GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS | ||||
International Conference on Aerospace Sciences and Aviation Technology | ||||
Article 17, Volume 9, ASAT Conference, 8-10 May 2001, May 2001, Page 1-13 PDF (1.37 MB) | ||||
Document Type: Original Article | ||||
DOI: 10.21608/asat.2001.24778 | ||||
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Author | ||||
ZAYED A-N. | ||||
Abstract | ||||
This paper describes criteria and formulas that are capable of evaluating the burning perimeters of cruciform and Inform solid propellant grains (externally burning grains) during combustion. The effect of the restrictor width on the burning perimeter during combustion is investigated and analyzed. Some dimensions of the grain configuration are optimized and recommended. | ||||
Keywords | ||||
Rocket motor; Solid propellant; Cruciform grain; Triform grain | ||||
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