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Navaho G-38 AV
Part of Navaho G-26 AV
Ramjet-powered missile stage. 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.

AKA: Navaho G-38;XB-64A;XSM-64A. Status: Development ended 1958. Payload: 4,550 kg (10,030 lb). Thrust: 89.26 kN (20,066 lbf). Gross mass: 54,648 kg (120,478 lb). Unfuelled mass: 14,512 kg (31,993 lb). Specific impulse: 1,200 s. Burn time: 10,300 s. Height: 26.61 m (87.30 ft). Diameter: 1.98 m (6.49 ft). Span: 12.25 m (40.19 ft). Location: 960.

Cost $ : 12.000 million. No Engines: 2. Release velocity: 960 m/s (3,140 ft/sec). Release altitude: 24 m (78 ft). Release conditions: 3,670 kph at 24 km.



Country: USA. Engines: RJ47. Launch Vehicles: Navaho G-38. Propellants: Air/Kerosene.

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