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PX-12B Cyclone

4,069 JSTQ  3 months ago

Aspire to become a master of playing vector!

Do you think I would give up because of data loss? No, although my plan to manufacture tanks was temporarily abandoned due to the removal of semi-finished products, I just switched to another plan.

As a gateway to return, this aircraft adopts some new technologies, including:

Mach ring

The engine of this aircraft has been redesigned, and although replacing the phone resulted in data being deleted, the more high-performance equipment allows me to be compatible with a larger number of parts, so I completed the production of the Mach ring.

Mode: Dog Fight

Transforming the principle of angle of attack suppression from minimum speed selection to angle of attack limiter, optimizing flight control, and increasing speed limiter to maintain around the optimal turning speed, significantly improving maneuverability. (But it's still relatively simple)
AG7 to open.At the same time, when the speed is below 600km/h, pull VTOL to the lowest to unlock AOA

brief introduction

PX-12B, It was launched by Kissa Federation in 165 AD under the threat of the superior performance and cost-effectiveness of the Skira Republic's M-12A fighter jet. Under the pressure of reality, the Federation was forced to abandon its usual idea of high-altitude and high-speed interceptors and began pursuing the low altitude, high-speed, and high maneuverability of fighter jets.
The initial plan implemented, PX-2A, was a twin engine medium multirole fighter aircraft with a mid coupled canard and delta wing layout, emphasizing more on multifunctionality rather than maneuverability. In subsequent discussions, the design bureau believes that this plan may result in the fighter's performance not meeting expectations. Moreover, the reform of the Federal Air Force proposed the theory of dual aircraft high-altitude and low altitude coordination, emphasizing more on the maneuverability of the PX-12, so this plan was rejected.
The new plan is named PX-12B. Compared to before, this scheme consists of a single engine and a near coupled canard wing. Although the number of engines is reduced by one, the near coupled canard wing has stronger subsonic maneuverability. At the same time, due to the high flight control requirements of delta wing aircraft, they have made some improvements to the existing flight control, greatly enhancing maneuverability.
At the end of 168, the aircraft completed its test flight and the Air Force gradually began using it. It, together with PX-9C, forms the new force of the Federal Air Force.

AG1:Cockpit cover
AG2:Deceleration Umbrella
AG3:Light
AG4:Discard all mounts
AG5:HMDS
AG6:Eject
AG7:DOG FIGHT

Spotlights

General Characteristics

  • Created On Android
  • Wingspan 44.3ft (13.5m)
  • Length 56.3ft (17.2m)
  • Height 20.2ft (6.2m)
  • Empty Weight N/A
  • Loaded Weight 21,997lbs (9,977kg)

Performance

  • Power/Weight Ratio 13.546
  • Wing Loading 26.7lbs/ft2 (130.2kg/m2)
  • Wing Area 824.8ft2 (76.6m2)
  • Drag Points 4323

Parts

  • Number of Parts 339
  • Control Surfaces 2
  • Performance Cost 2,564