This page no longer updated from 31 October 2001. Latest version can be found at RM-900

RM-900 -

Credit: Boeing / Rocketdyne. 5,749 bytes. 129 x 234 pixels.

Manufacturer Name: RM-900. Designer: Rocketdyne. Developed in: 1972. Propellants: N2O4/MMH Thrust(vac): 408 kgf. Isp: 309 sec. Comments: Shuttle Orbiter Reaction Control. 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 .