๐”– Bobbio Scriptorium
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Temperature sensitivity coefficients of solid propellant burning rate

โœ Scribed by Michael T. Gaunce; John R. Osborn


Publisher
Elsevier Science
Year
1986
Tongue
English
Weight
320 KB
Volume
13
Category
Article
ISSN
0094-5765

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โœ J. M. Smith ๐Ÿ“‚ Article ๐Ÿ“… 1960 ๐Ÿ› American Institute of Chemical Engineers ๐ŸŒ English โš– 772 KB
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Various theories [1,2] have been proposed for the pressure dependence of burning rate of composite propellants since a knowledge of this pressure dependence is vital for the design of a solid propellant rocket motor. Recently, Girdhar and Arora [3] have measured the burning rate of phenol-formaldehy

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โœ V. Swaminathan; M. Soosaimarian ๐Ÿ“‚ Article ๐Ÿ“… 1981 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 403 KB

## Abstract One of the principal parameters associated with a solid propellant is its linear burning rate. Many attempts have been made in the past to determine theoretically the burning rates of solid propellants by the use of appropriate combustion models. The object of the present paper is to pr