Active thermal control system for nano-satellites

• المؤلف الرئيسي: Karthikeyan Baskaran
• مؤلفون آخرون: Low Kay Soon
• التنسيق: Theses and Dissertations
• اللغة: English
• منشور في: 2015
• الموضوعات: DRNTU::Engineering::Aeronautical engineering::Materials of construction
• الوصول للمادة أونلاين: http://hdl.handle.net/10356/64879
• المؤسسة: Nanyang Technological University

Satellites are subjected to various types of thermal loads or radiative loads while in orbit. The evolution of reduction in the size of the satellites led to few important requirements which intend to reduction in size and mass of their subsystems. As a result a device has to be designed in order...