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Astrorocket-1
N2O4/Aerozine-50 propellant rocket stage. Delta wing configuration. LR87-derivative engines.

Status: Study 1962. Thrust: 14,700.00 kN (3,304,600 lbf). Gross mass: 981,859 kg (2,164,628 lb). Unfuelled mass: 132,000 kg (291,000 lb). Specific impulse: 293 s. Specific impulse sea level: 258 s. Burn time: 164 s. Height: 65.00 m (213.00 ft). Diameter: 7.00 m (22.90 ft). Span: 40.00 m (131.00 ft).

Cost $ : 18.000 million. No Engines: 9.



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

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