This page no longer updated from 31 October 2001. Latest version can be found at 5 mlbf

Used on stages: OOST, ROOST. Used on launch vehicles: OOST, ROOST. Propellants: Lox/LH2 Thrust(vac): 4,217,750 kgf. Thrust(vac): 41,361.00 kN. Isp: 410 sec. Isp (sea level): 345 sec. Burn time: 246 sec. Chambers: 1. Country: USA. Status: Study 1963.
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 .