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In the last decade, many parties have become interested in Hydrogen Peroxide for bi-propellant applications. Typical bipropellant rocket schemes involve various types of liquid-liquid co-injected. Hydrogen peroxide being a monopropellant offers opportunities in that it may be decomposed into superheated steam and oxygen prior to the addition of a fuel. It will be shown that this method has technical advantages over liquid-liquid injection schemes and additionally is lighter in mass. I.
Eric Wernimont (Sun,) studied this question.
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