Hobby Master – MiG-29 A Fulcrum , ‚553‘ KPAAF – Korean People’s Army Air and Anti-Air Force , North Korea 2015

Popis

- sběratelský model letadla MiG-29A  Fulcrum      1/72  
- provedení: kovový model s plastovými částmi
- model je v kvalitním provedení
- součástí balení je stojánek

                          Mikoyan MiG-29

Mikojan-Gurevič MiG-29 (rusky: МиГ-29, v kódu NATO „Fulcrum“) je dvoumotorový, proudový stíhací letoun k vybojování vzdušné nadvlády. Byl vyvinut v SSSR konstrukční kanceláří Mikojan v 70. letech 20. století. Spolu s větším letounem Suchoj Su-27 vznikl jako odpověď na nové americké letouny McDonnell Douglas F-15 Eagle a General Dynamics F-16 Fighting Falcon. Do služby v sovětském letectvu vstoupil MiG-29 v roce 1982.

The Mikoyan MiG-29 (Russian: Микоян МиГ-29; NATO reporting name: Fulcrum) 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.

MiG-29A (Product 9.12)

Initial production version; entered service in 1983. NATO reporting name is “Fulcrum-A”. 9.12A is the Initial production model version for Warsaw Pact while the 9.12B is the downgraded export version for non-Warsaw Pact nations. It lacks a nuclear weapon delivery system and has initial production radar, ECM and IFF (no ECM and IFF in 9.12B).

General characteristics

• Crew: 1
• Length: 17.32 m (56 ft 10 in)
• Wingspan: 11.36 m (37 ft 3 in)
• Height: 4.73 m (15 ft 6 in)
• Wing area: 38 m² (409 ft²)
• Empty weight: 11,000 kg (24,250 lb)
• Loaded weight: 14,900 kg (33,730 lb)
• Max. takeoff weight: 18,000 kg (44,100 lb)
• Fuel capacity: 3,500 kg (7,716 lb) internal
• Powerplant: 2 × Klimov RD-33 afterburning turbofans, 81.59 kN (18,342 lbf) each

Performance

• Maximum speed:
  • At high altitude: Mach 2.25 (2,400 km/h; 1,490 mph)
  • At low altitude: Mach 1.21 (1,500 km/h; 930 mph)
• Range: 1,430 km (888 mi; 772 nmi) with maximum internal fuel
• Ferry range: 2,100 km (1,300 mi; 1,130 nmi) with 1 drop tank
• Service ceiling: 18,000 m (59,100 ft)
• Rate of climb: 330 m/s (65,000 ft/min) (initial); 109 m/s (21,500 ft/min) (average)  (0–6,000 m)
• Wing loading: 403 kg/m² (82 lb/ft²)
• Thrust/weight: 1.09
• Maximum g-load: 9 g

Armament

• Guns: 1 × 30 mm Gryazev-Shipunov GSh-30-1 autocannon with 150 rounds
• Hardpoints: 7 × hardpoints (6 × underwing, 1 × fuselage) with a capacity of up to 4,000 kg (8,800 lb) of stores and provisions to carry combinations of:
  • Rockets:
    • S-5
    • S-8
    • S-24
  • Missiles:
    • 2 × R-27 R/ER/T/ET/P air-to-air missiles
    • 4 × R-60 AAMs
    • 4 × R-73 AAMs
  • Bombs: 6 × 665 kg (1,466 lb) bombs

Avionics

• Phazotron Rubin radar