Thermal analysis of the 6U CubeSat Velox-II

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...

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Bibliographic Details
Main Author: Ranjana Shivakumar
Other Authors: Sunil Chandrakant Joshi
Format: Theses and Dissertations
Language:English
Published: 2015
Subjects:
Online Access:http://hdl.handle.net/10356/64807
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Institution: Nanyang Technological University
Language: English
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