AABS

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AABS

Aerospike Annular
Aerospike Annular Booster
Credit: Boeing / Rocketdyne

Rocketdyne LOx/Kerosene rocket engine. Aerospike Annular Booster and Sustainer. Pressure-fed. Booster thrust 3000 to 4000 lb vac; sustainer 1500-2000 lb vac, 257 sec specific impulse.

Date: 1967. Thrust: 17.78 kN (3,997 lbf). Specific impulse: 285 s.

Propellant Formulation: Lox/RP-1.

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

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