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25121

COMPARISON BETWEEN PARTICLE SIZE DISTRIBUTION OF HEXOGEN AND OCTOGEN DURING FORCED CRYSTALLIZATION

Article

Last updated: 04 Jan 2025

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Abstract

Advanced solid rocket propellants with a low-pressure exponent and minimum signature comprise high- energy nitramine compounds such as hexogen and octogen. To achieve the desired processing conditions and increase the solid loading, the nitramine explosives are required with different grain size. The control of growth rate of crystals of nitramines by stirring, cooling and by crystal habit modifiers has been studied. The influence of these factors on crystal size distributions has been investigated and discussed. The results of both hexogen and octogen are compared.

DOI

10.21608/asat.1999.25121

Keywords

Rocket propellants, Composite rocket propellants, Nitramine propellants, Hexogen, Octogen

Authors

First Name

M.

Last Name

SADEKt

MiddleName

A.

Affiliation

Professor, Dpt. Of chemical engineering, Higher Technological Institute, 10th of Ramadan , Egypt.

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Volume

8

Article Issue

ASAT Conference, 4-6 May 1999

Related Issue

4551

Issue Date

1999-05-01

Receive Date

2019-01-17

Publish Date

1999-05-01

Page Start

1

Page End

8

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_25121.html

Detail API

https://asat.journals.ekb.eg/service?article_code=25121

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50

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

COMPARISON BETWEEN PARTICLE SIZE DISTRIBUTION OF HEXOGEN AND OCTOGEN DURING FORCED CRYSTALLIZATION

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Article

Created At

22 Jan 2023