Assessment of Catalysts for Hydrogen-Peroxide-Based Thrusters in a Flow Reactor

Hydrogen peroxide is a candidate propellant for rocket-propulsion applications with the potential to replace highly toxic propellants currently used. Decomposition of hydrogen peroxide yields a high-temperature oxygen-steam mixture, which can be used as monopropellant or as oxidizer in a bipropellan...

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Veröffentlicht in:	Journal of propulsion and power 2013-03, Vol.29 (2), p.321-330
Hauptverfasser:	Krejci, David, Woschnak, Alexander, Schiebl, Markus, Scharlemann, Carsten, Ponweiser, Karl, Brahmi, Rachid, Batonneau, Yann, Kappenstein, Charles
Format:	Artikel
Sprache:	eng
Schlagworte:	Carrier density Catalysis Catalysts Chemical Sciences Configurations Decomposition Density High temperature Hydrogen Hydrogen peroxide Mass flow Organic chemistry Other Oxidizing agents Propellants Propulsion Reactors Thrusters
Online-Zugang:	Volltext
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