This page no longer updated from 31 October 2001.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

astronautix.com Toroid FD


Used on stages: Nova MM T10RR-2-2. Used on launch vehicles: Nova MM T10RR-2. Propellants: Lox/LH2 Thrust(vac): 2,041,000 kgf. Thrust(vac): 20,015.00 kN. Isp: 455 sec. Burn time: 408 sec. Chambers: 1. Country: USA. Status: Study 1963. Comments: Operational date would have been December 1976. Engines for recoverable stage.
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 .