L-1 Linear Aerospike Booster

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L-1 Linear Aerospike Booster

L-2 Linear Aerospike
L-2 Linear Aerospike
L-1 Linear Aerospike Booster
Credit: Boeing / Rocketdyne

Rocketdyne LOx/Kerosene rocket engine. Gas generator, pump-fed. Thrust and specific impulse values are at sea level.

Date: 1970. Thrust: 889.36 kN (199,936 lbf). Specific impulse: 455 s. Specific impulse sea level: 455 s.

Thrust (sl): 889.360 kN (199,936 lbf). Thrust (sl): 90,690 kgf.

Country: USA. Propellants: Lox/Kerosene. Agency: Rocketdyne.

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