See also Born on this Day On this day in: 1951 - 03:16 GMT - Launch Site: White Sands. Launch Complex: LC33. Launch Pad: -. Launch Vehicle: V-2. LV Configuration: V-2 57. FAILURE: Failure. -
Blossom IVE Ionosphere/Aeronomy mission Nation: USA. Agency: USA/ARDC. Apogee: 3.00 km (1.80 mi). Launched 20:16 local time. Reached 3.1 km. Carried composition, air glow, sky brightness, ionosphere experiments for Air Research and Development Command.
1955 -
1956 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Honest John. Model: HJ Nike T40 T55. FAILURE: Failure. -
Test launch Nation: USA. Agency: NACA. Apogee: 1.00 km (0.60 mi).
1959 -
1960 - Launch Site: Cape Canaveral. Launch Complex: LC25A. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A1. LV Configuration: Polaris A1X-14. -
Test mission Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1961 - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Polaris. Model: Polaris A2. LV Configuration: Polaris A2X-8. -
Test mission Nation: USA. Agency: USN. Apogee: 1,000 km (600 mi).
1961 - 02:30 GMT - Launch Site: Cape Canaveral. Launch Complex: LC6. Launch Pad: -. Launch Vehicle: Redstone. Model: Redstone. LV Configuration: Redstone 2040. FAILURE: Control system malfunction during re-entry at 374 sec.
1961 - 06:29 GMT - Launch Site: Baikonur. Launch Complex: LC1. Launch Pad: -. Launch Vehicle: Soyuz. Model: Vostok 8K72K. LV Configuration: Vostok 8K72K E103-14. -
Korabl-Sputnik 4 Nation: USSR. Program: Vostok. Payload: Vostok 3KA s/n 1. Mass: 4,700 kg (10,300 lb). Class: Manned. Type: Spacecraft. Spacecraft: Vostok. Agency: RVSN. Perigee: 173 km (107 mi). Apogee: 239 km (148 mi). Inclination: 64.90 deg. Period: 88.60 min. COSPAR: 1961-Theta-1. USAF Sat Cat: 91. Duration: 0.0700 days. Decay Date: 1961-03-09. Flight: Vostok 1. Carried dog Chernushka, mannequin Ivan Ivanovich, and other biological specimens. Ivanovich was ejected from the capsule and recovered by parachute, and Chernsuhka was successfully recovered with the capsule on March 9, 1961 8:10 GMT. Officially: Development of the design of the space ship satellite and of the systems on board, which ensure necessary conditions for man's flight.
- Additional details.
1963 - 00:01 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.60GA. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 117 km (72 mi).
1963 - 00:01 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Cajun. Model: Nike Cajun. LV Configuration: Nike Cajun NASA 10.54GA. -
Grenades Aeronomy mission Nation: USA. Agency: NASA. Apogee: 119 km (73 mi).
1964 - 21:54 GMT - Launch Site: Walker AFB. Launch Complex: Missile Site 579. Launch Pad: 579-2. Launch Vehicle: Atlas. Model: Atlas F. LV Configuration: Atlas F 90F. FAILURE: Exploded during propellant loading.
1965 - 06:26 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 1.0 S x 84.0 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.65UA.
1965 - 16:25 GMT - Launch Site: Pacific Ocean. Launch Complex: -. Launch Pad: 3.1 S x 84.4 W. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.85UE.
1965 - 18:29 GMT - Launch Site: Vandenberg. Launch Complex: SLC2W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2 Agena D. LV Configuration: Thor SLV-2 Agena D 419 / Agena D SS-01A 2701.
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Oscar 3 Nation: USA. Program: Oscar. Mass: 14 kg (30 lb). Class: Communications. Type: Amateur Radio. Spacecraft: Oscar. Agency: OSCAR. Perigee: 876 km (544 mi). Apogee: 900 km (550 mi). Inclination: 70.10 deg. Period: 102.80 min. COSPAR: 1965-016F. USAF Sat Cat: 1293. OSCAR III was launched piggyback with seven United States Air Force satellites. Weight 16.3 kg. It was the first amateur satellite to operate from solar power and relay signals from Earth. OSCAR III was the first true amateur satellite relaying voice contacts in the VHF 2 meter band through a 1 W 50 kHz wide linear transponder (146 MHz uplink and 144 MHz downlink). OSCAR III's transponder lasted 18 days. More than 1000 amateurs in 22 countries communicated through the linear transponder. The two beacon transmitters continued operating for several months.
Note: Designed, built, and tested, a predecssor, OSCAR* was never launched. Similar in design to OSCAR I and II, OSCAR* contained a 250 mW beacon with phase-coherent keying. OSCAR* was never launched as the workers decided to focus their efforts on the first relay satellite -- OSCAR III.
