Thermal analysis of the 6U CubeSat Velox-II

• المؤلف الرئيسي: Ranjana Shivakumar
• مؤلفون آخرون: Sunil Chandrakant Joshi
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2015
• الموضوعات: DRNTU::Engineering::Aeronautical engineering
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/64807
• المؤسسة: Nanyang Technological University

Development and experimentation of small satellites have become feasible with the advancements in technologies in aerospace industries. The satellites are subjected to various types of thermal loads or radiative loads while in orbit. Every component of the spacecraft has its own temperature...