مشروع البحث: EVALUATING SOLAR ARRAY POSITIONING DESIGNS FOR SMALL SATELLITES IN DIFFERENT ORBITS
تحميل...
المساهمين
الممولين
رقم التعريف
1329
الباحث
محمد علي الصادق محمد
الوصف
generation capabilities of CubeSats pose a major challenge in ensuring the long-term sustainability
and reliability of these systems. Evaluating the power generated by solar arrays
in a CubeSats satellite is very important and necessary since it has a limitation in the area
of the solar arrays, and therefore the energy on board is small.
This research will study and evaluate the energy output from a 3U CubeSat in both Geosynchronous
and Sun-synchronous orbits with several solar panel design configurations. In
addition, this research creates virtual models to determine the weight penalty for advanced
positioning devices and ensure the packaged size remains suitable for standard 3U CubeSat.
الكلمات الدالة
EVALUATING SOLAR ARRAY POSITIONING DESIGNS