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