Navaho G-38 Booster

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Navaho G-38 Booster

Navaho G-38 Engine
Navaho G-38 Engine
Navaho G-38 3 Engine Cluster

LOx/Kerosene propellant rocket stage. Burns out at altitude 21,600 m, Mach 3. Empty Mass estimated.

AKA: XB-64A;XSM-64A. Status: Development ended 1958. Thrust: 2,048.16 kN (460,444 lbf). Gross mass: 76,870 kg (169,460 lb). Unfuelled mass: 16,780 kg (36,990 lb). Specific impulse: 282 s. Specific impulse sea level: 248 s. Burn time: 90 s. Height: 27.43 m (89.99 ft). Diameter: 2.37 m (7.77 ft). Span: 2.37 m (7.77 ft).

Cost $ : 12.000 million. No Engines: 3.

Country: USA. Engines: LR83-NA-1. Launch Vehicles: Navaho G-38. Propellants: Lox/Kerosene.

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