XJ40-WE-1 (original) (raw)

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XJ40-WE-1

Wright turbojet engine. Out of production. Thrust is maximum thrust at cruise altitude. Specific impulse is that at cruise design point. Used on Navaho X-10 launch vehicle. First flight 1955.

AKA: J40. Status: Out of production. Number: 30 . Thrust: 48.50 kN (10,903 lbf). Unfuelled mass: 850 kg (1,870 lb). Specific impulse: 1,800 s. Burn time: 2,000 s.

Thrust (sl): 48.500 kN (10,903 lbf). Thrust (sl): 4,943 kgf. Engine: 850 kg (1,870 lb). Thrust to Weight Ratio: 5.81.

Family: Turbojet. Country: USA. Launch Vehicles: Navaho X-10. Propellants: Air/Kerosene. Stages: Navaho X-10 stage. Agency: Wright.

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