Auto Credit Based on EnderWiggin's PY-AGK 'Olympia' Alpha
Supersonic variable-swept, inline bi-wing powered by two microjets. The third and last variable-sweep concept aircraft in the series. The wings sweep up to 45 degrees based on throttle position, just be careful going from high speed flight to slow flight, as to not over-stress the wings in their extended position.
Specifications
General Characteristics
- Predecessor PY-AGK 'Olympia' Alpha
- Created On Android
- Wingspan 36.6ft (11.2m)
- Length 31.2ft (9.5m)
- Height 7.8ft (2.4m)
- Empty Weight 6,584lbs (2,986kg)
- Loaded Weight 7,249lbs (3,288kg)
Performance
- Power/Weight Ratio 0.93
- Wing Loading 25.8lbs/ft2 (126.0kg/m2)
- Wing Area 280.9ft2 (26.1m2)
- Drag Points 2886
Parts
- Number of Parts 68
- Control Surfaces 6
- Performance Cost 384
@Stingray
They were variable-sweeping wings way back in the 60's. The F-111 Aardvark was built in '64 I think, ten years before the Lancer. These were more of a concept aircraft for SP, the actual concept has been proven. Cheers mate!
Yeah, coupling wing position with throttle position was done over 30 years ago on the F14 and Rockwell B1. @EnderWiggin @EnderWiggin
@Stingray
Thank you?
@spefyjerbf
Thanks!