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Influence of externally applied thermal radiation on the burning rates of homogeneous solid propellants

✍ Scribed by M.M. Ibiricu; F.A. Williams

Book ID
107741009
Publisher
Elsevier Science
Year
1975
Tongue
English
Weight
915 KB
Volume
24
Category
Article
ISSN
0010-2180

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## Abstract Through the analysis and calculation to the flow field in the solid rocket motor using high‐burning‐rate propellant, the authors believe that the existence of pressure difference between the inside and outside of the propellant tube causes the propellant crack. In this paper, the design