Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor

This investigation focuses on the regression rate behavior of polylactic acid (PLA) manufactured by fused deposition modeling (FDM) for the hybrid rocket motor (HRM). HRMs generally have many advantages but they suffer from a low regression rate. In view of this, PLA produced by FDM potentially can...

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Main Authors: Abd Razak, Najihah, Azami, Muhammad Hanafi
Format: Article
Language:English
English
Published: Aeronautical and Astronautical Society of the Republic of China 2024
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Online Access:http://irep.iium.edu.my/111377/2/111377_Investigation%20on%20regression%20rate%20behavior%20of%20polylactic%20acid.pdf
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spelling my.iium.irep.1113772024-03-25T07:29:52Z http://irep.iium.edu.my/111377/ Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor Abd Razak, Najihah Azami, Muhammad Hanafi TL780 Rockets TL787 Astronautics This investigation focuses on the regression rate behavior of polylactic acid (PLA) manufactured by fused deposition modeling (FDM) for the hybrid rocket motor (HRM). HRMs generally have many advantages but they suffer from a low regression rate. In view of this, PLA produced by FDM potentially can offer a more environmental-friendly alternative. The primary objective of this study is to determine the regression rate of PLA in HRMs by exploring different geometrical configurations and porosities. Analytical analyses are conducted to evaluate the performance of PLA HRMs in terms of regression rate, thrust and specific impulse. PLA motors with varying configurations and porosities are designed and developed. Static firings are done to demonstrate the motor performance and the collected data is used to establish empirical correlations between regression rate, thrust and specific impulse. The results obtained from this study indicate a minimal percentage of deviation between analytical and experimental regression rates for the PLA use in HRM, ranging between 0.53% at a mass flux of 79 kg⁄m2s to 1.69% at 112 kg⁄m2s. For PLA motor configurations, employing a star port at a mass flux of 50 kg⁄m2s yields maximum specific impulse of 674.52 s. On the other hand, using a cylindrical port or a wagon wheel port at a mass flux of 150 kg⁄m2s results in minimum specific impulse of 80.34 s. Aeronautical and Astronautical Society of the Republic of China 2024-03-01 Article PeerReviewed application/pdf en http://irep.iium.edu.my/111377/2/111377_Investigation%20on%20regression%20rate%20behavior%20of%20polylactic%20acid.pdf application/pdf en http://irep.iium.edu.my/111377/8/111377_Investigation%20on%20regression%20rate%20behavior%20of%20polylactic%20acid_Scopus.pdf Abd Razak, Najihah and Azami, Muhammad Hanafi (2024) Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor. Journaal of Aeronautics, Astronautics and Aviation, 56 (1S). pp. 157-165. ISSN 1990-7710 https://www.ipress.tw/J0039?pWebID=588&pType=4&mSeq=1 https://www.airitilibrary.com/Common/Click_DOI?DOI=10.6125/JoAAA.202403_56(1S).08
institution Universiti Islam Antarabangsa Malaysia
building IIUM Library
collection Institutional Repository
continent Asia
country Malaysia
content_provider International Islamic University Malaysia
content_source IIUM Repository (IREP)
url_provider http://irep.iium.edu.my/
language English
English
topic TL780 Rockets
TL787 Astronautics
spellingShingle TL780 Rockets
TL787 Astronautics
Abd Razak, Najihah
Azami, Muhammad Hanafi
Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor
description This investigation focuses on the regression rate behavior of polylactic acid (PLA) manufactured by fused deposition modeling (FDM) for the hybrid rocket motor (HRM). HRMs generally have many advantages but they suffer from a low regression rate. In view of this, PLA produced by FDM potentially can offer a more environmental-friendly alternative. The primary objective of this study is to determine the regression rate of PLA in HRMs by exploring different geometrical configurations and porosities. Analytical analyses are conducted to evaluate the performance of PLA HRMs in terms of regression rate, thrust and specific impulse. PLA motors with varying configurations and porosities are designed and developed. Static firings are done to demonstrate the motor performance and the collected data is used to establish empirical correlations between regression rate, thrust and specific impulse. The results obtained from this study indicate a minimal percentage of deviation between analytical and experimental regression rates for the PLA use in HRM, ranging between 0.53% at a mass flux of 79 kg⁄m2s to 1.69% at 112 kg⁄m2s. For PLA motor configurations, employing a star port at a mass flux of 50 kg⁄m2s yields maximum specific impulse of 674.52 s. On the other hand, using a cylindrical port or a wagon wheel port at a mass flux of 150 kg⁄m2s results in minimum specific impulse of 80.34 s.
format Article
author Abd Razak, Najihah
Azami, Muhammad Hanafi
author_facet Abd Razak, Najihah
Azami, Muhammad Hanafi
author_sort Abd Razak, Najihah
title Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor
title_short Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor
title_full Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor
title_fullStr Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor
title_full_unstemmed Investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor
title_sort investigation on regression rate behavior of polylactic acid manufactured by fused deposition modelling for hybrid rocket motor
publisher Aeronautical and Astronautical Society of the Republic of China
publishDate 2024
url http://irep.iium.edu.my/111377/2/111377_Investigation%20on%20regression%20rate%20behavior%20of%20polylactic%20acid.pdf
http://irep.iium.edu.my/111377/8/111377_Investigation%20on%20regression%20rate%20behavior%20of%20polylactic%20acid_Scopus.pdf
http://irep.iium.edu.my/111377/
https://www.ipress.tw/J0039?pWebID=588&pType=4&mSeq=1
https://www.airitilibrary.com/Common/Click_DOI?DOI=10.6125/JoAAA.202403_56(1S).08
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score 13.160551