Self consistent set of empirical equations presented for describing most important performance parameters of rocket motor; these equations relate propellant burning rate, propellant temperature, chamber pressure, and area ratio so that designer can construct coherent set of correlations from only fragmentary data. (formerly Am Rocket Soc -- J)
Correlation of interior ballistic data for solid propellants
Jet Propulsion
Jet Propulsion ; 24 , n 1
1954
5 pages
Article (Journal)
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Determination of interior ballistic characteristic data of propellants
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