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Static hot-fire testing of a green hybrid rocket engine

This paper presents the conduct of the hot-fire testing for a green hybrid rocket engine. The hybrid rocket engine consists of liquid nitrous oxide (N2O) as the oxidizer, with the stearic acid as the solid fuel and the incorporation of carbon nanotube and aluminum powder as the additives. From the c...

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Main Authors: Ahmad, Mohamed Tarmizi, Jagannathan, Anudiipnath, Abidin, Razali, Zhahir, Amzari, Saniman, Muhammad Nur Farhan
Format: Article
Language:English
English
Published: Aeronautical and Astronautical Society of the Republic of China 2014
Subjects:
Aerospace engineering
Jet propulsion
Online Access:http://psasir.upm.edu.my/id/eprint/111004/1/Static%20Hot-Fire%20Testing%20of%20a%20Green%20Hybrid%20Rocket%20Engine.pdf
http://psasir.upm.edu.my/id/eprint/111004/
https://www.airitilibrary.com/Article/Detail/P20140627004-N202403020027-00030
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spelling my.upm.eprints.1110042024-04-23T01:16:18Z http://psasir.upm.edu.my/id/eprint/111004/ Static hot-fire testing of a green hybrid rocket engine Ahmad, Mohamed Tarmizi Jagannathan, Anudiipnath Abidin, Razali Zhahir, Amzari Saniman, Muhammad Nur Farhan This paper presents the conduct of the hot-fire testing for a green hybrid rocket engine. The hybrid rocket engine consists of liquid nitrous oxide (N2O) as the oxidizer, with the stearic acid as the solid fuel and the incorporation of carbon nanotube and aluminum powder as the additives. From the conducted experimental, all systems that have been designed and developed in this study for the green hybrid rocket engine are demonstrated to be successful and fully functional, which also include the radio frequency control unit. Based on the results of the experiment, the developed laboratory-scale green hybrid rocket motor has been successfully ignited and produced a maximum thrust of 348 N, with the maximum combustion chamber pressure is recorded as 14 bar. In addition, several suggestions to improve the hybrid rocket engine design are also discussed. Aeronautical and Astronautical Society of the Republic of China 2014-03-13 Article PeerReviewed text en http://psasir.upm.edu.my/id/eprint/111004/1/Static%20Hot-Fire%20Testing%20of%20a%20Green%20Hybrid%20Rocket%20Engine.pdf Ahmad, Mohamed Tarmizi and Jagannathan, Anudiipnath and Abidin, Razali and Zhahir, Amzari and Saniman, Muhammad Nur Farhan (2014) Static hot-fire testing of a green hybrid rocket engine. Journal of Aeronautics, Astronautics and Aviation, 56 (1S). art. no. 30. pp. 405-417. ISSN 1990-7710 https://www.airitilibrary.com/Article/Detail/P20140627004-N202403020027-00030 Aerospace engineering Jet propulsion 10.6125/JoAAA.202403_56(1S).29 English
institution Universiti Putra Malaysia
building UPM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider Universiti Putra Malaysia
content_source UPM Institutional Repository
url_provider http://psasir.upm.edu.my/
language English
English
topic Aerospace engineering
Jet propulsion
spellingShingle Aerospace engineering
Jet propulsion
Ahmad, Mohamed Tarmizi
Jagannathan, Anudiipnath
Abidin, Razali
Zhahir, Amzari
Saniman, Muhammad Nur Farhan
Static hot-fire testing of a green hybrid rocket engine
description This paper presents the conduct of the hot-fire testing for a green hybrid rocket engine. The hybrid rocket engine consists of liquid nitrous oxide (N2O) as the oxidizer, with the stearic acid as the solid fuel and the incorporation of carbon nanotube and aluminum powder as the additives. From the conducted experimental, all systems that have been designed and developed in this study for the green hybrid rocket engine are demonstrated to be successful and fully functional, which also include the radio frequency control unit. Based on the results of the experiment, the developed laboratory-scale green hybrid rocket motor has been successfully ignited and produced a maximum thrust of 348 N, with the maximum combustion chamber pressure is recorded as 14 bar. In addition, several suggestions to improve the hybrid rocket engine design are also discussed.
format Article
author Ahmad, Mohamed Tarmizi
Jagannathan, Anudiipnath
Abidin, Razali
Zhahir, Amzari
Saniman, Muhammad Nur Farhan
author_facet Ahmad, Mohamed Tarmizi
Jagannathan, Anudiipnath
Abidin, Razali
Zhahir, Amzari
Saniman, Muhammad Nur Farhan
author_sort Ahmad, Mohamed Tarmizi
title Static hot-fire testing of a green hybrid rocket engine
title_short Static hot-fire testing of a green hybrid rocket engine
title_full Static hot-fire testing of a green hybrid rocket engine
title_fullStr Static hot-fire testing of a green hybrid rocket engine
title_full_unstemmed Static hot-fire testing of a green hybrid rocket engine
title_sort static hot-fire testing of a green hybrid rocket engine
publisher Aeronautical and Astronautical Society of the Republic of China
publishDate 2014
url http://psasir.upm.edu.my/id/eprint/111004/1/Static%20Hot-Fire%20Testing%20of%20a%20Green%20Hybrid%20Rocket%20Engine.pdf
http://psasir.upm.edu.my/id/eprint/111004/
https://www.airitilibrary.com/Article/Detail/P20140627004-N202403020027-00030
_version_ 1797911380770160640
score 13.222552

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