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