1966 - -
Douglas proposal on the airlock for the AAP. Nation: USA. Spacecraft: Orbital Workshop. A team of engineers from Douglas Aircraft Company, headed by Jack Bromberg, presented a technical briefing and cost proposal to Associate Administrator for Manned Space Flight George E. Mueller on the company's design on the airlock for the AAP. Mueller observed that Douglas' idea for a 30-day capability seemed technically sound. He expressed strong interest in the AAP spent-stage experiment because it would establish a solid basis for space station requirements and definition. However, he cautioned that he had not received definite approval from either the Administrator, James E. Webb, or his deputy, Robert C. Seamans, Jr., on the spent-stage concept and admitted that he had 'some selling to do.'
1966 - 02:22 GMT - Launch Site: White Sands. Launch Complex: LC35. Launch Pad: -. Launch Vehicle: Aerobee. Model: Aerobee 150. LV Configuration: Aerobee 150 KP3.15. -
Stellar spectra Ultraviolet astronomy mission Nation: USA. Agency: KPNO. Apogee: 150 km (90 mi).
1966 - 22:02 GMT - Launch Site: Vandenberg. Launch Complex: SLC1W. Launch Pad: -. Launch Vehicle: Delta. Model: Thor SLV-2A Agena D. LV Configuration: Thor SLV-2A Agena D 452 / Agena D SS-01B 1622.
1967 - 05:07 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.24GE. -
Auroral electrons Aurora mission Nation: USA. Agency: NASA. Apogee: 227 km (141 mi).
1967 - 13:27 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Apache. Model: Nike Apache. LV Configuration: Nike Apache NASA 14.162IA. -
ISRO 10.10 Aeronomy mission Nation: USA. Agency: NASA. Apogee: 184 km (114 mi).
1969 - 03:29 GMT - Launch Site: Cape Parry. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.85GE. -
Magnetospheric mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).
1969 - 16:35 GMT - Launch Site: Kheysa. Launch Complex: -. Launch Pad: -. Launch Vehicle: MR-12. -
Release? Aeronomy mission Nation: USSR. Agency: AN SSSR. Apogee: 172 km (106 mi).
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 - 03:14 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk CRL AT08.298. -
B field / particles Aurora mission Nation: USA. Agency: USAF. Apogee: 298 km (185 mi).
1970 - 03:21 GMT - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Nike. Model: Nike Iroquois. LV Configuration: Nike Iroquois CRL A07.907-2. -
E field Plasma mission Nation: USA. Agency: USAF. Apogee: 158 km (98 mi).
1970 - 08:25 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.99GI. -
ISRO 17.03 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 264 km (164 mi).
1970 - 14:30 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.97GI. -
ISRO 17.01 Ionosphere mission Nation: USA. Agency: NASA. Apogee: 298 km (185 mi).
1970 - 19:38 GMT - Launch Site: Thumba. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.98GI. -
ISRO 17.02? Ionosphere mission Nation: USA. Agency: NASA. Apogee: 296 km (183 mi).
1971 - -
Major DOS training exercise by first crew. Nation: USSR. Program: Salyut. Spacecraft: Salyut 1. Flight: Soyuz 10, Soyuz 11, Soyuz 12 / DOS 1. A major training session is held with Shatalov, Yeliseyev, and Rukavishnikov. They make a 15 hour simulated 'flight' aboard the DOS trainer from 09:15 to 22:45. All operations expected in a thirty-day mission to the station are gone through. This includes simulation of emergencies to test the reactions of both the crew and ground controllers. Kamanin receives a letter from Anders, thanking him for the tour of Star City. Representatives from the Swedish firm are in town to negotiate the contract for the TsF-18 18-metre radius centrifuge. Both Korolev and Mishin fought against the VVS getting such a centrifuge.
1972 - 12:00 GMT - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.73UE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 243 km (150 mi).
1972 - 14:08 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Tomahawk Sandia. Model: Nike Tomahawk. LV Configuration: Nike Tomahawk NASA 18.143GE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 270 km (160 mi).
1973 - Launch Site: Vandenberg. Launch Complex: LF06. Launch Pad: -. Launch Vehicle: Minuteman 1. Model: Minuteman 1B. -
ABRES NTV-1 re-entry vehicle test flight Nation: USA. Agency: USAF AFSC. Apogee: 1,300 km (800 mi).
1973 - Launch Site: Baikonur. Launch Complex: LC161/35. Launch Pad: -. Launch Vehicle: Tsiklon. Model: R-36 8K67MA. -
State trials missile test Nation: USSR. Agency: RVSN. Apogee: 1,000 km (600 mi).
