GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS
A-N., Z. (2001). GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS. EKB Journal Management System, 9(ASAT Conference, 8-10 May 2001), 1-13. doi: 10.21608/asat.2001.24778
ZAYED A-N.. "GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS". EKB Journal Management System, 9, ASAT Conference, 8-10 May 2001, 2001, 1-13. doi: 10.21608/asat.2001.24778
A-N., Z. (2001). 'GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS', EKB Journal Management System, 9(ASAT Conference, 8-10 May 2001), pp. 1-13. doi: 10.21608/asat.2001.24778
A-N., Z. GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS. EKB Journal Management System, 2001; 9(ASAT Conference, 8-10 May 2001): 1-13. doi: 10.21608/asat.2001.24778

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  XML 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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