This page no longer updated from 31 October 2001. Latest version can be found at RM-1-1

RM-1-1 -

Credit: Boeing / Rocketdyne. 6,736 bytes. 165 x 234 pixels.

Manufacturer Name: RM-1-1. Designer: Rocketdyne. Developed in: 1967. Propellants: N2O4/MMH Thrust(vac): 0 kgf. Isp: 245 sec. Comments: Satellite Reaction Control System. Pressure-fed.
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Last update 12 March 2001.
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© Mark Wade, 2001 .