Navaho G-26

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Model: Navaho G-26. Gross Mass: 29,478 kg (64,987 lb). Empty Mass: 9,977 kg (21,995 lb). Thrust (vac): 66.704 kN (14,996 lbf). Isp: 1,200 sec. Burn time: 6,500 sec. Propellants: Air/Kerosene. Isp(sl): 0 sec. Diameter: 1.55 m (5.08 ft). Span: 8.71 m (28.57 ft). Length: 20.67 m (67.81 ft). Country: USA. No Engines: 2. Motor: XRJ47-W-5. Status: Out of production. Cost $ : 10.000 million. First Flight: 1950. Last Flight: 1958. No Launched: 24. Other designations: XB-64, XSM-64. Payload: 2,500 kg (5,500 lb). Release velocity: 810 m/s (2,650 ft/sec). Release altitude: 24 m (78 ft). Release conditions: 3,048 kph at 24 km.

Separates from booster at 14,600 m, Mach 3. Mach 2.75 cruise, 5,600 km range, payload 2500 kg in 2.59 m x 1.50 m compartment.

Used on Launch Vehicles:

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