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Mathematical Problems in Engineering
/
2015
/
Article
/
Tab 1
/
Research Article
Optimal Sizing of a Photovoltaic-Hydrogen Power System for HALE Aircraft by means of Particle Swarm Optimization
Table 1
Hale aircrafts specifications taken from [
19
].
Aircraft
Total mass (kg)
Empty mass (kg)
Wing area (m
2
)
Pathfinder
252
207
70.8
Pathfinder +
315
247
87.1
Helios HP01
719
600
186.6