- $10,000 in Legal Protection (Indemnification)
- $1,000,000 in Legal Protection (Indemnification)
- Waiver from injunctive relief
- Assignable model rights
- $250,000 in Legal Protection (Indemnification)
- Assignable model rights
This is a high definition model of the MiG-29K 'Fulcrum' including high-resolution textures and several armaments including the R-73 'Archer', R-77 'Adder', and EL/L-8222 ECM Pod.
Detailed, articulated rudders, flaps, canopy, landing gear, IFR probe, arrestor, and air brake are provided.
4096x4096 maps are included that cover the fuselage, wings, and cockpit interior. Color, Specular, and Bump maps provided. Photoshop templates available as an extra download.
The Mikoyan MiG-29 (Russian: ???-29* ) (NATO reporting name 'Fulcrum') is a fighter aircraft designed for the air superiority role in the Soviet Union. Developed in the 1970s by the Mikoyan design bureau, it entered service in 1983 and remains in use by the Russian Air Force as well as in many other nations.
The history of the MiG-29, like that of the larger Sukhoi Su-27 'Flanker', started in 1969 when the Soviet Union learned of the U.S. Air Force 'FX' program, which resulted in the F-15 Eagle. The Soviet leadership soon realized that the new American fighter would represent a serious technological advance over all existing Soviet fighters. The MiG-21 'Fishbed' was agile by the standards of its day, but had deficiencies in range, armament, and growth potential. The MiG-23 'Flogger', developed to match the F-4 Phantom II, was fast and had more space for fuel and equipment, but lacked in maneuverability and dogfighting ability. What was needed was a better-balanced fighter with both good agility and sophisticated systems. In response, the Soviet General Staff issued a requirement for a Perspektivnyi Frontovoi Istrebitel (PFI, roughly 'advanced tactical fighter'). Specifications were extremely ambitious, calling for long range, good short-field performance (including the ability to use austere runways), excellent agility, Mach 2+ speed, and heavy armament. The aerodynamic design for the new aircraft was largely carried out by TsAGI, the Russian aerodynamics institute, in collaboration with Sukhoi.
Length: 17.37 m (57 ft)
Wingspan: 11.4 m (37 ft 3 in)
Height: 4.73 m (15 ft 6 in)
Wing area: 38 m (409 ft)
Empty weight: 11,000 kg (24,250 lb)
Loaded weight: 16,800 kg (37,000 lb)
Max takeoff weight: 21,000 kg (46,300 lb)
Powerplant: 2 Klimov RD-33K afterburning turbofans, 86.4 kN (20,725 lbf) each
Maximum speed: 2,445 km/h (1,518 mph)
Range: 700 km combat, 2,900 km ferry (430 mi / 1,800 mi)
Service ceiling: 18,013 m / 59 060 ft (59,100 ft)
Rate of climb: 330 m/s (65,000 ft/min)
Wing loading: 442 kg/m (90.5 lb/ft)