1973 - 21:00 GMT - Launch Site: Vandenberg. Launch Complex: SLC4E. Launch Pad: -. Launch Vehicle: Titan. Model: Titan 3D. LV Configuration: Titan IIID 23D-6.
1974 - -
Kamanin in retirement. Nation: USSR. Gagarin's birthday. Kamanin reflects that before Gagarin's death, everything seemed possible - they were planning manned expeditions to the Moon, Mars, Venus…now there are no plans for man to ever get beyond low earth orbit. Kamanin's life in retirement is full of small concerns. He spends time at the dacha, the apartment needs repairs but he has no savings to pay for it. He goes to Communist Party meetings and commemorations of various space anniversaries. He is consulted to provide advice for historical books and films.
1974 - Launch Site: Wake Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. Model: Athena H. -
HAVE MILL 2 re-entry vehicle test flight Nation: USA. Agency: USAF/USA. Apogee: 200 km (120 mi).
1974 - 02:22 GMT - Launch Site: Vandenberg. Launch Complex: SLC5. Launch Pad: -. Launch Vehicle: Scout. Model: Scout D-1. LV Configuration: Scout D-1-F S188C.
1976 - Launch Site: Wallops Island. Launch Complex: -. Launch Pad: -. Launch Vehicle: Athena RTV. LV Configuration: Athena SAMSO-37. -
ABRES Re-entry Vehicle test Nation: USA. Agency: USAF/Sandia. Apogee: 200 km (120 mi).
1977 - Launch Vehicle: Alfa.
1977 - Launch Site: Fort Churchill. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Orion. LV Configuration: Nike Orion NASA 31.02UA. -
Auroral NO Aeronomy mission Nation: USA. Agency: NASA. Apogee: 138 km (85 mi).
1977 - 16:40 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 5C. LV Configuration: Black Brant VC NASA 21.41US. -
Solar mission Nation: USA. Agency: NASA. Apogee: 191 km (118 mi).
1978 - 08:13 GMT - Launch Site: Poker Flat. Launch Complex: -. Launch Pad: -. Launch Vehicle: Terrier. Model: Terrier Malemute. LV Configuration: Terrier Malemute NASA 29.07UE. -
Plasma mission Nation: USA. Agency: NASA. Apogee: 336 km (208 mi).
1979 - Launch Vehicle: Shuttle.
1983 -
1983 - 03:06 GMT - Launch Site: Punta Lobos. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Orion. LV Configuration: Nike Orion NASA 31.27GE. -
Project Condor Plasma mission Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).
1983 - 03:27 GMT - Launch Site: Punta Lobos. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Orion. LV Configuration: Nike Orion NASA 31.32GE. -
Project Condor Plasma mission Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).
1983 - 08:57 GMT - Launch Site: Punta Lobos. Launch Complex: -. Launch Pad: -. Launch Vehicle: Hawk. Model: Nike Orion. LV Configuration: Nike Orion NASA 31.33GE. -
Project Condor Plasma mission Nation: USA. Agency: NASA. Apogee: 140 km (80 mi).
1986 - -
Vega 2, Comet Halley Flyby Nation: USSR. Spacecraft: Vega 5VK.
1989 - 21:33 GMT - Launch Site: ETR Launch Area. Launch Complex: -. Launch Pad: -. Launch Vehicle: Poseidon. -
Demonstration and shakedown operations launch Nation: USA. Agency: USN. Apogee: 500 km (310 mi).
1990 - 18:00 GMT - Launch Site: White Sands. Launch Complex: LC36. Launch Pad: -. Launch Vehicle: Black Brant. Model: Black Brant 9. LV Configuration: Black Brant IX NASA 36.66GU. -
Aeronomy mission Nation: USA. Agency: NASA. Apogee: 300 km (180 mi).
1992 - 22:35 GMT - Launch Site: Plesetsk. Launch Complex: LC132/1. Launch Pad: -. Launch Vehicle: Kosmos 3. Model: Kosmos 11K65M. LV Configuration: Kosmos 11K65M 53778-423.
1996 - 01:53 GMT - Launch Site: Point Arguello WADZ. Launch Complex: -. Launch Pad: 36.0 N x 123.0 W. Launch Vehicle: Pegasus. Model: Pegasus XL. LV Configuration: Pegasus XL F10. -
REX-II Nation: USA. Class: Earth. Type: Ionosphere. Spacecraft: REX. Agency: USAF STP. Perigee: 799 km (496 mi). Apogee: 835 km (518 mi). Inclination: 90.00 deg. Period: 101.20 min. COSPAR: 1996-014A. USAF Sat Cat: 23814. LEO
1996 -
2002 -
2004 - Launch Site: Sonmiani. Launch Complex: -. Launch Pad: -. Launch Vehicle: Shaheen. Model: Shaheen 2.
