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

Jan 29

Space Rocket History #98 – Apollo Beginnings

President Kennedy proposed the manned lunar landing as the focus of the US space program but, at the time of his address, only one American, Alan B. Shepard, Jr. had been into space, on a suborbital lob shot lasting 15 minutes. No rocket launch vehicle was available for a lunar voyage and there was no agreed upon method for placing any kind of spacecraft safely on the lunar surface and getting it back to the earth. Nor was there agreement within NASA itself on how it should be done.

Astronauts leave the spacecraft to investigate the lunar surface.

Astronauts leave the spacecraft to investigate the lunar surface.

The return vehicle takes off from the moon.

The return vehicle takes off from the moon.

The reentry vehicle begins to enter the atmosphere after jettisoning the propulsion unit.

The reentry vehicle begins to enter the atmosphere after jettisoning the propulsion unit.

Aug 08

Space Rocket History #24 – Mercury Redstone Test Flights – Ham in a Can

The objectives of the Mercury Project, were as follows:
1. Place a manned spacecraft in orbital flight around the earth.
2. Investigate man’s performance capabilities and his ability to function in the environment of space.
3. Recover the man and the spacecraft safely.
After the objectives were established for the project, a number of guidelines were created to insure that the most expedient and safest approach for attainment of the objectives was followed. The basic guidelines that were established are as follows:
1. Existing technology and off-the-shelf equipment should be used wherever practical.
2. The simplest and most reliable approach to system design would be followed.
3. An existing launch vehicle would be employed to place the spacecraft into orbit.
4. A progressive and logical test program would be conducted.

MerCapEscSys

Escape System

MerCapInt

Capsule

3AxisHandController

Hand Controller

mercury1

Capsule Interior

Assembly

Assembly

Parachute Canister

Parachute Can

MR-1

MR-1

Ham

Ham

Ham

Ham