Project of a Part 103 electric aircraft with my rod end folding wing system, wich allows the wings to fold and unfold easily and overlap on top of the aircraft, (see my previous projects). With this design the wings rise when we fold them and pass over the rudder.
Its specifications would be:
Wingspan: 8,80 m
Length: 5,30 m
Wing area: 10,5 m2
Empty weight: 115 k
Maxi weight: About 220 k
Wing loading: 21 k/m2
Electric motor: 20/25 kw
Motor + controler weight: 10 k
Batteries weight: 30 or 45 k .
With a 30 k batterie the empty plane can weight 75 k, but only 60 k with a 45 k batterie, unless a 15 k batterie could be considered as 5 gal fuel?
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