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Auto Credit Based on SturerEmil's XB-40 V1
Short (Fictional) History: after the initial flight test of the the V-1 prototype, the Navy was underwhelmed by the performance, and lack of armaments. the Army however, showed interest in the project and requested a prototype with minor modifications giving rise to the V-2 prototype, apart from slight wing changes, the airframes are nearly identical. the armament carried by the V-2 would have been the same on the V-1, however it was not tested on that variant.
Specifications
General Characteristics
- Predecessor XB-40 V1
- Created On Windows
- Wingspan 24.3ft (7.4m)
- Length 30.6ft (9.3m)
- Height 9.9ft (3.0m)
- Empty Weight 6,209lbs (2,816kg)
- Loaded Weight 7,633lbs (3,462kg)
Performance
- Horse Power/Weight Ratio 0.262
- Wing Loading 37.1lbs/ft2 (181.1kg/m2)
- Wing Area 205.8ft2 (19.1m2)
- Drag Points 1861
Parts
- Number of Parts 48
- Control Surfaces 8
- Performance Cost 361
