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MiG-29UB Fulcrum-C

12.1k logizAircrafts  6.1 years ago
Auto Credit Based on Watcing's SuperFulcrum Ver.Wat

The Mikoyan MiG-29UB (NATO reporting name: Fulcrum-C) is a twin-engine jet fighter aircraft designed in the Soviet Union.

Developed by the Mikoyan design bureau as an air superiority fighter during the 1970s, the MiG-29, along with the larger Sukhoi Su-27, was developed to counter new U.S. fighters such as the McDonnell Douglas F-15 Eagle and the General Dynamics F-16 Fighting Falcon.

The MiG-29 entered service with the Soviet Air Forces in 1982.

Stats are:
Speed @35,000 feet - Mach 2.25, 2.100 Km/h, 1310 mph
Speed @1000 feet - Mach 1.13, 1400 Km/H, 870 mph
Max G-Load - 8 to 9 G's.

Controls:
Regular controls
Flaps retract with AG1
Afterburner mode activates with "Throttle" and AG2
Canopy closes with AG3
Dragchute deploys with AG4.

General Characteristics

  • Predecessor SuperFulcrum Ver.Wat
  • Created On Windows
  • Wingspan 40.2ft (12.3m)
  • Length 65.1ft (19.8m)
  • Height 16.8ft (5.1m)
  • Empty Weight N/A
  • Loaded Weight 39,833lbs (18,068kg)

Performance

  • Power/Weight Ratio 8.801
  • Wing Loading 12.5lbs/ft2 (61.1kg/m2)
  • Wing Area 3,180.7ft2 (295.5m2)
  • Drag Points 13706

Parts

  • Number of Parts 674
  • Control Surfaces 8
  • Performance Cost 2,458