MiG-29UB Fulcrum-C
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.
Specifications
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
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