| astronautix.com | February 05 |
1946 - Nation: USA.
Bell flight 2. At Pinecastle AAF, Florida. References: 49 , 97 .
1946 - Nation: USA.
Bell flight 3. At Pinecastle AAF, Florida. References: 49 , 97 .
1947 - Nation: USA.
1947 - Nation: USA.
Bell flight 13. Machmeter calibration. References: 49 , 97 .
1955 - Nation: USSR. Launch Vehicle: R-1.
1958 - - 07:33 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC18A. Launch Vehicle: Vanguard. LV Configuration: Vanguard s/n TV-3BU. FAILURE: Control system malfunction - control lost after 57 sec.
Trial firing of IGY Vanguard (TV-3Bu) satellite. References: 5 , 126 .
1959 - Nation: USA.
A Working Group on Lunar Exploration was established by NASA at a meeting at Jet Propulsion Laboratory (JPL). Members of NASA, JPL, Army Ballistic Missile Agency, California Institute of Technology, and the University of California participated in the meeting. The Working Group was assigned the responsibility of preparing a lunar exploration program, which was outlined: circumlunar vehicles, unmanned and manned; hard lunar impact; close lunar satellites; soft lunar landings (instrumented). Preliminary studies showed that the Saturn booster with an intercontinental ballistic missile as a second stage and a Centaur as a third stage, would be capable of launching manned lunar circumnavigation spacecraft and instrumented packages of about one ton to a soft landing on the moon. References: 16 .
1960 - Nation: USSR. Launch Vehicle: Burya.
Decree 138-48 'On termination of work on the La-350 Burya at OKB-301' was issued. Project finally cancelled based on availability and invulnerability of R-7, R-9, and R-16 ICBM's. Flight test for technology purposes of already-built missiles was allowed to the end of the year. References: 474 .
1965 - Nation: USA.
SM 001's service propulsion engine was static-fired for 10 sec at White Sands. The firing was the first in a program to verify the mission profiles for later flight tests of the module. (SM 001 was the first major piece of flight-weight Apollo hardware.) References: 16 .
1966 - Nation: USSR. Launch Site: Baikonur . Launch Complex: LC67. Launch Vehicle: R-36-O.
1967 - - 01:17 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC13. Launch Vehicle: SLV-3 Atlas / Agena D. LV Configuration: Atlas s/n 5803 / Agena D s/n 6632.
Crashed into Moon; returned 182 photos of lunar surface. Selenocentric orbit. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 1 , 2 , 5 , 6 , 278 .
1969 - - 21:59 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC3W. Launch Vehicle: LT Thor Agena D. LV Configuration: Thorad 2L s/n 519 / Agena D s/n 1650.
KH-4B. The best image quality to date. References: 1 , 2 , 5 , 6 .
ABM monitoring. References: 1 , 2 , 5 , 6 , 172 .
1971 - Nation: USA.
Explored lunar surface near LM and deployed ALSEP unmanned scientific station equipment. References: 66 .
1975 - - 13:12 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC132. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53753-212.
Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 .
1976 - - 14:30 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Complex: LC133/1. Launch Vehicle: Kosmos 11K63.
Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 , 99 .
1981 - Nation: Russia. Launch Vehicle: Energia.
NPO Energia developed for the Ministry of Defence the interorbital tug Gerkules with 550 kW maximum output and continuous operation in the 50-150 kW range for 3 to 5 years. In 1986 an interorbital tug was studied to solve the specific application of transporting heavy satellites of 100 tonnes to geostationary orbit, launched by Energia.
1982 - - 09:12 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC200P. Launch Vehicle: Proton 8K82K / 11S86. LV Configuration: Proton 8K82K s/n 308-01 / 11S86 .
Transmission of Central Television programmes to a network of receivers for collective use. References: 1 , 2 , 5 , 6 , 67 , 274 .
1984 - - 18:44 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC3E. Launch Vehicle: Atlas H. LV Configuration: Atlas s/n 69F / 6003H.
Deployed from NOSS 6. References: 1 , 2 , 5 , 6 , 278 .
Deployed from NOSS 6. References: 1 , 2 , 5 , 6 , 278 .
Ocean surveillance; aka White Cloud type spacecraft; Navy Ocean Surveillance Satellite; PARCAE. References: 1 , 2 , 5 , 6 , 172 , 278 .
1987 - - 06:43 GMT. Nation: Japan. Launch Site: Kagoshima . Launch Complex: M. Launch Vehicle: Mu-3S. LV Configuration: Mu-3S-II s/n M-3S2-3.
Studyied galactic gamma ray, X-ray sources. ASTRO-C (Ginga). Observation of variabilities of X-rays from active galactic nuclei and galactic compact sources. Launching organization ISAS. Launch time 0630 GMT. References: 1 , 2 , 5 , 6 .
1987 - - 21:38 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U2.
Mir Expedition EO-02. Docked with Mir 7 February 1987. Carried Yuri Romanenko, Aleksander Laveykin to Mir; returned Laveykin, crew of Soyuz TM-3 to Earth. Undocked from Mir 8:34 GMT 29 July. Orbital Module left in a 308 X 356 orbit. Recovered July 30, 1987 01:54 GMT. References: 1 , 2 , 6 , 32 , 51 .
1990 - Nation: USSR.
Viktorenko tested SPK manoeuvring unit. References: 66 .
1991 - - 04:48 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 47148-407.
Civilian navigation satellite. Positioned in plane 13 of constellation. Testing of components and equipment of a space navigation system being set up to determine the position of civil aircraft and ships of the USSR merchant marine and fishing fleet at any point on the oceans and seas. References: 1 , 2 , 5 , 6 , 107 .
1992 - Nation: Russia. Launch Site: Baikonur . Launch Complex: LC45L. Launch Vehicle: Zenit-2. FAILURE: Second stage malfunction due to heating problems in main engine.
1994 - - 08:46 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC81L. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 375-02 / 11S861 s/n 83L.
Stationed at 48 deg E; third launch of alternate Raduga design. Extension of the telephone and telegraph radio communications system on the territory of the Russian Federation. References: 1 , 2 , 5 , 6 , 67 , 274 .
1996 - - 07:19 GMT. Nation: Japan. Launch Site: Kourou . Launch Complex: ELA2. Launch Vehicle: Ariane 44P. LV Configuration: Ariane 44P s/n V83.
Geostationary at 128.9E. References: 4 , 6 .