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This version uses RCN nozzles to give the fighter more control at higher speeds at the cost of stability at lower speeds. This version is being used to test the flight system to be used on the EAS-430, that will incorporate a 3 axis vector controlled thrust system, a RCN system, and a purpose built airframe designed to maximize maneuverability without the use any control surfaces to minimize drag.
Specifications
General Characteristics
- Created On Windows
- Wingspan 18.5ft (5.6m)
- Length 27.4ft (8.3m)
- Height 5.1ft (1.5m)
- Empty Weight N/A
- Loaded Weight 12,592lbs (5,711kg)
Performance
- Power/Weight Ratio 7.227
- Wing Loading 68.3lbs/ft2 (333.5kg/m2)
- Wing Area 184.3ft2 (17.1m2)
- Drag Points 4890
Parts
- Number of Parts 492
- Control Surfaces 0
- Performance Cost 2,201
