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

• 主要な著者: Abdul Hamid, Ahmad Hussein (著者), Mohamad Aliman, Mohamad Haziq (著者), Salleh, Zuraidah (著者), Sujana, Mohammad Juani (著者), Ismail, Osmera (著者), Muhammad, Mohamad Amirul (著者), Mohd Fazli, Mohamad Akmal (著者)
• フォーマット: 図書
• 出版事項: Smart Manufacturing Research Institute (SMRI), 2022-03.
• 主題: Article; PeerReviewed
• オンライン･アクセス: 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...