Mar 30

Space Rocket History #155 – Apollo 7 – Assembly, Testing, Training, and Launch

Command Service Module-101 started through the manufacturing cycle early in 1966. By July, it had been formed, wired, fitted with subsystems, and made ready for testing. After the Apollo 1 fire in January 1967, changes had to be made, mainly in the wiring, hatch areas, and the forward egress tunnel. It was December before the spacecraft came back into testing. CSM-101 passed through a three-phase customer acceptance review; during the third session, held in Downey on May 7th 1968, no items showed up that might be a “constraint to launch.” North American cleared up what few deficiencies there were (13) and shipped the craft to Kennedy on  May 30th 1967…

AS-205's First Stage on the pedestal

AS-205’s First Stage on the pedestal

Apollo 7 Crew practice climbing out of the spacecraft

Apollo 7 Crew practice climbing out of the spacecraft

Apollo 7 Launch

Apollo 7 Launch

Feb 25

Space Rocket History #150 – Apollo 6: Pogo and the Tang Ceremony

The success of Apollo 4 gave good reason to believe that the Saturn V could be trusted to propel men into space. But NASA pushed on with its plans for a second unmanned booster flight, primarily to give the Pad 39 launch team another rehearsal before sending men into deep space on the Saturn V.  The mission was called Apollo 6…

Apollo 6 patch

Apollo 6 patch

Lunar Test Article

Lunar Test Article

Apollo 6 launch

Apollo 6 launch

Exhaust plume of Apollo 6

Exhaust plume of Apollo 6

Interstage falling away

Interstage falling away

Apollo 6 splashdown and recovery

Apollo 6 splashdown and recovery

Feb 04

Space Rocket History #147 – Saturn: S-II Stage Part 2: Trials and Tribulations

“The S-II stage was a nightmare the minute it was conceived, and it only got worse from there. During the course of its creation, it would grind up people and careers the way the transcontinental railway devoured laborers.  Though the methods and materials used to build the S-II were reasonably well known, nobody had ever tried to apply them on such a titanic scale.  Originally, it was to be somewhere around 8 stores tall with a diameter of 22 feet, but the width ballooned from there to 27 feet before the contract was  even signed, then to 30, and finally to 33 feet.  And all the while as the size of thing increased, NASA was trimming the allowable weight.”  Harrison Storms of NAA.

Test firing of S-II Stage in Mississippi

Test firing of S-II Stage in Mississippi

Saturn V S-II Second Stage

Saturn V S-II Second Stage

Saturn S-II Assembly Building at Seal Beach.

Saturn S-II Assembly Bldg at Seal Beach.

S-II during stacking operations in the VAB

S-II during stacking operations in the VAB

S-II Inboard Profile in 1963

S-II Inboard Profile in 1963

S-II Cut-away with callouts

S-II Cut-away with callouts

Jan 28

Space Rocket History #146 – Saturn: S-II Stage Part 1: Common Bulkheads, Gores, & Honeycomb Sandwiches

The structural efficiency of the S-II stage, in terms of the weight and pressures taken by its extra-thin walls, was comparable only to the capacity of one of nature’s most refined examples of structural efficiency, the egg.

Saturn S-II Stage Diagram

Saturn S-II Stage Diagram

Saturn S-II Stage Exploded View

Saturn S-II Stage Exploded View

Saturn S-II Cut-Away Drawing

Saturn S-II Cut-Away Drawing