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24884

HYBRID PROPELLANT ROCKET MOTOR

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Last updated: 24 Dec 2024

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Abstract

The paper deals with hybrid propellant rocket motor as a propulsion unit of prospective rocket weapon systems, as well as a drive unit of some cosmic rocket carriers. There are introduced possible constructional schemes of hybrid propellant rocket motor and is mentioned further on the particular general internal ballistic solution of the solid part of the hybrid propellant.
The paper shows the advantages and disadvantages of such types of propulsion units.

DOI

10.21608/asat.1999.24884

Keywords

Hybrid propulsion, hybrid rocket, Internal Ballistics, Rocket motor

Authors

First Name

Frantitek

Last Name

LUDVIK

MiddleName

-

Affiliation

Prof. Dipl.Eng., Ph.D., Department of Rocketry, Military Academy in Brno, Czech Republic.

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Volume

8

Article Issue

ASAT Conference, 4-6 May 1999

Related Issue

4551

Issue Date

1999-05-01

Receive Date

2019-01-16

Publish Date

1999-05-01

Page Start

1

Page End

15

Print ISSN

2090-0678

Online ISSN

2636-364X

Article File

ASAT_Volume 8_Issue ASAT Conference, 4-6 May 1999_Pages 1-15.pdf

PDF . 2.1MB

Link

https://asat.journals.ekb.eg/article_24884.html

Detail API

https://asat.journals.ekb.eg/service?article_code=24884

Order

14

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

HYBRID PROPELLANT ROCKET MOTOR

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Article

Created At

22 Jan 2023