The sign accompanying the ascent propulsion system engine. It reads
Lunar Module Ascent Engine
The descent stage served as a launching platform from which the ascent stage
lifted off the lunar surface.
Thrust: |
3,500 lb |
Propellant: |
Aerozine 50/Nitrogen Tetroxide (hypergolic) |
Mixture ratio: |
1.6:1 |
Engine start capability: |
35 times |
Developed by Bell Aerosystems
On loan from Smithsonian Institute
|
|