Solar UAV : design and fabrication of structural test rig for loading and testing a 7.5m half wing
The Solar UAV is a multi-functional aerial vehicle that can be used in many applications. The objective of the project was to design and manufacture a Solar UAV with wingspan of 17.5m, take-off weight of 60kg and having an endurance of 24 hours. To achieve this feat, a lightweight design...
Saved in:
| Main Author: | |
|---|---|
| Other Authors: | |
| Format: | Final Year Project |
| Language: | English |
| Published: |
2013
|
| Subjects: | |
| Online Access: | http://hdl.handle.net/10356/54145 |
| Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
| Institution: | Nanyang Technological University |
| Language: | English |
Be the first to leave a comment!