SPECIFICATIONS
| WEIGHT: |
Empty: 3920 kg (8650 lb) |
| |
Crew & Propellant: 14,700 kg (32,500 lb) |
| HEIGHT: |
7.0 m (22 ft 11 in) |
| WIDTH: |
9.4 m (31 ft 00 in) |
| THRUST: |
Descent Engine: |
44,316 Newtons (9870 lb) maximum |
| |
|
4710 Newtons (1050 lb) minimum |
| THRUST: |
Ascent Engine: |
15,700 Newtons (3500 lb) |
| FUEL: |
50-50 mix of Unsymmetrical Dimethyl Hydrazine (UDMH)
& Hydrazine |
| OXYDIZER: |
Nitrogen Tetroxide |
| PRIME CONTRACTOR: |
Grumman Aerospace Corporation |
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Lunar Module Specifications
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