Episodes Tagged with "Saturn C 3"
Posted on February 26, 2015
John_Houbolt_and_LOR2
Earth Orbit Rendezvous
Apollo_Direct_Ascent
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 March 12, 2015
Lifting the first stage from the transporter
Hoisting the stage in vertical attitude
Erecting the upper stages
Early design concepts of C-1 and C-5 versions of the Saturn launch vehicles
16-Unloading Compromise in Florida
15-S-I and S-IV stages aboard the Compromise
14-Booster movement around Wheeler Dam
11-Launch Complex 34
10-Configurations of Saturn flight vehicles
9-Saturn Barge route
7-Six-engine configuration of the S-IV stage
6-Redesigned tail of the Saturn booster
5- The barge Palaemon
3-First horizontal mating of the Saturn vehicle
2-Movement of dummy S-IV stage to checkout
Posted on March 18, 2015
To assemble the large Saturns, NASA needed a plant, preferably one already built. The Michoud facility (above), close to New Orleans, suited the requirements
Saturn_SA1_on_launch_pad
Modules of the Apollo spacecraft were tested in Florida in the Manned Spacecraft Operations Building. Above, NASA officials Walt Williams, Merritt Preston, Kurt Debus, Brainerd Holmes, and Wernher von Braun
Maiden launch of the Apollo program- Saturn SA-1 from Cape Canaveral, 27 October 1961
First Saturn Launch
Liftoff of Saturn I. Note the long cable mast falling away on the right
mySuperLamePic_c001b3d7f61bec278243523bf2e79253
Abe Silverstein, NASA’s Director of Space Flight Development, is shown touring a rocket engine facility
1-Launch Complex 34, blockhouse interior
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 January 30, 2014
The operating principle of the fuel cell designed by General Electric, adopted for use in the Gemini spacecraft
modified Titan II booster
Gemini spacecraft to be released publicly
Adapter Section of Mark II
Four stages in a rendezvous mission as conceived early in 1962
An artist’s version of the use of ejection seats to escape from the Gemini spacecraft
fig8 proposed lunar lander to be used with an advanced version of the Mercury spacecraft
