| astronautix.com | January 26 |
1946 - Nation: USA.
Army announced creation by AAF of the First Experimental Guided Missiles Group to develop and test rocket missiles at Eglin Field, Fla. References: 17 .
1949 - Nation: USSR.
The 5-2 second aircraft, with rocket engine installed, made its first glide flight.
1952 - Nation: USA.
1954 - Nation: USSR. Launch Vehicle: R-11FM.
Council of Soviet Ministers (SM) Decree 'On approval of work on the R-11FM' was issued. References: 474 .
1956 - Nation: USA.
Symposium on "The Scientific Uses of Earth Satellites" held at the University of Michigan under sponsorship of the Upper Atmosphere Rocket Research Panel, James A. Van Allen of the State University of Iowa, Chairman. References: 17 .
1959 - Nation: USA.
NASA completed contract negotiations with McDonnell for the design and development of the Mercury spacecraft. At that time, McDonnell estimated that the first 3 spacecraft could be delivered in 10 months. Spacecraft refinements slipped this estimated goal by only 2 months. References: 483 .
1960 - Nation: USA. Launch Site: White Sands . Launch Complex: ALA3. Launch Vehicle: Redstone. LV Configuration: Redstone s/n CC-2011.
Successful missile test. Missed aimpoint by 277 m. References: 439 .
1960 - Nation: USA. Launch Site: Vandenberg . Launch Complex: LC576-A. Launch Vehicle: Atlas D. LV Configuration: Atlas 6D. FAILURE: Failure.
1961 - Nation: USA. Launch Vehicle: Saturn I.
Wernher von Braun, Director of Marshall Space Flight Center, proposed that the Saturn C-1 launch vehicle be changed from a three-stage to a two-stage configuration to meet Apollo program schedules. The planned third stage (S-V) would be dropped. References: 16 .
1962 - - 20:30 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC12. Launch Vehicle: Atlas LV-3A / Agena B. LV Configuration: Atlas s/n 121D / Agena B s/n 6003 (AA3). FAILURE: Agena B second stage guidance system failure.
Lunar impact probe; missed the moon by 36,874 km and went into solar orbit. A malfunction in the booster guidance system resulted in excessive spacecraft speed. Reversed command signals caused the telemetry antenna to lose earth acquisition, and mid-course correction was not possible. Some useful data were obtained from the flight. Of four scientific experiments only one was partially completed: gamma-ray readings of the lunar surface. Attempts to relay television pictures of the moon and to bounce radar signals off the moon at close range were unsuccessful. References: 1 , 2 , 5 , 6 , 16 , 278 , 296 .
1963 - Nation: USA.
Specialty assignments were announced by the Manned Spacecraft Center for its astronaut team: L. Gordon Cooper, Alan B. Shepard, pilot phases of Project Mercury; Virgil I. Grissom, Project Gemini; John H. Glenn, Project Apollo; M. Scott Carpenter, lunar excursion training; Walter M. Schirra, Gemini and Apollo operations and training; Donald K. Slayton, remained in duties assigned in September 1962 as Coordinator of Astronaut Activities. These assignments superseded those of July 1959. Assignments of the new flight-crew members selected on September 17, 1962, were as follows: Neil A. Armstrong, trainers and simulators; Frank Borman, boosters; Charles Conrad, cockpit layout and systems integration; James A. Lovell, recovery systems; James A. McDivitt, guidance and navigation; Elliott M. See, electrical, sequential, and mission planning; Thomas P. Stafford, communications, instrumentation, and range integration; Edward H. White, flight control systems; John W. Young, environmental control systems, personal and survival equipment. References: 483 .
1963 - Nation: USA.
MSC announced new assignments for the seven original astronauts: L. Gordon Cooper, Jr., and Alan B. Shepard, Jr., would be responsible for the remaining pilot phases of Project Mercury; Virgil I. Grissom would specialize in Project Gemini; John H. Glenn, Jr., would concentrate on Project Apollo; M. Scott Carpenter would cover lunar excursion training; and Walter M. Schirra, Jr., would be responsible for Gemini and Apollo operations and training. As Coordinator for Astronaut Activities, Donald K. Slayton would maintain overall supervision of astronaut duties.
Specialty areas for the second generation were: trainers and simulators, Neil A. Armstrong; boosters, Frank Borman; cockpit layout and systems integration, Charles Conrad, Jr.; recovery system, James A. Lovell, Jr.; guidance and navigation, James A. McDivitt; electrical, sequential, and mission planning, Elliot M. See, Jr.; communications, instrumentation, and range integration, Thomas P. Stafford; flight control systems, Edward H. White II; and environmental control systems, personal equipment, and survival equipment, John W. Young. References: 16 .
1965 - Nation: USA.
Warren J. North, Chairman of the Lunar Landing Research Vehicle (LLRV) Coordination Panel, reported to MSC Director Robert R. Gilruth that the LLRV had been flown 10 times by Flight Research Center pilots - eight times by Joe Walker and twice by Don Mallick. Maximum altitude achieved was 91 m (300 ft) and maximum forward velocity was 12 m (40 ft) per sec. Additional Details: Apollo Lunar Landing Research Vehicle results. References: 16 .
1967 - Nation: USA.
