This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
Used on stages: Saturn LCB-Storable-140, Saturn PFL. Used on launch vehicles: Saturn LCB-Storable-140. Propellants: N2O4/UDMH Thrust(vac): 2,911,600 kgf. Thrust(vac): 28,552.00 kN. Isp: 267 sec. Isp (sea level): 245 sec. Burn time: 167 sec. Chambers: 1. Country: USA. Status: Design concept 1960's.
Back to Index
Last update 12 March 2001.
Definitions of Technical Terms.
Contact Mark Wade with any corrections or comments.
Conditions for use of drawings, pictures, or other materials from this site..
© Mark Wade, 2001 .