High entropy alloy as metal additive for hybrid rocket propellant

A typical solid propellant used in rocket propulsion systems is made from polymeric fuel, crystalline liquid binder and additives. In comparison to conventional propulsion systems, hybrid propulsion is more safe, reliable and environmentally friendly. However, the hybrid systems have some drawbacks,...

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Main Authors: Mohamad Jamil, Nur Arifah, Mohamaddiah, Ahmad Hadi, Azami, Muhammad Hanafi, Nordin, Norhuda Hidayah
Format: Article
Language:English
English
Published: Elsevier 2023
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spelling my.iium.irep.1013562023-06-21T08:06:54Z http://irep.iium.edu.my/101356/ High entropy alloy as metal additive for hybrid rocket propellant Mohamad Jamil, Nur Arifah Mohamaddiah, Ahmad Hadi Azami, Muhammad Hanafi Nordin, Norhuda Hidayah TL780 Rockets TP200 Manufacture and use of chemicals TP315 Fuel A typical solid propellant used in rocket propulsion systems is made from polymeric fuel, crystalline liquid binder and additives. In comparison to conventional propulsion systems, hybrid propulsion is more safe, reliable and environmentally friendly. However, the hybrid systems have some drawbacks, including low fuel regression rates and low combustion efficiency. As a result, several approaches have been developed to increase the rate of solid fuel regression rate including the introduction of metal additives to the system. Nowadays, high entropy alloys (HEA) are among the most advanced materials for high performance applications. This alloy has a potential to replace the existing metal additives in hybrid propulsion systems. The present work proposes a new composition based on Paraffin wax fuel, loaded with high entropy alloy as a metal additive for hybrid propulsion systems using the following ratio of 80:20. Therefore, this research explores the efficacy of high entropy alloys as additives for hybrid propulsion systems. Characterizations and thermal analysis of solid fuel using X-ray diffraction (XRD), differential scanning calorimetry (DSC) and thermogravimetric analysis are carried out to determine the structure, thermal decomposition and energy characteristics of the solid fuel with the HEA as additive. XRD result shows that HEA in a form of solid solutions produces BCC and FCC structures. Thermal analysis of paraffin wax with the addition of HEA gives the maximum value of 136.34 J/g for the total latent heat of the mixture. It is concluded that HEA increases the energy released from the fuel by 86.92 % compared to pure paraffin wax fuel. The mixture of paraffin and HEA fuel has a prospect to be used as future rocket fuel. Elsevier 2023-02-08 Article PeerReviewed application/pdf en http://irep.iium.edu.my/101356/1/101356_High%20entropy%20alloy%20as%20metal%20additive%20for%20hybrid.pdf application/pdf en http://irep.iium.edu.my/101356/2/101356_High%20entropy%20alloy%20as%20metal%20additive%20for%20hybrid_Scopus.pdf Mohamad Jamil, Nur Arifah and Mohamaddiah, Ahmad Hadi and Azami, Muhammad Hanafi and Nordin, Norhuda Hidayah (2023) High entropy alloy as metal additive for hybrid rocket propellant. Materials Today: Proceedings, 75 (Part 1 (January 2023)). pp. 140-146. E-ISSN 2214-7853 https://www.sciencedirect.com/science/article/abs/pii/S2214785322067761 10.1016/j.matpr.2022.10.257
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
TP200 Manufacture and use of chemicals
TP315 Fuel
spellingShingle TL780 Rockets
TP200 Manufacture and use of chemicals
TP315 Fuel
Mohamad Jamil, Nur Arifah
Mohamaddiah, Ahmad Hadi
Azami, Muhammad Hanafi
Nordin, Norhuda Hidayah
High entropy alloy as metal additive for hybrid rocket propellant
description A typical solid propellant used in rocket propulsion systems is made from polymeric fuel, crystalline liquid binder and additives. In comparison to conventional propulsion systems, hybrid propulsion is more safe, reliable and environmentally friendly. However, the hybrid systems have some drawbacks, including low fuel regression rates and low combustion efficiency. As a result, several approaches have been developed to increase the rate of solid fuel regression rate including the introduction of metal additives to the system. Nowadays, high entropy alloys (HEA) are among the most advanced materials for high performance applications. This alloy has a potential to replace the existing metal additives in hybrid propulsion systems. The present work proposes a new composition based on Paraffin wax fuel, loaded with high entropy alloy as a metal additive for hybrid propulsion systems using the following ratio of 80:20. Therefore, this research explores the efficacy of high entropy alloys as additives for hybrid propulsion systems. Characterizations and thermal analysis of solid fuel using X-ray diffraction (XRD), differential scanning calorimetry (DSC) and thermogravimetric analysis are carried out to determine the structure, thermal decomposition and energy characteristics of the solid fuel with the HEA as additive. XRD result shows that HEA in a form of solid solutions produces BCC and FCC structures. Thermal analysis of paraffin wax with the addition of HEA gives the maximum value of 136.34 J/g for the total latent heat of the mixture. It is concluded that HEA increases the energy released from the fuel by 86.92 % compared to pure paraffin wax fuel. The mixture of paraffin and HEA fuel has a prospect to be used as future rocket fuel.
format Article
author Mohamad Jamil, Nur Arifah
Mohamaddiah, Ahmad Hadi
Azami, Muhammad Hanafi
Nordin, Norhuda Hidayah
author_facet Mohamad Jamil, Nur Arifah
Mohamaddiah, Ahmad Hadi
Azami, Muhammad Hanafi
Nordin, Norhuda Hidayah
author_sort Mohamad Jamil, Nur Arifah
title High entropy alloy as metal additive for hybrid rocket propellant
title_short High entropy alloy as metal additive for hybrid rocket propellant
title_full High entropy alloy as metal additive for hybrid rocket propellant
title_fullStr High entropy alloy as metal additive for hybrid rocket propellant
title_full_unstemmed High entropy alloy as metal additive for hybrid rocket propellant
title_sort high entropy alloy as metal additive for hybrid rocket propellant
publisher Elsevier
publishDate 2023
url http://irep.iium.edu.my/101356/1/101356_High%20entropy%20alloy%20as%20metal%20additive%20for%20hybrid.pdf
http://irep.iium.edu.my/101356/2/101356_High%20entropy%20alloy%20as%20metal%20additive%20for%20hybrid_Scopus.pdf
http://irep.iium.edu.my/101356/
https://www.sciencedirect.com/science/article/abs/pii/S2214785322067761
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score 13.160551