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Episodes Tagged with "Saturn C 3"

Posted on February 26, 2015

Max Faget thought the first stage of the moon rocket should use four solid-fueled engines, 6.6 meters in diameter.  He reasoned these could certainly accomplish whatever mission was required of either the Saturn or Nova, and it would be more cost eff...

John_Houbolt_and_LOR2

Earth Orbit Rendezvous

Apollo_Direct_Ascent

Posted on March 5, 2015

Many historians agree, the U.S. took its first step toward the moon in the spring of 1957, four years before President Kennedy declared the national goal of landing a man on the Moon, and returning him safely to the Earth. While still preparing for t...

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

Just as launch complex 34 dwarfed its predecessors, Saturn’s checkout represented a new magnitude in launch operations. The Saturn C-1 stood three times higher, required six times more fuel, and produced ten times more thrust than the Jupiter. Its si...

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

No previous maiden launch had gone flawlessly, and the Saturn C-1 was considerably more complicated than any rocket launched thus far. Launch Operations Directorate officials gave the rocket a 75% chance of getting off the ground, and a 30% chance of...

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

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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

The mode that Apollo would use to land on the moon was the most studied, analyzed, and debated decision made for the lunar landing program.  There were four main choices Direct-ascent, Earth-Orbit Rendezvous, Lunar-Orbit Rendezvous, and Lunar Surface...

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 main trouble with the Mercury capsule was that most system components were in the pilot’s cabin; and often, to pack them in this very confined space, they had to be stacked like a layer cake and components of one system had to be scattered about...

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