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Auto Credit Based on amoldymuffin's Chinook in progress
WARNING!!!! This is not an easy flyer, itrequires tedious adjustments. roll and yaw are controlled via rcn nozzles, jets are via vtol and rotors throttle. suggested take off throttle: 45%, use rcn to stabalize then gradually increase vtol. as the helo slants forward flatten with rcn and iincrease throttle, throttle should NOT exceed 78% or else the helo WILL flip backwards even with full jets and counter rcn. Hope everyone enjoys and i am gonna work on one with larger jets but it will be another day
Specifications
General Characteristics
- Predecessor Chinook in progress
- Created On Windows
- Wingspan 13.1ft (4.0m)
- Length 53.5ft (16.3m)
- Height 16.0ft (4.9m)
- Empty Weight 8,972lbs (4,070kg)
- Loaded Weight 18,309lbs (8,305kg)
Performance
- Power/Weight Ratio 1.104
- Horse Power/Weight Ratio 0.327
- Wing Loading 27.5lbs/ft2 (134.4kg/m2)
- Wing Area 665.2ft2 (61.8m2)
- Drag Points 8078
Parts
- Number of Parts 94
- Control Surfaces 0
- Performance Cost 415
