Transient thermal analysis of solid propellant rocket motor / Dr. Ts. Ahmad Hussein Abdul Hamid … [et al.]
The creation of stable, high-temperature combustion of propellant is critical in the operation of rocket engines. Due to the high operating temperature and pressure, it is likely that the structural strength of the rocket’s engine component will deteriorate. This will eventually increase the likelih...
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Main Authors: | Abdul Hamid, Ahmad Hussein, Mohamad Aliman, Mohamad Haziq, Salleh, Zuraidah, Sujana, Mohammad Juani, Ismail, Osmera, Muhammad, Mohamad Amirul, Mohd Fazli, Mohamad Akmal |
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Format: | Article |
Language: | English |
Published: |
Smart Manufacturing Research Institute (SMRI)
2022
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Online Access: | https://ir.uitm.edu.my/id/eprint/66458/1/66458.pdf https://ir.uitm.edu.my/id/eprint/66458/ https://jaeds.uitm.edu.my/ |
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