Rocketdyne LOx/LH2 rocket engine. Study 1993. Plug nozzle version of J-2 proposed for certain Saturn V upgrades in late 1960's. Used on DC-I launch vehicle.
Status: Study 1993. Thrust: 6,864.60 kN (1,543,223 lbf). Specific impulse: 425 s. Specific impulse sea level: 330 s. Burn time: 260 s.