Episodes Tagged with "Holmes"
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
Posted on April 30, 2015
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 28, 2015
VonBraunMuellerReesSA6
SA5_launch
sa-6-spacecraft
sa-6-dem
SA-6 spacecraft and launch vehicle ready to go
SA-6 on pad
SA-5Section cuts
SA-5
SA-5 S-IV stage
SA-5 on pad
SA-5 Demensions
apollo_sa7_launch
apollo_sa4
Posted on June 11, 2015
6-NASA engineers in 1964 decided that astronauts could stand in the lunar module cabin during the trip to the lunar surface. Note triangular windows
7-Proposed sleeping positions for astronauts on the moon
5-Mockup of lunar module cabin with seats
4-The drawing of the stage indicates positions of components
3-underside of the lunar module descent stage shows fuel tank installation
2-Administrator James Webb examines models of the lunar and command modules in docked position
1-Lunar module generations from 1962 (above left; the vehicle originally proposed by Grumman) to 1969
Posted on July 16, 2015
4- Saturn_SA10_launch
Saturn_SA8_launch
2- The SA-9
8- Pegasus_Deployment_sequence
7- Cutaway views show the interior of the command module (for clarity, the center couch is not shown)
6- Pegasus Deployed
5- Pegasus Stowed
4- Saturn_SA10_launch
Posted on August 20, 2015
AS-203_launch
AS-202_launch
AS-201_launch
Apollo-Saturn 201 mission – launch, recovery
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
