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Astrorocket-2
N2O4/Aerozine-50 propellant rocket stage. X-20 Dynasoar configuration. LR87-derivative engines.

Status: Study 1962. Thrust: 2,150.00 kN (483,330 lbf). Gross mass: 151,927 kg (334,941 lb). Unfuelled mass: 23,500 kg (51,800 lb). Specific impulse: 345 s. Specific impulse sea level: 230 s. Burn time: 181 s. Height: 30.00 m (98.00 ft). Diameter: 3.00 m (9.80 ft). Span: 20.00 m (65.00 ft).

Cost $ : 18.000 million.



Country: USA. Engines: LR87plus. Launch Vehicles: Martin Astrorocket. Propellants: N2O4/Aerozine-50.

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