Electrification of nozzle in a liquid rocket engine

descriptionPublicationkeyboard_double_arrow_right Article 01 Jan 1995 English Publisher:Springer Science and Business Media LLCJournal:Combustion, Explosion, and Shock Waves, volume 31, pages 450-454 (issn: 0010-5082, eissn: 1573-8345,

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Authors: D. A. Yagodnikov; A. V. Voronetskii; N. M. Pushkin;

doi: 10.1007/bf00789365

Electrification of nozzle in a liquid rocket engine

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Abstract

A method of electrical-physical diagnostics is developed and experimental studies are conducted of the process of nozzle electrification in a liquid rocket engine operating on a hydrocarbon fuel. The highest electric potential is shown to be realized at about a stoichiometric ratio of the components, i.e., when the flow velocity, temperature, and, hence, ionization of combustion products are maximum. Recommendations for practical application of the information obtained are given.

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