2005 - -
Cassini, Enceladus & Tethys Flyby, Successful Nation: USA. Spacecraft: Cassini.
2007 - 03:10 GMT - Launch Site: Cape Canaveral. Launch Complex: LC41. Launch Pad: SLC41. Launch Vehicle: Atlas V. Model: Atlas V 401. LV Configuration: Atlas V 401 AV-013. -
Astro Nation: USA. Mass: 1,090 kg (2,400 lb). Class: Technology. Type: Rendezvous. Spacecraft: Orbital Express Astro. Manufacturer: Boeing. Agency: DARPA. Perigee: 491 km (305 mi). Apogee: 498 km (309 mi). Inclination: 46.00 deg. Period: 94.50 min. COSPAR: 2007-006A. USAF Sat Cat: 30772. The active satellite portion of DARPA's Orbital Express satellite servicing experiment. Following operational tests while still joined or grappled together, the first 10-m distance Nextsat free flight and redocking by Astro was conducted on 5 May. On the second free-flight test on 11 May a serious computer failure left the two spacecraft 6 km apart. The problem was solved, revised software was uploaded to Astro, and it redocked with Nextsat on 19 May.
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CFESat Nation: USA. Payload: Heavily modified Surrey MicroSat-100. Mass: 159 kg (350 lb). Class: Technology. Spacecraft: MicroSat-100. Manufacturer: Surrey. Agency: LANL. Perigee: 558 km (346 mi). Apogee: 563 km (349 mi). Inclination: 35.40 deg. Period: 95.90 min. COSPAR: 2007-006F. USAF Sat Cat: 30777. The Cibola Flight Experiment satellites carried eight new technologies for space flight validation, including a new power supply, inflatable antennas, deployable booms, a new type of launch-vehicle separation system, and a high-density pack of AA lithium-ion batteries. Cibola's on-board field programmable gate array supercomputer processed data onboard, then beamed only the results rather than the raw data to the ground. The Cibola also had a science mission: the study of lightning, ionospheric disturbances, and other sources of radio frequency (RF) atmospheric noise.
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MEPSI Picosat Nation: USA. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: Aerospace. Agency: DARPA. Perigee: 558 km (346 mi). Apogee: 563 km (349 mi). Inclination: 35.40 deg. Period: 1,436.10 min. COSPAR: 2007-006x. Released from STPSat.
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MEPSI Picosat Nation: USA. Mass: 1.00 kg (2.20 lb). Class: Technology. Spacecraft: Cubesat. Manufacturer: Aerospace. Agency: DARPA. Perigee: 558 km (346 mi). Apogee: 563 km (349 mi). Inclination: 35.40 deg. COSPAR: 2007-006x. Released from STPSat.
2008 - 04:03 GMT - Launch Site: Kourou. Launch Vehicle: Ariane 5. Model: Ariane 5ES. -
Jules Verne ATV Nation: France. Mass: 19,012 kg (41,914 lb). Class: Manned. Type: Logistics. Spacecraft: ESA Automated Transfer Vehicle. Perigee: 336 km (208 mi). Apogee: 343 km (213 mi). Inclination: 51.60 deg. Period: 91.30 min. COSPAR: 2008-008A. USAF Sat Cat: 32686. First launch of Europe's Automated Transfer Vehicle, a logistics vehicle designed for ISS resupply. The Ariane model 5ES launch vehicle, vehicle L528, had the enhanced EAP solid boosters and EPC core stage of the Ariane 5ECA, but with the new EPS-V upper stage with restart capability and a vehicle equipment bay instrument unit strengthened to carry the heavier LEO payload. Jules Verne carried 1300 kg of dry cargo, 302 kg of water and oxygen, and 860 kg of propellant to the ISS. For this test mission it had a dry mass of 10075 kg and 6475 kg of maneuvering propellant (in later missions the propellant could be thousands of kilograms less, in order to deliver more cargo).
The EPS stage made its first burn and placed the stack into a 137 km x 260 km orbit at 04:20 GMT. The EPS restarted at 05:05, burned for 30-seconds, and released the ATV into a 254 km x 272 km orbit.
Born on this day in: - 1934 - Yuri Alekseyevich Gagarin. Russian Pilot Cosmonaut. Birth City: Gzhatsk. Birth State: Smolensk. Birth Country: Russia.
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