Hobby Master – Mikoyan MiG-29A (9-12A) Fulcrum Fighter Aircraft , ‘7702’ 1.Letka 11.Stíhací Letecký Pluk Vzdušné síly Armády České Republiky (Československé letectvo) / 1st Sqn.11th Fighter Aviation Regiment Czech Air Force (Czechoslovak Air Force) , Žatec 1993

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

Czech Air Force Vzdušné síly Armády České Republiky
Czech Air Force emblem
Founded	1 January 1993
Country	Czech Republic
Type	Air force
Role	Aerial warfare
Size	53 fixed-wing aircraft 50 helicopters
Part of	Army of the Czech Republic
Headquarters	Prague
Motto(s)	Vzduch je naše moře (The air is our sea)
Commanders
Air Force Commander	Brigade general Petr Hromek
Insignia
Roundel
Aircraft flown
Attack	Mi-24, L-159A
Fighter	JAS 39 Gripen
Helicopter	Mi-8, Mi-17, W-3A
Trainer	L-39ZA, L-159T1
Transport	CASA C-295M, Bombardier Challenger CL-601, Airbus A319, Let L-410, Yak-40