PROGRESS IN THE DEVELOPMENT OF A SMALL-SCALE ROCKET ENGINE USING HOMOGENEOUS CATALYSIS OF HYDROGEN PEROXIDE

机译：过氧化氢的均相催化发展小型火箭发动机的研究进展

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The high purity of rocket grade hydrogen peroxide places stringent operational and cost constraints on the user in terms of transportation and storage because of the peroxide's sensitivity to contamination and hence accidental decomposition. This paper explores the possibility of using a much more stable form of hydrogen peroxide in conjunction with the aggressive use of a liquid catalyst in a catalytic decomposition chamber. Some experiments are described and preliminary results are reported.

机译：火箭级过氧化氢的高纯度在运输和存储方面给用户带来了严格的操作和成本限制，因为过氧化物对污染物的敏感性很高，因此会意外分解。本文探讨了在催化分解室中积极使用液态催化剂并结合使用更稳定形式的过氧化氢的可能性。描述了一些实验并报告了初步结果。

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来源
《1st International conference on green propellant for space propulsion》|2001年|p.1-8|共8页
会议地点 Noordwijk(NL)
作者
Antony J Musker;
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作者单位

School of Engineering Sciences, University of Southampton. White Lodge, Ryde Place, Lee on Solent, Hampshire, England, PO13 9AU Tel: 02392 349187 email: tony.musker@cwcom.net;

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正文语种 eng
中图分类空气动力学;
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PROGRESS IN THE DEVELOPMENT OF A SMALL-SCALE ROCKET ENGINE USING HOMOGENEOUS CATALYSIS OF HYDROGEN PEROXIDE

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