AJ23-127

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AJ23-127

Part of AJ23

Aerojet LOx/LH2 rocket engine. Booster. The AJ23 was a series of high-performance staged combustion engine designs. None ever made it to production. The -127 featured a gas generator cycle, 56 atm

Date: 1969. Thrust: 1,010.00 kN (227,050 lbf).

Chamber Pressure: 57.00 bar.

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

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