American test pilot astronaut 1978-1989. Heavyset Navy pilot with a talent for playing to a crowd. Flew 64 combat missions in Vietnam. Later ran in, but lost, the Republican primary for governor of West Virginia. 1 spaceflight, 8.2 days in space. Flew to orbit on STS-41G (1984).
Titan missile B-5, scheduled to be the first fully powered-flight test missile, was heavily damaged when a faulty release mechanism allowed an earlier-than-planned liftoff that resulted in engine shutdown and the missile's dropping back on the launch pad.
North American began flight tests of the half-scale vehicle (HSTV) in Phase II-A of the Paraglider Development Program two months behind schedule. The instrumented HSTV with the paraglider predeployed was towed aloft by helicopter. Objectives of the predeployed flights were to evaluate flight performance, longitudinal and lateral control characteristics, effectiveness of control, and the flare maneuver capability of the paraglider. Despite various minor malfunctions in all five test flights (August 14, 17, 23, September 17, and October 23, 1962), test results verified the stability of the wing/vehicle combination in free flight and the adequacy of control effectiveness.
The NAA spacecraft Statement of Work was revised to include the requirements for the lunar excursion module (LEM) as well as other modifications. The LEM requirements were identical with those given in the LEM Development Statement of Work of July 24.
The command module (CM) would now be required to provide the crew with a one-day habitable environment and a survival environment for one week after touching down on land or water. In case of a landing at sea, the CM should be able to recover from any attitude and float upright with egress hatches free of water. Additional Details: here....
NASA Administrator James E. Webb signed the definitive contract with North American for the development of the Apollo CSM. This followed by almost two years North American's selection as prime contractor, The $938.4 million cost-plus-fixed-fee agreement was the most valuable single research and development contract in American history. The contract called for the initial production (i.e., through May 15, 1965) of 11 mockups, 15 boilerplate vehicles, and 11 production articles.
The first Atlas/Agena D standard launch vehicle (SLV-3, 7100 Series) was successfully launched from Vandenberg AFB. This vehicle, Number 7101, was the first Atlas booster to be designed and produced to fully standardized specifications. KH-7 type satellite. Space craft engaged in investigation of spaceflight techniques and technology (US Cat A).
During a key meeting of Apollo senior figures - top NASA management first approached regarding an Apollo 8 lunar mission in December - reaction: negative. Participants in the August 14 meeting in Washington were Low, Gilruth, Kraft, and Slayton from MSC; von Braun, James, and Richard from MSFC; Debus and Petrone from KSC; and Deputy Administrator Thomas Paine, William Schneider, Julian Bowman, Phillips, and Hage from NASA Hq. Low reviewed the spacecraft aspects; Kraft, flight operations; and Slayton, flight crew support. MSFC had agreed on the LTA-B as the substitute and were still ready to go; and KSC said they would be ready by December 6. Additional Details: here....
He solicited their support in the reorganization and new projects for the bureau. Glushko was sartorially perfect, and had an aristocratic air, never using the familiar forms of address in Russian. He only loosened up a little in the last years of his life. He was a nitpicker, correcting Russian syntax in documents. He was capable of clear logic but did not have the intuitive genius of Korolev (according to Barmin, while Korolev did not look after his appearance, he possessed a pure 'Russian' intelligence).
Transport of various cargoes to the Salyut-7 orbital station. Docked with Salyut 7 on 16 Aug 1984 08:11:00 GMT. Undocked on 26 Aug 1984 16:13:00 GMT. Destroyed in reentry on 28 Aug 1984 01:28:00 GMT. Total free-flight time 3.46 days. Total docked time 10.33 days.
International communications; 14.5 deg W. Positioned in geosynchronous orbit at 24 deg W in 1991-1997; 27 deg W in 1997-1999 As of 2 September 2001 located at 27.48 deg W drifting at 0.015 deg W per day. As of 2007 Mar 10 located at 174.03E drifting at 0.000W degrees per day.
Geosynchronous ballistic missile early warning satellite. Positioned in geosynchronous orbit at 23 deg W in 1997-1999 As of 4 September 2001 located at 142.44 deg E drifting at 0.028 deg E per day. As of 2007 Mar 9 located at 66.03W drifting at 0.329E degrees per day.
Following a mission that seemed to consist of an endless series of collisions, breakdowns, fires, and other emergencies, the EO-23 crew handed over the station to EO-24 and on August 14 entered Soyuz TM-25 landed in Kazakstan at 12:17 UTC, 170 km SE of Dzezkazgan. The Soyuz landing rockets failed to fire on touchdown, giving one of the roughest landings experienced by a returning Mir crew.
Discovery's crewmembers, including their new Expedition Two crewmates from the International Space Station, were awakened at 4:10 a.m. Central time to the theme from the movie, "Arthur", to begin a day highlighted by the transfer of equipment and supplies to the station from Discovery and from the pressurized cargo carrier the shuttle brought into space. Additional Details: here....
First USAF Advanced EHF communications satellite. Placed in an initial 221 x 50179 km x 22.2 deg geosynchronous transfer orbit by the Atlas Centaur upper stage. However the satellite's main BT-4 engine failed, meaning the secondary hydrazine thrusters were used to much more satellite raise the spacecraft to geosynchronous orbit.
JCSAT-16 satellite for Sky Perfect JSAT, a Japanese satellite broadcasting company. The second stage put JCSAT-16 in geostationary transfer orbit, while the first stage completed a ballistic trajectory and landed on the droneship 'Of Course I Still Love You' in the Atlantic. After its first orbit raising burn, JCSAT-16 was in a 5581 x 35905 km x 10.8 deg orbit. The Falcon 9 second stage was in an 82 x 34111 km geotransfer orbit, ensuring quick orbital decay.
See OSIRIS-3U ↑. 3U cubesat by Pennsylvania State University SSPL. Mission: In situ measurements of temporal and spatial characteristics of ionospheric space weather. Constellation of three 1U spacecraft launched simultaneously.