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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.

Country
USA
Engines
Scramjet
Launch Vehicles
Tu-2000, X-30
Propellants
Air/Slush LH2