This page no longer updated from 31 October 2001. Latest version can be found at www.astronautix.com
astronautix.com Nova MM 14B-2
Advanced Engines
Advanced Engines
Advanced Engines planned for uprated Saturn and Nova boosters

Credit: © Mark Wade. 6,664 bytes. 571 x 365 pixels.

Gross Mass: 2,721,000 kg. Empty Mass: 245,000 kg. Thrust (vac): 2,721,000 kgf. Isp: 428 sec. Burn time: 383 sec. Propellants: Lox/LH2 Diameter: 18.3 m. Span: 18.3 m. Length: 50.5 m. Country: USA. No Engines: 4. M-1 Status: Study 1963. Comments: Operational date would have been February 1973 .
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 .