Apr 09

Space Rocket History #108 – Apollo: The Mode Decision – Part 3

“I would like to reiterate once more that it is absolutely mandatory that we arrive at a definite mode decision within the next few weeks. . . . If we do not make a clear-cut decision on the mode very soon, our chances of accomplishing the first lunar expedition in this decade will fade away rapidly.” Wernher Von Braun June 7, 1962.

Rocket Comparison

Rocket Comparison

Shea demonstrates Lunar Docking

Shea demonstrates Lunar Docking

Lunar orbit insertion

Lunar orbit insertion

Apr 02

Space Rocket History #107 – Apollo: The Mode Decision – Part 2

Langley’s brochure for the Golovin Committee described Lunar landers of varied sizes and payload capabilities.  There were illustrations and data on a very small lander that was able to carry one man for 2 to 4 hours on the moon.  There was an “economy” model that could two men for a 24-hour stay. The third model was called the “plush” module, it would carry two men for a 7-day stay on the moon. Weight estimates for the three craft, without fuel, were 580, 1,010, and 1,790 kilograms, respectively…

Langley's Small Lunar Lander Concept.

Langley’s Small Lunar Lander Concept.

Proposed Lunar Lander for an Advanced Mercury

Proposed Lunar Lander for an Advanced Mercury

Design Concepts of Saturn C-1 thru C-5

Design Concepts of Saturn C-1 thru C-5

Mar 26

Space Rocket History #106 – Apollo: The Mode Decision – Part 1

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 Rendezvous.

Direct Ascent Landing Modes

Direct Ascent Landing Modes

Lunar Surface Rendezvous

Lunar Surface Rendezvous

Rendezvous Methods

Three Rendezvous Methods

Comparison of Lander Sizes

Comparison of Lander Sizes

Apollo Spacecraft Configuration Changes

Apollo Spacecraft Configuration Changes

Feb 26

Space Rocket History #102 – Apollo: Preliminary Design Part 3 – Command Module Contract, Mode, and Launch Vehicles

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 effective.  Faget said it made good sense to use cheap solid fuels for expendable rockets and more expensive liquid fuels for reusable engines. Faget called the individual solid rocket ‘the Tiger.’

Artist Conception of Apollo Direct Accent

Artist Conception of Apollo Direct Accent

Earth Orbit Rendezvous

Earth Orbit Rendezvous

John Houbolt Explains Lunar Orbit Rendezvous

John Houbolt Explains Lunar Orbit Rendezvous