Design of a heat pipe for spacecraft cooling

المؤلفون

  • Mohamed Amer Ali Rahim المؤلف
  • Abdossalam Mohamed Ahmed Ashek المؤلف
  • Mohamed Omran Mohamed Sefreta المؤلف
  • Tarek M M Khalifa المؤلف

الكلمات المفتاحية:

Heat pipe, thermal management, spacecraft cooling, phase change, thermal conductivity.

الملخص

Heat pipes are highly efficient thermal management devices that transfer heat utilizing the phase change of a working fluid. Their ability to achieve thermal conductivities far exceeding those of solid conductors makes them ideal for extreme environments, such as spacecraft thermal control systems. This study focuses on designing a heat pipe for spacecraft cooling, addressing challenges such as weight and space limitations. The design process incorporates thermodynamic principles, heat transfer, and structural mechanics, to ensure optimal performance under stringent conditions.

السير الشخصية للمؤلفين

  • Mohamed Amer Ali Rahim

    Mechanical Engineering - Higher institute of science and technology / Tripoli

  • Abdossalam Mohamed Ahmed Ashek

    Mechanical Engineering - Higher institute of science and technology / Tripoli

  • Mohamed Omran Mohamed Sefreta

    Mechanical Engineering - Higher institute of science and technology / Tripoli

  • Tarek M M Khalifa

    Mechanical Engineering - Higher institute of science and technology / Tripoli

التنزيلات

منشور

2025-12-20

كيفية الاقتباس

Design of a heat pipe for spacecraft cooling. (2025). مجلة تاج المعرفة, 1(الرابع). https://histt.edu.ly/ojs/index.php/tajournal/article/view/109