Toroidal 400k

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Engine Model: Toroidal 400k. Propellants: Lox/LH2. Thrust(vac): 1,778.000 kN (399,710 lbf). Isp: 447 sec. Isp (sea level): 200 sec. Burn time: 385 sec. Chambers: 1. Country: USA. Status: Study 1967. Toroidal 400k used on Rocket Stages Used on stage: Saturn II. on launch vehicle: Saturn C-2. Used on stage: Saturn II. on launch vehicle: Saturn C-3. Used on stage: Saturn II. on launch vehicle: Saturn C-8. Used on stage: Saturn II. on launch vehicle: Saturn V. Used on stage: Saturn S-IV. on launch vehicle: Saturn I. Used on stage: Saturn S-IV. on launch vehicle: Saturn V. Toroidal 400k used on Spacecraft Used on: Saturn MS-IVB-3B. 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.