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Credit: Boeing / Rocketdyne. 13,735 bytes. 210 x 354 pixels.
: 1957. Propellants:
: 89,780 kgf.
: Booster applications. Gas generator, pump-fed. Thrust from 165,000 to 198,000 lbs.
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Last update 12 March 2001.
Definitions of Technical Terms
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© Mark Wade, 2001 .