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【已售完】Northrop F-5E Tiger II 5342,30012,台湾空军【2011年12月到货】
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【已售完】Northrop F-5E Tiger II 5342,30012,台湾空军【2011年12月到货】

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模型名称:Northrop F-5E Tiger II 5342,30012,台湾空军      Northrop F-5E Tiger II 5342, 30012, ROCAF

合金,P.V.C

规格:1/72

模型历史背景:

F-5E/F“虎”II式战斗机在20世纪70年代成为美国对其第三世界盟国进行军火倾销的主力机种,由于该机经历过实战考验并承袭有前一代F-5A/B“自由战士”战斗机维护方便等特点,使其在问世后的10年内,被销售至全球21个国家和地区。并因此在国际军火交易中形成法国“幻影”III、前苏联MiG-21以及F-5E/F三种机型鼎立的局面。

 

 

General Background
The Northrop F-5 tactical fighter was designed as an extremely maneuverable, supersonic fighter with a high rate of reliability at a low operating cost. The F-5 first flew on July 30, 1959 with the first customer delivery in 1964. The last of more than 2,600 F-5’s was produced in 1989 and about two-thirds of these are still in service with 26 countries more than 4 decades later. The F-5 was manufactured by Northrop Grumman and under license in Canada, Taiwan, South Korea, Spain and Switzerland.
The Aircraft
In 1982 the 44th, 45th and 46th FS formed the 7th FG of the 737th FW. In 1984 the wing converted from the F-5A/B to the F-5E/F and the 46th became a independent TFS reporting directly to the 737th TFW and tasked as an Aggressor Squadron. The 46th TFS F-5Es were painted with large red buzz numbers on the nose and the stenciled "Chung Chen" on the side of the fuselage. In 1988 ROCAF installed its Tactical Aircrew Combat Training System/Air Combat Maneuvering Instrumentation (TACTS/ACMI) training range at Taitung AFB with the 46th TFS as its sole unit. ROCAF Northrop F-5E buzz number 5342 was built as c/n VG.1069 serial number 83-00112 Module C.
Specifications :
Crew: 1
Dimensions  
Length: 47 ft 4.75 in (14.45 m)
Wingspan: 26 ft 8 in (8.13 m)
Height: 13 ft 4.5 in (4.08 m)
Powerplant: 2 X General Electric J85-GE-21B turbojet
Dry thrust: 3,500 lbf (15.5 kN) per engine
Thrust with afterburner: 5,000 lbf (22.2 kN) per engine
Internal fuel : 677 US gal (2,563 L)
External fuel: 275 US gal (1,040 L) per tank in up to 3 tanks
Weight  
Empty weight: 9,558 lb (4,349 kg)
Loaded weight: 15,745 lb (7,157 kg)
Max takeoff weight: 20,486 lb (9,312 kg)
Performance  
Maximum speed: 917 kn (1,060 mph, 1,700 km/h, Mach 1.6)
Range: 760 nmi (870 mi, 1,405 km)
Ferry range: 2,010 nmi (2,310 mi, 3,700 km)
Service ceiling: 51,800 ft (15,800 m)
Rate of climb: 34,400 ft/min (175 m/s)
Armament  
Guns: 2 X 20 mm (0.787 in) Pontiac M39A2 Revolver cannons in the nose, 280 rounds/gun
Hardpoints: 7 total (3 X wet): 2 X wing-tip AAM launch rails, 4 X under-wing and 1 X under-fuselage pylon stations holding up to 7,000 pounds (3,200 kg) of payload.
Rockets: 2 X LAU-61/LAU-68 rocket pods (each with 19 X / 7 X Hydra 70 mm rockets, respectively) or
  2 X LAU-5003 rocket pods (each with 19 X CRV7 70 mm rockets) or
  2 X LAU-10 rocket pods (each with 4 X Zuni 127 mm rockets) or
  2 X Matra rocket pods (each with 18 X SNEB 68 mm rockets)
Missiles  
Air-to-air missile: 4 X AIM-9 Sidewinders or 4 X AIM-120 AMRAAMs
Air-to-surface missile: 2 X AGM-65 Mavericks
Bombs: A variety of air-to-ground ordnance such as the Mark 80 series of unguided iron bombs (including 3 kg and 14 kg practice bombs), CBU-24/49/52/58 cluster bomb munitions, napalm bomb canisters and M129 Leaflet bomb and laser guided bombs of Paveway family.
Others: up to 3 X 150/275 US gallon Sargent Fletcher drop tanks for ferry flight or extended range/loitering time.
Avionics: Emerson Electric AN/APQ-153 radar on early batch of F-5E
  Emerson Electric AN/APQ-159 radar on later production F-5E

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