Scramjet
USA
Original archive entry. The text, images and links below are kept as they were written.
Scram. Development ended 1992. Thrust is maximum sea level thrust; specific impulse is average during ascent. Propellant Slush LH2.
Thrust (sl): 1,372.900 kN (308,640 lbf). Thrust (sl): 140,000 kgf.
Related
- Country
- USA
- Engines
- Scramjet
- Propellants
- Air/Slush LH2
- Stages
- Tu-2000 EAP