L-2 Linear Aerospike Booster

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L-2 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: 1971. Thrust: 444.63 kN (99,957 lbf). Specific impulse: 455 s. Specific impulse sea level: 455 s.

Thrust (sl): 444.630 kN (99,957 lbf). Thrust (sl): 45,340 kgf.

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

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