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Timberwind 250
DoE nuclear/LH2 rocket stage. Development ended 1992. Used on Timberwind launch vehicle.

Status: Development ended 1992. Thrust: 2,450.00 kN (550,780 lbf). Gross mass: 170,000 kg (370,000 lb). Unfuelled mass: 45,000 kg (99,000 lb). Specific impulse: 1,000 s. Specific impulse sea level: 780 s. Burn time: 493 s. Height: 30.00 m (98.00 ft). Diameter: 8.70 m (28.50 ft). Span: 8.70 m (28.50 ft).

Thrust (sl): 1,912.300 kN (429,902 lbf). Thrust (sl): 195,000 kgf. Engine: 8,300 kg (18,200 lb). Thrust to Weight Ratio: 30.1204819277108.

Cost $ : 100.000 million.



Family: nuclear-powered. Country: USA. Launch Vehicles: Timberwind. Propellants: Nuclear/LH2. Stages: Timberwind 250. Agency: AEC.

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