CTR-1B MK IV
1,969 WorldWideDefenseAeronauticLabs
8.1 years ago
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Auto Credit Based on WorldWideDefenseAeronauticLabs's CTR-1A
Intorducing the final protoyped CTR-1 Bravo model Mark 4. Now fully capable of VTOL and safety parachute for quick horizontal landings (Activation Group 6). Test Pilots now have no complaints for the forward suspension failing and improved balance for maximum effectiveness for the more powerful powerplants. ://: End Training Manual ://:
Specifications
General Characteristics
- Predecessor CTR-1A
- Successors 1 airplane(s)
- Created On iOS
- Wingspan 97.2ft (29.6m)
- Length 56.3ft (17.2m)
- Height 17.4ft (5.3m)
- Empty Weight 13,297lbs (6,031kg)
- Loaded Weight 30,046lbs (13,628kg)
Performance
- Power/Weight Ratio 0.448
- Horse Power/Weight Ratio 0.199
- Wing Loading 40.8lbs/ft2 (199.2kg/m2)
- Wing Area 736.4ft2 (68.4m2)
- Drag Points 9145
Parts
- Number of Parts 124
- Control Surfaces 8
- Performance Cost 859