Episodes Tagged with "Space Task Group"
Posted on February 12, 2015
Using a model at upper left, William Rector of General Dynamics Corp. describes the design his company proposed for the Apollo lunar mission
Spacecraft modules in this drawing were identified in the Space Task Group’s request for proposals from contractors for developing and producing the command module
Saturn 1 test
Saturn 1 test 2
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At lower left, E. E. Clark and Carlos de Moraes of the Martin Company display three of a dozen command module configurations considered before the choice of the one to the right
ASA’s second Administrator, James E. Webb (at center above), and George M. Low (right above) of NASA Headquarters receive a model of General Electric’s proposed vehicle
Posted on February 19, 2015
David G. Hoag, technical design director at the laboratory, examines the inertial measuring unit that would measure changes in Apollo spacecraft velocity when propulsion systems were fired
MIT Instrumentation Laboratory Director C. Stark Draper inspects a mockup of the Apollo guidance and control system in the September 1963
astronaut positions
Posted on February 26, 2015
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Earth Orbit Rendezvous
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Posted on March 26, 2015
two landing techniques proposed for the direct ascent mode
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proposed lunar-surface-rendezvous procedure, a propellant-transfer vehicle takes fuel from the tanker to a manned space vehicle. After loading the fuel, the two astronauts would fire the engine of their spacecraft to return to the earth
Major configuration changes in the Apollo spacecraft from May 1960 to July 1962
Early design concepts of C-1 and C-5 versions of the Saturn launch vehicles
A ferry that would leave a command ship in orbit around the moon, visit the lunar surface, and then return to the command ship for the voyage back to the earth
Posted on April 2, 2015
Early design concepts of C-1 and C-5 versions of the Saturn launch vehicles
NASA announced selection of the lunar-orbit-rendezvous landing technique at an 11 July 1962 press conference. left to right James E. Webb, Robert C. Seamans, Jr., D. Brainerd Holmes, and Joseph F. Shea
Harry C. Shoaf (Space Task Group Engineering Division 15 November 1961 of a proposed lunar lander to be used with an advanced version of the Mercury spacecraft
concept of a small lunar lander during descent to the surface of the moon, as proposed by Langley Research Center employees in October 1961
Posted on April 9, 2015
Shea uses models to demonstrate how the lunar module would dock with the command module
Rocket Comparison
Lunar orbit insertion
Posted on July 30, 2015
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2-Back row- See, McDivitt, Lovell, White, & Stafford. Front row- Conrad, Borman, Armstrong, & Young
1- Project_Mercury_AstronautsBack row- Shepard, Grissom, Cooper; front row- Schirra, Slayton, Glenn, Carpenter.
Posted on August 5, 2015
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4-Group 4 L-R- Garriott, Gibson. Front row, L-R- Michel, Schmitt, Kerwin.
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Posted on August 13, 2015
5-Back row, from L-R- Swigert, Pogue, Evans, Weitz, Irwin, Carr, Roosa, Worden, Mattingly, Lousma. Front row, from L-R- Givens, Mitchell, Duke, Lind, Haise, Engle, Brand, Bull, McCandless
Posted on August 27, 2015
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2-Wally Schirra (right) consults the flight plan for his Mercury-Atlas-8 (MA-8) mission with Flight Director Chris Kraft
1-Chris Kraft and Rober Gilruth
Posted on September 3, 2015
3-Robert F. Thompson (center) and Christopher C. Kraft Jr. (right) brief Rear Admiral W.C. Abhau
2-Kraft with his new flight directors before the Gemini 4 mission Clockwise from lower right Kraft, Gene Kranz, Glynn Lunney and John Hodge
1-Kraft Kranz Gemini Fuel Cell problem
Posted on September 10, 2015
3-Kranz and his teacher Kraft
2-Kranz at his console on May 30, 1965, in the Mission Operations Control Room, Mission Control Center, Houston
1-Kranz-F86 Sabre Cat
Posted on June 13, 2013
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Posted on August 29, 2013
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Mercury_4_Hatch
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Posted on January 23, 2014
fig6 (1)McDonnell-proposed two-man Mercury spacecraft. Shown is the interior arrangement of spacecraft equipment
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Posted on January 30, 2014
The operating principle of the fuel cell designed by General Electric, adopted for use in the Gemini spacecraft
modified Titan II booster
Gemini spacecraft to be released publicly
Adapter Section of Mark II
Four stages in a rendezvous mission as conceived early in 1962
An artist’s version of the use of ejection seats to escape from the Gemini spacecraft
fig8 proposed lunar lander to be used with an advanced version of the Mercury spacecraft
Posted on January 29, 2015
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Posted on February 5, 2015
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