Development of pressurised burning rate test rig for solid propellant [electronic resource] /

Project Paper (Sarjana Muda Kejuruteraan Mekanikal (Aeronautik)) - Universiti Teknologi Malaysia, 2007

Bibliographic Details
Main Authors: 428135 Nasrulhakim Musa, Fakulti Kejuruteraan Mekanikal
Format:
Language:eng
Published: Skudai : Universiti Teknologi Malaysia, 2007
Subjects:
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author 428135 Nasrulhakim Musa
Fakulti Kejuruteraan Mekanikal
author_facet 428135 Nasrulhakim Musa
Fakulti Kejuruteraan Mekanikal
author_sort 428135 Nasrulhakim Musa
collection OCEAN
description Project Paper (Sarjana Muda Kejuruteraan Mekanikal (Aeronautik)) - Universiti Teknologi Malaysia, 2007
first_indexed 2024-03-05T09:00:44Z
format
id KOHA-OAI-TEST:410371
institution Universiti Teknologi Malaysia - OCEAN
language eng
last_indexed 2024-03-05T09:00:44Z
publishDate 2007
publisher Skudai : Universiti Teknologi Malaysia,
record_format dspace
spelling KOHA-OAI-TEST:4103712020-12-19T17:14:19ZDevelopment of pressurised burning rate test rig for solid propellant [electronic resource] / 428135 Nasrulhakim Musa Fakulti Kejuruteraan Mekanikal Skudai : Universiti Teknologi Malaysia,2007engProject Paper (Sarjana Muda Kejuruteraan Mekanikal (Aeronautik)) - Universiti Teknologi Malaysia, 2007Includes bibliographical referencesPSZJBLRocket planesSolid propellants
spellingShingle Rocket planes
Solid propellants
428135 Nasrulhakim Musa
Fakulti Kejuruteraan Mekanikal
Development of pressurised burning rate test rig for solid propellant [electronic resource] /
title Development of pressurised burning rate test rig for solid propellant [electronic resource] /
title_full Development of pressurised burning rate test rig for solid propellant [electronic resource] /
title_fullStr Development of pressurised burning rate test rig for solid propellant [electronic resource] /
title_full_unstemmed Development of pressurised burning rate test rig for solid propellant [electronic resource] /
title_short Development of pressurised burning rate test rig for solid propellant [electronic resource] /
title_sort development of pressurised burning rate test rig for solid propellant electronic resource
topic Rocket planes
Solid propellants
work_keys_str_mv AT 428135nasrulhakimmusa developmentofpressurisedburningratetestrigforsolidpropellantelectronicresource
AT fakultikejuruteraanmekanikal developmentofpressurisedburningratetestrigforsolidpropellantelectronicresource