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24425

EFFECT OF POST-CHAMBER ON COMBUSTION EFFICIENCY IN HYBRID ROCKET MOTORS

Article

Last updated: 24 Dec 2024

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Abstract

In recent years hybrid propulsion has attracted widespread attention in view of a number of potentially attractive features, which could combine the advantages of both liquid and solid rocket motors. This article compares the characteristics of the hybrid propulsion system with those of solid and liquid propulsion systems. Because of the low combustion efficiency of the hybrid systems, the enhancement of the hybrid combustion efficiency, by means of the post-combustion chamber, is investi-
gated theoretically and experimentally.

DOI

10.21608/asat.2013.24425

Keywords

Rocket motor, Hybrid propulsion, Regression rate

Authors

First Name

A.

Last Name

Makle

MiddleName

-

Affiliation

Egyptian Armed Forces.

Email

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City

-

Orcid

-

First Name

A-N.

Last Name

Zaye

MiddleName

-

Affiliation

Egyptian Armed Forces.

Email

-

City

-

Orcid

-

First Name

H.

Last Name

Abdalla

MiddleName

-

Affiliation

Egyptian Armed Forces.

Email

-

City

-

Orcid

-

First Name

M.

Last Name

EI-Senbawi

MiddleName

-

Affiliation

Egyptian Armed Forces.

Email

-

City

-

Orcid

-

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

253

Page End

266

Print ISSN

2090-0678

Online ISSN

2636-364X

Link

https://asat.journals.ekb.eg/article_24425.html

Detail API

https://asat.journals.ekb.eg/service?article_code=24425

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

EFFECT OF POST-CHAMBER ON COMBUSTION EFFICIENCY IN HYBRID ROCKET MOTORS

Details

Type

Article

Created At

22 Jan 2023