RM-1-2 home
topic index
RM-1-2
Credit - Boeing / Rocketdyne
Engine Model: RM-1-2. Manufacturer Name: RM-1-2. Designer: Rocketdyne. Developed in: 1967. Propellants: N2O4/MMH. Thrust(vac): 4.41 N (0.99 lbf). Isp: 238 sec. Country: USA.

Satellite Reaction Control. Pressure-fed.

Contact us with any corrections, additions, or comments.
Conditions for use of drawings, pictures, or other materials from this site..
To contact astronauts or cosmonauts.

© Mark Wade, 1997 - 2008 except where otherwise noted.