H-1c Designer: Rocketdyne. Propellants: Lox/Kerosene. Thrust(vac): 1,130.000 kN (254,030 lbf). Isp: 296 sec. Isp (sea level): 262 sec. Burn time: 128 sec. Chambers: 1. Country: USA. Status: Study 1965. H-1c used on Rocket Stages Used on stage: Saturn S-IB-A. on launch vehicle: Saturn IB-A. Used on stage: Saturn S-IB-A. on launch vehicle: Saturn IB-B.                   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 - 2007 except where otherwise noted.

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