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SSME Demonstrator Booster
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SSME Demonstrator
SSME Demonstrator Booster
Credit: Boeing / Rocketdyne Rocketdyne LOx/LH2 rocket engine. Pressure-fed.
Date: 1970. Thrust: 2,445.70 kN (549,815 lbf). Specific impulse: 465 s.
Country: USA. Propellants: Lox/LH2. Agency: Rocketdyne. Back to top of page Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
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