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LE-3
LE-3 -
Credit: Boeing / Rocketdyne. 5,926 bytes. 143 x 235 pixels.
Designer
: Rocketdyne.
Developed in
: 1970. Propellants:
N2O4/Aerozine-50
Thrust(vac)
: 5,440 kgf.
Isp
: 285 sec.
Comments
: MHI(Japan)/Rocketdyne Upper Stage. Pressure-fed.
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Last update 12 March 2001.
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© Mark Wade, 2001 .
