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24412

EXPERIMENTAL STUDY OF LAB-SCALE HTPB/GOX HYBRID ROCKET MOTOR

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Last updated: 24 Dec 2024

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Abstract

The presented paper introduces main results obtained during the course of static tests carried out for reaching a proper design of testing hybrid motor using several compositions of hydroxy terminated polybutadiene (HTPB) fuel binder and some additives with gaseous oxygen as an oxidizer. The results of preliminary experiments for testing motor design are presented. Investigation on the methods of enhancing the regression rate for the HTPB fuel used in HTPB/GOX testing hybrid motor is presented. The effect of the addition of Ammonium Perchlorate (AP) and aluminum (Al) to the fuel binder was also taken into consideration.

DOI

10.21608/asat.2013.24412

Authors

First Name

HOSAM,

Last Name

M.

MiddleName

E.

Affiliation

Egyptian Armed Forces, MTC, Cairo - Egypt.

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Volume

10

Article Issue

10th International Conference On Aerospace Sciences & Aviation Technology

Related Issue

4497

Issue Date

2003-05-01

Receive Date

2019-01-14

Publish Date

2003-05-01

Page Start

99

Page End

107

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_24412.html

Detail API

https://asat.journals.ekb.eg/service?article_code=24412

Order

8

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 STUDY OF LAB-SCALE HTPB/GOX HYBRID ROCKET MOTOR

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Article

Created At

22 Jan 2023