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RM-1-2
RM-1-2 -
Credit: Boeing / Rocketdyne. 4,964 bytes. 165 x 207 pixels.
Manufacturer Name
: RM-1-2.
Designer
: Rocketdyne.
Developed in
: 1967. Propellants:
N2O4/MMH
Thrust(vac)
: 0 kgf.
Isp
: 238 sec.
Comments
: Satellite Reaction Control. Pressure-fed.
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Last update 12 March 2001.
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© Mark Wade, 2001 .