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AJ23-144
Part of AJ23 Family
Aerojet LOx/LH2 rocket engine. Booster (Pre-Development, Staged Combustion, 4000 psi). Pre-Development, Staged Combustion, 272 atm

Date: 1985. Thrust: 3,020.00 kN (678,920 lbf).

Chamber Pressure: 276.00 bar.



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

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