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Basic proof of concept for dual main rotor design along with a static RCN control based tail. dual rotors seems to offset rotation issues normally solved by active tail rotors. low fuel amount on test platform though controlled flight is possible. set VTOL completely down for 30* main rotor deflection.
Specifications
General Characteristics
- Created On Android
- Wingspan 65.4ft (19.9m)
- Length 65.4ft (19.9m)
- Height 15.6ft (4.8m)
- Empty Weight 22,553lbs (10,230kg)
- Loaded Weight 24,197lbs (10,975kg)
Performance
- Power/Weight Ratio 3.714
- Wing Loading 52.7lbs/ft2 (257.3kg/m2)
- Wing Area 459.1ft2 (42.7m2)
- Drag Points 10879
Parts
- Number of Parts 119
- Control Surfaces 0
- Performance Cost 369
