Encyclopedia Astronautica

Aerojet lox/lh2 rocket engine. 2213.850 kN. Booster. Pre-Development, Staged Combustion, 204 atm

Application: Booster.

Chamber Pressure: 207.00 bar.

Thrust: 2,213.85 kN (497,693 lbf).
First Launch: 1968.

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Associated Countries
See also
Associated Manufacturers and Agencies
  • Aerojet American manufacturer of rockets, spacecraft, and rocket engines. Aerojet, Sacramento, CA, USA. More...

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