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AJ23-143
Part of AJ23 Family
Aerojet LOx/LH2 rocket engine. Booster. Pre-Development, Staged Combustion, 204 atm

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

Chamber Pressure: 207.00 bar.



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

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