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Model: Astrorocket-2. Gross Mass: 151,927 kg (334,941 lb). Empty Mass: 23,500 kg (51,800 lb). Thrust (vac): 2,150.000 kN (483,330 lbf). Isp: 345 sec. Burn time: 181 sec. Propellants: N2O4/Aerozine-50. Isp(sl): 230 sec. Diameter: 3.00 m (9.80 ft). Span: 20.00 m (65.00 ft). Length: 30.00 m (98.00 ft). Country: USA. No Engines: 1. Status: Study 1962. Cost $ : 18.000 million. First Flight: 1973.

X-20 Dynasoar configuration. LR87-derivative engines.

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