Proof of concept - Gyro
232 Meepmaster87
6.1 years ago
Unlisted
No Tags
Ignoring the poor design of the helicopter, I am rather happy to present the first proof of concept for a gyroscopic high mobility craft. I must first thank @randomusername for aiding me in the gyroscopic brain (third picture)
The concept is a rather simple one, using high power gyroscopes to replace flaps in order to increase mobility. This is the first craft, a simple helicopter.
Use VTOL to increase/decrease the power of the main rotor
Use throttle for increased Yaw stability
Pitch, Roll and Yaw are all the same but are gyroscopic and non self righting.
AG 1 to activate the stabiliser.
Specifications
General Characteristics
- Successors 1 airplane(s)
- Created On Windows
- Wingspan 14.3ft (4.4m)
- Length 30.1ft (9.2m)
- Height 12.4ft (3.8m)
- Empty Weight 6,622lbs (3,003kg)
- Loaded Weight 12,715lbs (5,767kg)
Performance
- Power/Weight Ratio 1.06
- Horse Power/Weight Ratio 0.039
- Wing Loading 157.5lbs/ft2 (769.0kg/m2)
- Wing Area 80.7ft2 (7.5m2)
- Drag Points 6368
Parts
- Number of Parts 124
- Control Surfaces 6
- Performance Cost 435