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Scramjet
Scram. Development ended 1992. Thrust is maximum sea level thrust; specific impulse is average during ascent. Propellant Slush LH2.

Status: Development ended 1992. Thrust: 1,372.90 kN (308,640 lbf). Specific impulse: 1,550 s. Burn time: 886 s. Diameter: 16.00 m (52.00 ft).

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. Stages: Tu-2000 EAP.
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