Auto Credit Based on RTNF's Comet Prototype-IIIA
I think he probably did not improve much. He used a new vertical tail, with the horizontal tail to turn. In addition, he solved the speedbrakes sometimes can not achieve the effect of the problem. The next prototype version I will test the new full-motion tail and adjustable main wing to further enhance maneuverability. If you find some problems with this aircraft or have good electronics, welcome to submit.
In fact, his maneuverability can be further improved when the fuel is reduced. When the fuel is reduced by 50%, the radius is reduced to 800 ft. To better target incoming aircraft
Specifications
Spotlights
- RTNF 7.1 years ago
General Characteristics
- Predecessor Comet Prototype-IIIA
- Successors 2 airplane(s)
- Created On Windows
- Wingspan 23.6ft (7.2m)
- Length 29.3ft (8.9m)
- Height 9.6ft (2.9m)
- Empty Weight N/A
- Loaded Weight 9,434lbs (4,279kg)
Performance
- Power/Weight Ratio 3.573
- Wing Loading 15.2lbs/ft2 (74.1kg/m2)
- Wing Area 622.0ft2 (57.8m2)
- Drag Points 2087
Parts
- Number of Parts 79
- Control Surfaces 3
- Performance Cost 507
Subsequent versions of the fuel in the premise can reach 800ft radius of gyration, the speed is even faster.
https://www.simpleplanes.com/a/1cQ0D9/Comet-NT-Prototype-III