Active thermal control system for nano-satellites

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...

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Bibliographic Details
Main Author: Karthikeyan Baskaran
Other Authors: Low Kay Soon
Format: Theses and Dissertations
Language:English
Published: 2015
Subjects:
Online Access:http://hdl.handle.net/10356/64879
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Institution: Nanyang Technological University
Language: English
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