PF RP-1

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Engine Model: PF RP-1. Propellants: Lox/Kerosene. Thrust(vac): 20,306.000 kN (4,564,970 lbf). Isp: 275 sec. Isp (sea level): 253 sec. Burn time: 163 sec. Chambers: 1. Country: USA. Status: Study 1967. PF RP-1 used on Rocket Stages Used on stage: Saturn PF. on launch vehicle: Saturn I. Contact us with any corrections, additions, or comments. Conditions for use of drawings, pictures, or other materials from this site.. To contact astronauts or cosmonauts. © Mark Wade, 1997 - 2008 except where otherwise noted.