This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com

astronautix.com Plug-Nozzle SSME


Used on stages: VTOVL 150t. Used on launch vehicles: VTOVL. Propellants: Lox/LH2 Thrust(vac): 380,221 kgf. Thrust(vac): 3,728.70 kN. Isp: 485 sec. Isp (sea level): 412 sec. Burn time: 500 sec. Mass Engine: 2,973 kg. Chambers: 1. Area Ratio: 600.00. Country: USA. Status: Study 1970.
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 .