AJ23-145
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet LOx/LH2 rocket engine. Booster (Pre-Development, Staged Combustion, 4000 psi, LOX/RJ-5 or LH2, Single Stage). Pre-Development, Staged Combustion, 272 atm, LOX/RJ-5 or LH2, Single Stage
Chamber Pressure: 276.00 bar.