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Design and theoretical performance prediction of hydrogen peroxide hybrid thruster

A design procedure to realize a hybrid rocket engine that uses hydrogen peroxide as the oxidizer and a solid polymer as the fuel is presented. In the design procedure, the products of decomposition and of combustion at different stations are calculated by linking a standard complex chemical-equilibr...

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Main Authors: Muhalim, Noor Muhammad Feizal, Krishnan, Subramanian, Mohd. Jaafar, Mohammad Nazri, Wan Ali, Wan Khairuddin
Format: Conference or Workshop Item
Published: 2009
Subjects:
TJ Mechanical engineering and machinery
Online Access:http://eprints.utm.my/id/eprint/15036/
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spelling my.utm.150362020-07-20T01:23:53Z http://eprints.utm.my/id/eprint/15036/ Design and theoretical performance prediction of hydrogen peroxide hybrid thruster Muhalim, Noor Muhammad Feizal Krishnan, Subramanian Mohd. Jaafar, Mohammad Nazri Wan Ali, Wan Khairuddin TJ Mechanical engineering and machinery A design procedure to realize a hybrid rocket engine that uses hydrogen peroxide as the oxidizer and a solid polymer as the fuel is presented. In the design procedure, the products of decomposition and of combustion at different stations are calculated by linking a standard complex chemical-equilibrium program of NASA. For the designed basic-configuration, applying the mass conservation principle, theoretical performance results are presented with propellant-tank pressure and grain port length as parameters. 2009 Conference or Workshop Item PeerReviewed Muhalim, Noor Muhammad Feizal and Krishnan, Subramanian and Mohd. Jaafar, Mohammad Nazri and Wan Ali, Wan Khairuddin (2009) Design and theoretical performance prediction of hydrogen peroxide hybrid thruster. In: Conference on Aerospace Technology of the XXI Century (AEROTECH2009), 2009, Novotel Kuala Lumpur City Center.
institution Universiti Teknologi Malaysia
building UTM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Teknologi Malaysia
content_source UTM Institutional Repository
url_provider http://eprints.utm.my/
topic TJ Mechanical engineering and machinery
spellingShingle TJ Mechanical engineering and machinery
Muhalim, Noor Muhammad Feizal
Krishnan, Subramanian
Mohd. Jaafar, Mohammad Nazri
Wan Ali, Wan Khairuddin
Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
description A design procedure to realize a hybrid rocket engine that uses hydrogen peroxide as the oxidizer and a solid polymer as the fuel is presented. In the design procedure, the products of decomposition and of combustion at different stations are calculated by linking a standard complex chemical-equilibrium program of NASA. For the designed basic-configuration, applying the mass conservation principle, theoretical performance results are presented with propellant-tank pressure and grain port length as parameters.
format Conference or Workshop Item
author Muhalim, Noor Muhammad Feizal
Krishnan, Subramanian
Mohd. Jaafar, Mohammad Nazri
Wan Ali, Wan Khairuddin
author_facet Muhalim, Noor Muhammad Feizal
Krishnan, Subramanian
Mohd. Jaafar, Mohammad Nazri
Wan Ali, Wan Khairuddin
author_sort Muhalim, Noor Muhammad Feizal
title Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
title_short Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
title_full Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
title_fullStr Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
title_full_unstemmed Design and theoretical performance prediction of hydrogen peroxide hybrid thruster
title_sort design and theoretical performance prediction of hydrogen peroxide hybrid thruster
publishDate 2009
url http://eprints.utm.my/id/eprint/15036/
_version_ 1674066110141431808
score 13.160551

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