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Rocket engines / Spacecraft propulsion / Rocket propulsion / Pyrotechnics / Rocket propellants / Liquid-propellant rocket / Propellant / RP-1 / Ignition system / Space technology / Transport / Rocketry


Development of ignition systems for 200N and 500N thrusters
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Document Date: 2010-04-20 04:01:17

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File Size: 289,33 KB

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