00:09 GMT - Launch Site: Cape Canaveral. Launch Complex: LC17B. Launch Pad: -. Launch Vehicle: Delta. Model: Delta 7925. LV Configuration: Delta 7925 D204. -
ASC-2 / Spacenet F4 Nation: USA. Program: GTE. Mass: 1,350 kg (2,970 lb). Class: Communications. Spacecraft: ASC. Agency: Contel. Perigee: 35,780 km (22,230 mi). Apogee: 35,794 km (22,241 mi). Inclination: 0.00 deg. Period: 1,436.20 min. COSPAR: 1991-028A. USAF Sat Cat: 21227. Commercial business communications; stationed at 101 deg W. C, Ku band communications satellite. Positioned in geosynchronous orbit at 101 deg W in 1991-1999; 81 deg W in 2000. As of 6 September 2001 located at 172.04 deg E drifting at 0.007 deg W per day. As of 2007 Mar 9 located at 34.51E drifting at 2.539W degrees per day.
1994 - 06:04 GMT - Launch Site: Cape Canaveral. Launch Complex: LC36B. Launch Pad: -. Launch Vehicle: Atlas. Model: Atlas I. LV Configuration: Atlas I AC-73 / Centaur I 5053. -
GOES 8 Nation: USA. Payload: GOES I. Mass: 2,105 kg (4,640 lb). Class: Earth. Type: Weather. Spacecraft: GOES-Next. Agency: NOAA. Perigee: 35,770 km (22,220 mi). Apogee: 35,807 km (22,249 mi). Inclination: 0.10 deg. Period: 1,436.20 min. COSPAR: 1994-022A. USAF Sat Cat: 23051. Geostationary Environmental Satellite. Stationed at 75 deg W. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A). Launch vehicle put payload into supersynchronous earth orbit with MRS trajectory option. Positioned in geosynchronous orbit at 90 deg W in 1994-1995; 75 deg W in 1995-1999 As of 5 September 2001 located at 74.78 deg W drifting at 0.019 deg E per day. NASA announced that GOES-8 was "de-orbited" (presumably moved to a sub-synchronous orbit) on May 5, 2004 after 10 years of service. As of 2007 Mar 11 located at 87.46E drifting at 4.935W degrees per day.
2002 - 14:09 GMT -
2004 - 03:30 GMT - Launch Site: White Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Mk 70 Orion. LV Configuration: Terrier Mk 70 Orion NASA 12.54GT. -
NMACS test Nation: USA. Agency: NASA GSFC. Apogee: 122 km (75 mi).
2006 - Launch Site: Barking Sands. Launch Complex: -. Launch Pad: -. Launch Vehicle: SR19/SR19. -
CMCM-1 Target mission Nation: USA. Agency: USA SMDC/MDA. Apogee: 200 km (120 mi). A two-stage SR19 rocket was flown from the Kaui Test Facility in the Pacific Missile Range Facility. The payload included the deployment of complex countermeasures, a mock reentry vehicle, an onboard sensor package. This series of radar certification flight was initially part of the Block 2004 effort.
Born on this day in:
Died on this day in: - 2002 - Aleksandr Yakovlevich Kramarenko
. Ukrainian Pilot Cosmonaut. Cause of Death: Heart attack at a railway station.
- 2004 - Joachim Wilhelm Muehlner. German Rocket engineer.
- 2008 - Vladimir Mkrtychovich Gevorkyan. Russian Engineer Cosmonaut.
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© Mark Wade, 1997 - 2008 except where otherwise noted.
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