This page no longer updated from 31 October 2001. Latest version can be found at RM-1500H

RM-1500H -

Credit: Boeing / Rocketdyne. 7,245 bytes. 137 x 235 pixels.

Manufacturer Name: RM-1500H. Designer: Rocketdyne. Developed in: 1971. Propellants: Lox/LH2 Thrust(vac): 680 kgf. Isp: 400 sec. Comments: Space Shuttle Orbiter Auxiliary Propulsion. Pressure-fed.
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 .