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