This page no longer updated from 31 October 2001.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

SSME Demonstrator
SSME Demonstrator - SSME Demonstrator Booster

Credit: Boeing / Rocketdyne. 9,091 bytes. 168 x 202 pixels.

Designer: Rocketdyne. Developed in: 1970. Propellants: Lox/LH2 Thrust(vac): 249,400 kgf. Isp: 465 sec. Comments: Pressure-fed.
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Last update 12 March 2001.
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© Mark Wade, 2001 .