This page no longer updated from 31 October 2001.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