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...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Theses and Dissertations |
| Language: | English |
| Published: |
2015
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/64879 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Nanyang Technological University |
| Language: | English |