Investigation of hybrid rocket motor regression rate doped with high entropy metallic additives

Investigation of hybrid rocket motor regression rate doped with high entropy metallic additives

Low combustion efficiency and low regression rate in the hybrid rocket limit the implementation of the Hybrid Rocket Motor (HRM) in the propulsion system. Due to this, a comprehensive investigation of utilising the paraffin wax doped with the high entropy metallic additives is used to enhance the re...

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Bibliographic Details
Main Authors: Ismail, Izham Izzat, Mohamad Jamil, Nur Arifah, Mohamad Anuar, Mai Nurul Fareesya, Azami, Muhammad Hanafi, Nordin, Norhuda Hidayah
Format: Conference or Workshop Item
Language:English
Published: American Institute of Aeronautics & Astronautics (AIAA) 2023
Subjects:
TL780 Rockets
TL787 Astronautics
Online Access:http://irep.iium.edu.my/103723/1/103723_Investigation%20of%20hybrid%20rocket%20motor%20regression.pdf
http://irep.iium.edu.my/103723/
https://arc.aiaa.org/doi/abs/10.2514/6.2023-0891
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Institution: Universiti Islam Antarabangsa Malaysia
Language: English

Internet

http://irep.iium.edu.my/103723/1/103723_Investigation%20of%20hybrid%20rocket%20motor%20regression.pdf
http://irep.iium.edu.my/103723/
https://arc.aiaa.org/doi/abs/10.2514/6.2023-0891

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