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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2019
/
Article
/
Tab 2
/
Research Article
Conceptual Design of an Unmanned Fixed-Wing Aerial Vehicle Based on Alternative Energy
Table 2
Conceptual design data.
Parameter
Value
0.74 m
4.5152 kg
12.35
0.009
0.7477
122
0
0.2446 m
257,835.61