Aerojet lox/lh2 rocket engine. 3020 kN. Booster (Pre-Development, Staged Combustion, 4000 psi). Pre-Development, Staged Combustion, 272 atm
Application: Booster (Pre-Development, Staged Combustion, 4000 psi).
Chamber Pressure: 276.00 bar.
Thrust: 3,020.00 kN (678,920 lbf).
First Launch: 1985.
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Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...
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