This page no longer updated from 31 October 2001.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

astronautix.com RB545


Designer: Rolls Royce. Used on stages: HOTOL. Used on launch vehicles: HOTOL. Propellants: Liquid Air/Lox/LH2 Thrust(vac): 37,500 kgf. Thrust(vac): 367.70 kN. Isp: 700 sec. Isp (sea level): 2,000 sec. Burn time: 730 sec. Chambers: 1. Country: UK. Status: Developed -1992.
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 .