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Analysis of liquid-propellant rocket engines designed by F. A. TsanderThe development of the oxygen-gasoline OR-2 engines and the oxygen-alcohol GIRD-10 rocket engine is described. A result of Tsander's rocket research was an engineering method for propellant calculation of oxygen-propellant rocket engines that determined the basic parameters of the engine and the structural elements.
Document ID
19770026111
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Dushkin, L. S. (USSR)
Moshkin, Y. K. (USSR)
Date Acquired
August 8, 2013
Publication Date
September 1, 1977
Publication Information
Publication: Essays on the History of Rocketry and Astronautics, Vol. 2
Subject Category
Propellants And Fuels
Accession Number
77N33055
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19770026104Collected WorksEssays on the History of Rocketry and Astronautics: Proceedings of the Third Through the Sixth History Symposia of the International Academy of Astronautics, Volume 2
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