Episodes Tagged with "Rocketdyne"
Posted on March 5, 2015
12-Second stage (S-IV)
11-Booster stage (S-I)
10-Proposed C-2
9-C-1 and earlier vehicles
8-Model of blockhouse at Launch Complex 34
7-Vehicles using Titan and Atlas stages
6-Saturn C
5-Saturn B
4-Preliminary concept of Launch Complex 34, Cape Canaveral
3-Early H-1 Engine
2-Thor-Jupiter engine
1-Proposed configuration of a clustered booster
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 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 August 20, 2015
AS-203_launch
AS-202_launch
AS-201_launch
Apollo-Saturn 201 mission – launch, recovery
Posted on February 25, 2016
5-Apollo-6-1968-04-04
4-Apollo 6’s interstage falling away
3-Apollo6fireyExhaustPlume
2-Apollo_6_launch
1-The Lunar Module Test Article (LTA-2R) is being moved for mating with the spacecraft Lunar Module Adapter
0-apollo-6-final_0
Posted on March 16, 2016
3-Scientist observing lunar tort
2-Zond-5 has delivered two tortoises back to the Earth
1-Zond 5 Makes Lunar Round-Trip
Posted on May 4, 2016
3-Zond 6 Double-dip reentry
2-Zond 6 Mission Profile
1-Proton-K with 7K-L1
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 January 29, 2015
c012a
GilruthThompsonGlennan
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