E-1 Credit: Boeing / Rocketdyne |
Status: Study 1957. Date: 1957. Thrust: 1,884.59 kN (423,673 lbf). Specific impulse: 290 s. Specific impulse sea level: 260 s.
Thrust (sl): 1,689.600 kN (379,837 lbf). Thrust (sl): 172,300 kgf. Propellant Formulation: Lox/RP-1.
E-1 Engine Credit: © Mark Wade |