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CCA ED-P-13A Ancalagon

1,110 RondenKiagre  5.7 years ago

An experimental engine testbed/technology demonstrator based on the PF-4C airframe. Capable of sea-level supercruise (930 mph at 80% throttle on the deck) and Mach 3.363 at 77000 ft, with a service ceiling of 105000 ft (can get higher, but is almost uncontrollable by that point).

General Characteristics

  • Successors 1 airplane(s)
  • Created On Windows
  • Wingspan 21.8ft (6.7m)
  • Length 38.8ft (11.8m)
  • Height 12.3ft (3.7m)
  • Empty Weight 4,284lbs (1,943kg)
  • Loaded Weight 10,997lbs (4,988kg)

Performance

  • Power/Weight Ratio 6.13
  • Wing Loading 36.1lbs/ft2 (176.2kg/m2)
  • Wing Area 304.8ft2 (28.3m2)
  • Drag Points 2331

Parts

  • Number of Parts 172
  • Control Surfaces 7
  • Performance Cost 883