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23407

Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test

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Last updated: 04 Jan 2025

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Abstract

An experimental data treatment is introduced to manage with the tensile test responses of highly non-linear viscoelastic materials. This work investigates the effects of strain rate and temperature on the behaviour of solid propellant treated as non-linear viscoelastic material. The material investigated was rubber composite based on hydroxylterminated poly butadiene (HTPB).Viscoelastic design properties were derived from the experimentally measured tensile data. Design properties include isochronous stress–strain diagrams at different strain rates and temperatures.

DOI

10.21608/asat.2011.23407

Keywords

Solid propellant, Mechanical behavior, Non-linear viscoelastic, Strain rate

Authors

First Name

W.

Last Name

Adel

MiddleName

M.

Affiliation

Egyptian Armed Forces, Egypt.

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Orcid

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First Name

H.

Last Name

Kamal

MiddleName

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Affiliation

Egyptian Armed Forces, Egypt.

Email

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Orcid

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First Name

D.

Last Name

El-Soualey

MiddleName

-

Affiliation

Professor, High Institute of Technology of 10th Ramadan, October Branch, Egypt.

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Volume

14

Article Issue

AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 – May 24 - 26, 2011

Related Issue

4330

Issue Date

2011-05-01

Receive Date

2019-01-02

Publish Date

2011-05-01

Page Start

1

Page End

11

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 14_Issue AEROSPACE SCIENCES & AVIATION TECHNOLOGY, ASAT - 14 &nd….pdf

PDF . 537.3kB

Link

https://asat.journals.ekb.eg/article_23407.html

Detail API

https://asat.journals.ekb.eg/service?article_code=23407

Order

93

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

Experimental Determination of Some Design Properties of Viscoelastic Solid Propellant Using Uniaxial Tensile Test

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Article

Created At

22 Jan 2023