PF N204/UDMH-2912k

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Engine Model: PF N204/UDMH-2912k. Propellants: N2O4/UDMH. Thrust(vac): 28,552.000 kN (6,418,744 lbf). Isp: 267 sec. Isp (sea level): 245 sec. Burn time: 167 sec. Chambers: 1. Country: USA. Status: Study 1967. PF N204/UDMH-2912k 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.