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24778

GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS

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Last updated: 04 Jan 2025

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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.

DOI

10.21608/asat.2001.24778

Keywords

Rocket motor, Solid propellant, Cruciform grain, Triform grain

Authors

First Name

ZAYED

Last Name

A-N.

MiddleName

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Orcid

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Volume

9

Article Issue

ASAT Conference, 8-10 May 2001

Related Issue

4547

Issue Date

2001-05-01

Receive Date

2019-01-15

Publish Date

2001-05-01

Page Start

1

Page End

13

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 9_Issue ASAT Conference, 8-10 May 2001_Pages 1-13.pdf

PDF . 1.4MB

Link

https://asat.journals.ekb.eg/article_24778.html

Detail API

https://asat.journals.ekb.eg/service?article_code=24778

Order

17

Type

Original Article

Type Code

737

Publication Type

Journal

Publication Title

International Conference on Aerospace Sciences and Aviation Technology

Publication Link

https://asat.journals.ekb.eg/

MainTitle

GEOMETRIC ANALYSIS OF CRUCIFORM AND TRIFORM SOLID PROPELLANT GRAINS

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Article

Created At

22 Jan 2023