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L-1 Linear Aerospike Booster
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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. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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