This page no longer updated from 31 October 2001. Latest version can be found at
Credit: Boeing / Rocketdyne. 5,263 bytes. 124 x 210 pixels.
: 1999. Propellants:
: 27,200 kgf.
: 467 sec.
: MHI (Japan)/Boeing Cryogenic Upper Stage. Expander bleed, pump-fed. Delta-IV upper stage.
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Last update 12 March 2001.
Definitions of Technical Terms
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© Mark Wade, 2001 .