PF N204/Alumizine-1925k

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Engine Model: PF N204/Alumizine-1925k. Propellants: N2O4/Alumizine. Thrust(vac): 18,873.000 kN (4,242,819 lbf). Isp: 280 sec. Isp (sea level): 260 sec. Burn time: 168 sec. Chambers: 1. Country: USA. Status: Study 1967. PF N204/Alumizine-1925k 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.