Regression rate end-burning hybrid rocket motor doped with high entropy metallic additives

• Main Authors: Sabri, Muhammad Ezamuddin Ezzad, Roslan, Mohammad Amirul Qayyum, Azami, Muhammad Hanafi, Salleh, Zuraidah
• 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/103724/1/103724_Regression%20rate%20end-burning%20hybrid%20rocket%20motor.pdf; http://irep.iium.edu.my/103724/; https://arc.aiaa.org/doi/10.2514/6.2023-0893
• Institution: Universiti Islam Antarabangsa Malaysia

Hybrid Rocket Motor (HRM) has a critical weakness that impacts performance because of low regression rate. Due to this, extensive investigation has been done on the end-burning hybrid rocket (EBHR) to enhance the regression rate. Analytical studies were conducted on the EBHR to model the internal ba...