This page no longer updated from 31 October 2001. Latest version can be found at LH2-80k

Used on stages: Nova 59-4-3, Nova 59-4-4. Used on launch vehicles: Nova 4L. Propellants: Lox/LH2 Thrust(vac): 36,274 kgf. Thrust(vac): 355.70 kN. Isp: 425 sec. Isp (sea level): 306 sec. Burn time: 656 sec. Mass Engine: 1,438 kg. Chambers: 1. Chamber Pressure: 30.00 bar. Area Ratio: 28.00. Country: USA. Status: Study 1959.
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 .