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Rocket engines / Transport / Rocket propulsion / Liquid-propellant rocket / LE-5 / Expander cycle / Multistage rocket / RL10 / Spacecraft propulsion / Space technology / Aerospace engineering


DETERMINATION METHOD OF OPTIMUM MAIN DESIGN PARAMETERS OF LOX-LH2 EXPANDER-CYCLE LRE
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Document Date: 2010-04-20 04:01:01

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File Size: 245,33 KB

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