Transient thermal analysis of solid propellant rocket motor / Dr. Ts. Ahmad Hussein Abdul Hamid ... [et al.]

• Главные авторы: Abdul Hamid, Ahmad Hussein (Автор), Mohamad Aliman, Mohamad Haziq (Автор), Salleh, Zuraidah (Автор), Sujana, Mohammad Juani (Автор), Ismail, Osmera (Автор), Muhammad, Mohamad Amirul (Автор), Mohd Fazli, Mohamad Akmal (Автор)
• Формат: ‌
• Опубликовано: Smart Manufacturing Research Institute (SMRI), 2022-03.
• Предметы: Article; PeerReviewed
• Online-ссылка: Link Metadata

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 li...