Episodes Tagged with "Webb"
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
mySuperLamePic_c1194b7fa9498eb5af694d8530d3ebf8
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 May 12, 2016
OwenMaynardStepstotheMoon
chief of the LEM engineering office in the Apollo Program Office in Houston, TexasJPG
3-GeorgeLow
Posted on May 19, 2016
IMG_0988
3-GEMueller
1-Samuel_C._Phillips
Posted on May 26, 2016
3-Jim_Lovell_official
2-William_Anders
1-Frank_Borman
Posted on August 22, 2013
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413px-John_F._Kennedy_speaks_at_Rice_University
Posted on February 6, 2014
The general arrangement of liquid rocket systems (OAMS and RCS) in the Gemini spacecraft
Gemini landing gear part of the land landing system along with the paraglider
fig41The B. F. Goodrich partial-wear full-pressure suit being developed for the Gemini program
fig33Figure 33. The emergency parachute recovery system for the half-scale paraglider flight test vehicle for Phase II-A of the development program – Copy
fig27Gemini spacecraft nomenclature – Copy
Agena B
Posted on February 12, 2014
fig58 Astronauts after a training session in desert near Stead Air Force Base, Nevada
Goal
fig54 Instrumented mannequin being lowered into a boilerplate Gemini spacecraft in preparation for a dynamic sled test of the Gemini ejection system
fig52 Gemini launch vehicle 1 undergoing tests in the vertical test facility at Martin’s Baltimore plant
fig51 POGO suppression equipment proved out in the Titan II development program
fig48 Proposed deployment sequence for the ballute stabilization device
fig47 Titan II flight N-15 was launched from Cape Canaveral on January 10, 1963