At a NASA Hq briefing, Associate Administrator for Manned Space Flight George E. Mueller stated that NASA planned to form an 'embryonic space station' in 1968-69 by clustering four AAP payloads launched at different times. The first mission would be the launch of a manned spacecraft followed several days later by a spent S-IVB stage converted into an OWS. After the two spacecraft had docked, the crew would enter the Workshop through an airlock. Twenty-eight days later they would passivate the OWS and return to Earth in their spacecraft. In three to six months, a second manned spacecraft would be launched on a 56-day mission to deliver a resupply module to the OWS and to rendezvous with an unmanned ATM, the fourth and last launch of the series. The cluster would be joined together using the multiple docking adapter. Emphasizing the importance of manning the ATM, Mueller said that 'if there is one thing the scientific community is agreed on it is that when you want to have a major telescope instrument in space it needs to be manned.'
1967 - - 17:32 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC2E. Launch Vehicle: Delta E. LV Configuration: Thor Delta E s/n 472 / Delta s/n 45.
Replaced ESSA 2. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1970 - Nation: USA.
Maximum Speed - 1443 kph. Maximum Altitude - 26730 m. Flight Time - 411 sec. References: 49 , 97 .
1971 - - 00:36 GMT. Nation: International. Launch Site: Cape Canaveral . Launch Complex: LC36A. Launch Vehicle: Atlas Centaur SLV-3C. LV Configuration: Atlas SLV-3C s/n AC-25 / Centaur D-1A s/n 5005C.
Stationed at 24.5 deg W. 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 References: 1 , 2 , 5 , 6 , 278 .
1971 - - 12:45 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 .
1973 - Nation: USA.
Ames Research Center requested that six R4D rocket engines designed for use in the Apollo program be transferred from MSC to Ames. Possibly the engines would be suitable for the retro-injection function in the Pioneer Venus series of atmospheric probe and orbiter missions. First launch was planned for early 1977. References: 16 .
1973 - Nation: USA.
MSFC Director Eberhard F. M. Rees retired. He had served as Director since 1 March 1970. Rocco A. Petrone, NASA Apollo Program Director, became the new MSFC Director.
1973 - - 06:14 GMT. Nation: USSR. Launch Site: Kapustin Yar . Launch Complex: LC107. Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n Yu149-37.
Investigation of the upper atmosphere and outer space. References: 1 , 2 , 5 , 6 .
1978 - - 04:57 GMT. Nation: China. Launch Site: Jiuquan . Launch Complex: LA2. Launch Vehicle: CZ-2C. LV Configuration: Chang Zheng 2C s/n CZ2C-3.
Photo surveillance; film capsule; capsule returned 1/30. References: 1 , 2 , 5 , 6 .
1978 - - 17:36 GMT. Nation: USA. Launch Site: Cape Canaveral . Launch Complex: LC17A. Launch Vehicle: Delta 2914. LV Configuration: Delta 2914 s/n 628 / Delta s/n 138.
International Ultraviolet Explorer. Spacecraft engaged in practical applications and uses of space technology such as weather or communication (US Cat C). References: 1 , 2 , 5 , 6 .
1983 - - 02:17 GMT. Nation: USA. Launch Site: Vandenberg . Launch Complex: SLC2W. Launch Vehicle: Delta 3914. LV Configuration: Delta 3910 s/n 650 / Delta s/n 166.
All-sky survey of astronomical IR bodies. Spacecraft engaged in research and exploration of the upper atmosphere or outer space (US Cat B). References: 1 , 2 , 5 , 6 .
1984 - - 08:52 GMT. Nation: USSR. Launch Site: Baikonur . Launch Vehicle: Soyuz 11A511U.
Photo surveillance; returned film capsule. References: 1 , 2 , 6 .
1984 - - 12:00 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 53793-469.
Radar calibration mission. References: 1 , 2 , 5 , 6 .
1988 - - 11:16 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Soyuz 11A511U.
Military cartographic satellite; returned film capsule. References: 1 , 2 , 6 .
1989 - - 09:16 GMT. Nation: USSR. Launch Site: Baikonur . Launch Complex: LC200P. Launch Vehicle: Proton 8K82K / 11S861. LV Configuration: Proton 8K82K s/n 351-02 / 11S861 s/n 20L.
Stationed at 53 deg E. Provision of telephone and telegraph radiocommunications and television broadcasting. Satellite sold to Rimsat Corporation in June 1993. References: 1 , 2 , 5 , 6 , 67 , 111 , 274 .
1989 - - 15:50 GMT. Nation: USSR. Launch Site: Plesetsk . Launch Vehicle: Kosmos 11K65M. LV Configuration: Kosmos 11K65M s/n 65079-812.
1990 - Nation: USSR.
Tested spacesuit. Examined exterior of Kvant 2. References: 66 .
1991 - Nation: USSR.
Installed solar array supports. References: 66 .
1993 - - 14:24 GMT. Nation: Russia. Launch Site: Plesetsk . Launch Complex: LC16/2. Launch Vehicle: Molniya 8K78M. LV Configuration: Molniya 8K78M / 2BL.
Covered Oko constellation plane 4 - 34 degree longitude of ascending node. References: 1 , 2 , 5 , 6 , 100 .
1994 - - 02:24 GMT. Nation: Russia. Launch Site: Baikonur . Launch Complex: LC1. Launch Vehicle: Soyuz 11A511U. LV Configuration: Soyuz 11A511U s/n N15000-635.
Unmanned resupply vessel to Mir. Docked with Mir on 30 Jan 1994 03:56:13 GMT. Undocked on 23 Mar 1994 01:20:29 GMT. Destroyed in reentry on 23 Mar 1994 05:13:00 GMT. Total free-flight time 2.23 days. Total docked time 51.89 days. References: 1 , 2 , 6 , 275 .