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

• 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

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...