Preliminary Assessment of Hydrogen Peroxide Gel as an Oxidizer in a Catalyst Ignited Hybrid Thruster

In regard to propulsion system applications, the stability of liquid propellants in long-term storage is of increasing importance, and this had led to a greater interest in gelation technology. As part of a preliminary test to determine the feasibility of using a gel propellant in a rocket with a ca...

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Veröffentlicht in:International journal of aerospace engineering 2018-01, Vol.2018 (2018), p.1-14
Hauptverfasser: Shoaib, M. N., Yun, Yongtae, Jyoti, Botchu V. S., Huh, Jeongmoo, Kwon, Sejin
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Sprache:eng
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