Episodes Tagged with "Direct Ascent"
Posted on March 26, 2015
two landing techniques proposed for the direct ascent mode
SA-1
RendezvousMethods
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 April 16, 2015
REF: 2-903-6 SA-2 LAUNCH AT CAPE. IGNITION OF ROCKET (SATURN 1 VEHICLE)
SA-2 erected on launch pedestal
Wernher_von_Braun_confers_with_Brainerd_Holmes_and_Nicholas_Golovin
Posted on April 23, 2015
The impact facility at North American was used to drop-test the CM
Selection of Little Joe II completed the Apollo family of launch vehicles.
Scott Carpenter, John Glenn, and Walter Schirra in 1963 inspect a full-scale mock up of the Apollo CM
North American Aviation Stormy,
Interior of a partial full-scale mockup of the Apollo command module
major parts of the command module structure
