| astronautix.com | July 10 |
1947 - Nation: USA. Launch Site: White Sands . Launch Complex: LC33. Launch Vehicle: V-2. LV Configuration: V-2 number 29.
Launched 12:18 local time. Reached 16.1 km. Carried cosmic radiation, pressure, temperature, ionosphere, biological (Harvard) experiments for Naval Research Lab.
1950 - Nation: USA. Launch Vehicle: Redstone.
Office, Chief of Ordnance directed that the Ordnance Guided Missile Center conduct a preliminary study of the technical requirements and possibilities of developing a 500-mile tactical missile that would be used principally in providing support for the operations of the Army Field Forces.
1950 - Nation: UK.
1951 - Nation: USA. Launch Vehicle: Redstone.
The Office, Chief of Ordnance formally transferred the responsibility for conducting the research and development phase of the HERMES Cl project to Redstone Arsenal
1958 - Nation: USA. Launch Site: Cape Canaveral . Launch Vehicle: Thor Able. LV Configuration: Thor-DM18 / Able.
Suborbital. Mouse 'Mia II' reached 1600 km altitude, flew 9600 km range, but re-entry vehicle not recovered. References: 5 .
1959 - Nation: USSR. Launch Vehicle: R-2.
1962 - Nation: USA.
The first Apollo spacecraft mockup inspection was held at NAA's Space and Information Systems Division. In attendance were Robert R. Gilruth, Director, MSC; Charles W. Frick, Apollo Program Manager, MSC; and Astronaut Virgil I. Grissom. References: 16 .
1962 - - 08:35 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17B. Launch Vehicle: Delta. LV Configuration: Thor Delta s/n 316 / Delta s/n 11.
First commercial comsat; active repeater. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1963 - Nation: USA.
The Marquardt Corporation began testing the prototype engine for the SM reaction control system. Preliminary data showed a specific impulse slightly less than 300 seconds. References: 16 .
1963 - Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Vostok 8A92. FAILURE: Shutdown of Block B strap-on engine stage 1.9 seconds after liftoff. Pad damaged.
Area survey photo reconnaissance satellite. References: 93 .
1964 - - 23:15 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: LC1-1. Launch Vehicle: TA Thor Agena D. LV Configuration: Thor 2C s/n 404 / Agena D s/n 1177.
KH-4A. Cameras operated satisfactorily, some light leaks. References: 1 , 2 , 5 , 6 .
1966 - Nation: USSR.
Komarov announces in Japan that USSR would beat the US to moonlanding by one year. References: 72 .
1968 - - 19:50 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC31. Launch Vehicle: Voskhod 11A57.
Area survey photo reconnaissance satellite. References: 1 , 2 , 6 , 93 .
1969 - - 09:07 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Voskhod 11A57.
High resolution photo reconnaissance satellite; returned film capsule References: 1 , 2 , 6 .
1972 - - 16:19 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC132. Launch Vehicle: Kosmos 11K65M.
Possible navigation satellite. Replaced Cosmos 425. References: 1 , 2 , 5 , 6 .
1979 - - 09:07 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
High resolution photo reconnaissance satellite; returned film capsule; maneuverable. References: 1 , 2 , 6 .
1981 - - 05:16 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Vostok 8A92M.
Also performed earth resources tasks. Acquisition of information required for continued investigation of the natural resources of the earth; development of remote sensing methods for measuring the parameters of the atmosphere and the earth's surface beneath the satellite. Carried scientific i nstruments developed in the People's Republic of Bulgaria, as well as Soviet equipment. Objects 1595 and 1596 launched by a single rocket. References: 1 , 2 , 6 .
Launched from Salyut 7 airlock. Conduct of scientific experiments to study diffusion and heat processes in weightlessness. References: 1 , 2 , 6 .
1982 - - 19:58 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n Shch15000-318.
