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Timberwind 45
DoE nuclear/LH2 rocket stage. Development ended 1992. Used on Timberwind Centaur launch vehicle.

Status: Development ended 1992. Thrust: 441.00 kN (99,140 lbf). Gross mass: 28,000 kg (61,000 lb). Unfuelled mass: 7,500 kg (16,500 lb). Specific impulse: 1,000 s. Specific impulse sea level: 890 s. Burn time: 449 s. Height: 23.87 m (78.31 ft). Diameter: 4.25 m (13.94 ft). Span: 4.25 m (13.94 ft).

Thrust (sl): 392.800 kN (88,305 lbf). Thrust (sl): 40,050 kgf. Engine: 1,500 kg (3,300 lb). Thrust to Weight Ratio: 30.

Cost $ : 100.000 million.



Family: nuclear-powered. Country: USA. Launch Vehicles: Timberwind Centaur. Propellants: Nuclear/LH2. Stages: Timberwind 45. Agency: AEC.

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