Aerospike Annular Booster

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Aerospike Annular Booster

Part of J-2

AERO
Credit: Boeing / Rocketdyne

Rocketdyne LOx/LH2 rocket engine. Aerospike Typical Annular Booster . Pressure-fed. Thrust from 50,000 to 250,000 lbs at altitude.

Date: 1967. Thrust: 1,111.66 kN (249,912 lbf). Specific impulse: 450 s.

Country: USA. Propellants: Lox/LH2. Agency: Rocketdyne.

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