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The CV-25 is a cargo varient VTOL aircraft. Based on the Boeing QTR (Quad Tilt Rotor), it has a significantly higher external payload capacity than its predecessor, the CH-47 Chinook. ____________________________________Operating Instructions: Control 1: Enables rotor tilt. Pitch: Operates totor tilt. Control 2: Enables winch. Trim: Operates winch. Control 3: Activates winch magnet. ____________________________________Note: If taking of like a traditional fixed wing aircraft, ensure rotors are tilted no more than 45° or they will impact the ground.
Specifications
General Characteristics
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- Wingspan 99.4ft (30.3m)
- Length 89.0ft (27.1m)
- Height 16.3ft (5.0m)
- Empty Weight 32,076lbs (14,549kg)
- Loaded Weight 41,732lbs (18,929kg)
Performance
- Power/Weight Ratio 11.201
- Wing Loading 42.8lbs/ft2 (209.1kg/m2)
- Wing Area 974.6ft2 (90.5m2)
- Drag Points 20911
Parts
- Number of Parts 147
- Control Surfaces 9
- Performance Cost 1,483
