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SSME Demonstrator Booster
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 .
