LH2 2000/3000 lbf thrust
Engine · USA
Original archive entry. The text, images and links below are kept as they were written.
Aerojet LOx/LH2 rocket engine. Development begun July 1946. Engine R&D, hydrogen production
Thrust (sl): 13.330 kN (2,997 lbf). Thrust (sl): 1,360 kgf.