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Timberwind 75

Stage · USA

Original archive entry. The text, images and links below are kept as they were written.

DoE nuclear/LH2 rocket stage. Development ended 1992. Used on Timberwind Titan launch vehicle.

Thrust (sl): 654.600 kN (147,160 lbf). Thrust (sl): 66,750 kgf. Engine: 2,500 kg (5,500 lb). Thrust to Weight Ratio: 30.

Cost $ : 100.000 million. No Engines: 3.

Country
USA
Launch Vehicles
Timberwind Titan
Propellants
Nuclear/LH2
Agency
AEC