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Gross Mass: 54,648 kg (120,478 lb). Empty Mass: 14,512 kg (31,993 lb). Thrust (vac): 89.260 kN (20,066 lbf). Isp: 1,200 sec. Burn time: 10,300 sec. Propellants: Air/Kerosene. Isp(sl): 0 sec. Diameter: 1.98 m (6.49 ft). Span: 12.25 m (40.19 ft). Length: 26.61 m (87.30 ft). Country: USA. No Engines: 2. Engine: RJ47. Status: Development ended 1958. Cost $ : 12.000 million. Other designations: XB-64A, XSM-64A. Payload: 4,550 kg (10,030 lb). Release velocity: 960 m/s (3,140 ft/sec). Release altitude: 24 m (78 ft). Release conditions: 3,670 kph at 24 km. Separates from booster at 21,600 m, Mach 3. Mach 3.25 cruise, 10,200 km range, payload 4545 kg in 3.76 m x 1.78 m weapons bay. Empty mass estimated.
Used on Launch Vehicles:
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