Aviation 72 – Saab J35 Draken , ‚DK-202‘ Finnish Air Force (FAF/FiAF)
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-sběratelský model letadla Saab 35 Draken 1/72 -provedení: kovový model s plastovými částmi -model je v kvalitním provedení -součástí balení je stojánek
Saab 35 Draken
Saab 35 Draken byl stíhací letoun vyráběný mezi roky 1955 a 1974 švédskou firmou Saab. Draken byl původně navržen, aby nahradil starší letouny Saab J 29 Tunnan a později i stíhací verzi (J 32B) letounu Saab 32 Lansen. Bylo u něho představeno inovativní dvojité delta křídlo. Za účelem otestování tohoto dosud neprobádaného aerodynamického prvku bylo vyrobeno a zalétáno menší experimentální letadlo, Saab 210.
The Saab 35 Draken (‚The Kite or The Dragon‘) is a Swedish fighter aircraft developed and manufactured by Saab between 1955 and 1974. It was the first fully supersonic aircraft to be deployed in Western Europe and the first aircraft to do the Cobra maneuver.
| Role | Fighter aircraft |
|---|---|
| National origin | Sweden |
| Manufacturer | Saab |
| Designer | Erik Bratt |
| First flight | 25 October 1955 |
| Introduction | 8 March 1960 |
| Retired | 2005 (Austria) |
| Status | Retired from military service |
| Primary users | Swedish Air Force Austrian Air Force Finnish Air Force Royal Danish Air Force |
| Produced | 1955–1974 |
| Number built | 651 |
| Variants | Saab 210 |
General characteristics
- Crew: 1
- Length: 15.35 m (50 ft 4 in)
- Wingspan: 9.42 m (30 ft 11 in)
- Height: 3.89 m (12 ft 9 in)
- Wing area: 49.2 m2 (530 sq ft)
- Airfoil: 5%
- Empty weight: 7,865 kg (17,339 lb)
- Gross weight: 11,000 kg (24,251 lb)
- Max takeoff weight: 11,914 kg (26,266 lb)
- Powerplant: 1 × Svenska Flygmotor RM6C afterburning turbojet engine, 56.5 kN (12,700 lbf) thrust dry, 78.4 kN (17,600 lbf) with afterburner
Performance
- Maximum speed: 2,450 km/h (1,520 mph, 1,320 kn) at 11,000 m (36,089 ft)
- Maximum speed: Mach 2
- Ferry range: 2,750 km (1,710 mi, 1,480 nmi) with external drop tanks
- Service ceiling: 20,000 m (66,000 ft)
- Rate of climb: 199 m/s (39,200 ft/min)
- Wing loading: 231.6 kg/m2 (47.4 lb/sq ft)
- Thrust/weight: 0.7
- Takeoff roll: 800 m (2,625 ft)
Armament
- Guns: 1× or 2× 30 mm AKAN M/55 ADEN cannon with 100 rounds per gun (in Saab 35F one cannon was omitted to fit avionics needed for Falcon missile integration, earlier variants and export variants retained twin guns.)
- Hardpoints: for fuel tanks or ordnance with a capacity of 2,900 kg (6,393 lb),with provisions to carry combinations of:
- Rockets: 2× 75 mm air-to-ground rocket pods ventrally or 12× 135 mm rockets on six underwing pylon
- Missiles: Rb 24, Rb 27 and Rb 28 air-to-air missile
- Bombs: The Danish export version, (F-35), was modified according to NATO standards and was fitted with 1,000lb bomb hardpoints.