Unmanned supply vessel to Salyut 7. Docked with Salyut 7 on 12 Jul 1982 11:41:00 GMT. Undocked on 10 Aug 1982 22:11:00 GMT. Destroyed in reentry on 13 Aug 1982 01:29:00 GMT. Total free-flight time 4.21 days. Total docked time 29.44 days. References: 1 , 2 , 6 , 275 .
1985 - - 03:21 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC41/1. Launch Vehicle: Soyuz 11A511U.
Biological research. Carried monkeys Verniy and Gordiy. Continued investigations of the influence of space flight factors on living organisms and radiation physics research. Cosmos 1667 was the second USSR biosatellite mission with a primate payload. Cosmos 1667 also featured a large rodent payload, however the U.S. only conducted a single experiment cardiovascular experiment on one of the two flight monkeys. Mission parameters were very similar to those of Cosmos 1514. Countries participating in the mission included the USSR, U.S., France, Czechoslovakia, the German Democratic Republic, Poland, Romania, Bulgaria and Hungary. Additional Details: Cosmos 1667. References: 1 , 2 , 6 , 104 , 297 .
1987 - - 15:21 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC90. Launch Vehicle: Tsyklon 2.
Ocean surveillance; nuclear powered. - Tested Plasma-2 SPT electric engine. References: 1 , 2 , 5 , 6 .
1991 - - 13:55 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U2.
Photo/digital surveillance. References: 1 , 2 , 6 .
1992 - - 22:42 GMT. Nation: Europe. Launch Site: Kourou . Launch Complex: ELA2. Launch Vehicle: Ariane 44L. LV Configuration: Ariane 44L s/n V51.
Stationed at 7 deg E. References: 2 , 5 , 6 .
Stationed at 74 deg E; also performed communications functions. INSAT-2A is a multi-purpose satellite, and it will provide the following services: Domestic long-distance telecommunications, meteorological earth observation and data collection services, direct satellite TV broadcasting to community TV receivers in rura l and remote areas, radio and TV progamme distribution, and Satellite Aided Search and Rescue services. Geostationary longitude 74 +/0 0.1 deg E. References: 1 , 2 , 5 , 6 .
1995 - - 12:38 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC41. Launch Vehicle: Titan 4. LV Configuration: Titan 401A / Centaur G s/n K-19 (45E-5).
1998 - - 06:30 GMT. Nation: Australia. Launch Site: Baikonur . Launch Complex: LC45. Launch Vehicle: Zenit-2.
Formerly known as WPLTN-1, this geodesy satellite was a copy of Potsdam's GFZ-1 satellite, a sphere covered with laser retroreflectors, with a different `Fizeau' corner cube design. It serves as a target for the Western Pacific Laser Tracking Network (WPLTN) and is a joint project of Electro Optic Systems of Queanbeyan, New South Wales, Australia, and the Russian Space Agency. Diameter is 0.24m.
Customer: Chilean Air Force (FACH). Chile's second satellite carrying store and forward and Earth observation payloads, replacing those lost on FASat-Alpha. Still operational as of 2000. Additional Details: Fasat-Bravo.
In addition to its remote sensing equipment, the satellite carried the Belgian LLMS (Little LEO Messaging System) communications payload for the IRIS system. The launch was critical in restoring confidence in the Zenit vehicle prior to planned commercial launches of Globalstar satellites from Baikonur and the first Sea Launch flights using a three-stage Zenit from a California-based floating launch platform. Expected life 3 to 5 years.
Customer: Thailand (Thai Microsatellite Company and MUT). Thailand's first microsatellite built through a technology transfer programme with Surrey Satellite Technology Ltd. Carried store and forward and Earth observation payloads. Still operational as of 2000. Additional Details: TMSAT.
Relay satellite built by OHB System of Bremen.
Built by Technion-Israel Institute of Technology. Replaced earlier Russian-launched Techsat which failed to orbit in 1995.
1999 - - 08:45 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: SLC17B. Launch Vehicle: Delta 7925. LV Configuration: Delta 7420 s/n D272.