Episodes Tagged with "General Electric"
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
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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 May 7, 2015
General Electric employees monitor activities of a spacecraft test in the automatic-checkout-equipment spacecraft control room in 1965
comparison of spacecraft and launch vehicle configuration
Apollo tracking network in 1966. Radar stations with large antennas for continuous tracking and communications were at Goldstone, California; Madrid, Spain; and Canberra, Australia
Posted on May 14, 2015
Full-scale model of the command module, above- the strake aerodynamic devices may be seen at either side of the spacecraft just above the aft heatshield
Removing LM from S=IVB stage
On 16 November 1963 in Cape Canaveral’s Blockhouse 37, NASA’s new manned space flight chief George Mueller
Communications with the moon as the earth turned. Astronauts on the moon’s surface also could talk to one another
Posted on May 21, 2015
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The cabin section (or primary structure) of the CM is assembled at North American in 1965
The CM probe would slip into the LM’s dish-shaped drogue, and 12 latches on the docking ring would engage, to lock the spacecraft together, airtight
Full-scale model of the service module, resting on a mockup of a spacecraft-lunar module adapter, with panels off to reveal part of the internal arrangement
Jettison of the launch escape system (right) after successful launch, also pulls away the boost protective cover that protects the windows from flame and soot
On the drawing of the launch escape system at upper right, the canard aerodynamic devices are near the top of the escape tower
Posted on May 19, 2016
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Posted on August 21, 2014
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