May 12

Space Rocket History #160 – Apollo 8 – The Decision Part 1

An ‘A’ type mission would be flown with a Saturn V and be used to test the Launch vehicle, spacecraft, and a high velocity lunar return. Nasa cover the ‘A’ mission with Apollo 4 & 6.
A ‘B’ type mission would be flow with a Saturn IB and test the lunar module development, and propulsion, and launch vehicle staging. This was accomplished with Apollo 5.
A ‘C’ type mission would be flown with a Saturn IB and test the command and service module and evaluate the crew performance in low earth orbit. This was accomplished with Apollo 7…

Owen Maynard's Seven Step Plan to land on the Moon

Owen Maynard’s Seven Step Plan to land on the Moon

Owen Maynard, Chief of LEM engineering office

Owen Maynard, Chief of LEM engineering office

George Low, Manager of the Apollo Spacecraft Program Office

George Low, Manager of the Apollo Spacecraft Program Office

Apr 20

Space Rocket History An Encore Presentation of Episode #35 – Textbook Spaceflight – Mercury-Atlas 8, Sigmac 7 with Wally Schirra

After Scott Carpenter’s science heavy Mercury-Atlas 7 flight, Nasa’s next mission would concentrate on the technical and engineering aspects of space travel.  Mercury Atlas 8 became the third manned orbital flight of the Mercury program. The pilot selected was Walter M. Schirra, Jr., but most people called him Wally…

Mission Logo

Mission Logo

Wally Schirra

Wally Schirra

Sigma 7

Sigma 7

Lift-off

Lift-off

Splash Down

Splash Down

Recovery

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