LR83-NA-1

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LR83-NA-1

Part of LR79

XLR-83-NA-1
Credit: Boeing / Rocketdyne

Rocketdyne LOx/Kerosene rocket engine. Development ended 1958. Planned production version of the engine for the booster of the Navaho G-38 intercontinental cruise missile.

AKA: G-38. Status: Development ended 1958. Thrust: 683.00 kN (153,544 lbf). Specific impulse: 282 s. Specific impulse sea level: 248 s. Diameter: 0.88 m (2.88 ft).

Designed for booster applications. Gas generator, pump-fed. Three gimbaled engines would have been used in the Navaho booster. The engine was fully developed before Navaho G-38 cancellation.

Thrust (sl): 602.000 kN (135,334 lbf). Thrust (sl): 61,393 kgf.

Country: USA. Launch Vehicles: Navaho G-38. Propellants: Lox/Kerosene. Stages: Navaho G-38 Booster. Agency: Rocketdyne.

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