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                F-20 Tigershark   Click here to download the FSM model

Scale 1 : 10.5

Wing span 970mm

first photo of our new plug

 

Fully fiber glass, fuselage reinforced with already installed elevator mounts. One part fiberglass sandwich wing, elevators with already mounting rods designed for Taileron configuration. Our kit is designed for small gas turbines like the Lambert Kolibri Microturbine, the Wren MW44 Gold or 90mm EDF

Kit consists of fuselage with preinstalled elevator tubes, wing, a pair of elevators,fiber glass canopy frame and clear canopy.

To complete the Tigershark you only need to fit your electronics and engine and do the paint works.

 

 

 

   - Lenght 1370 mm
   -

Wing span 970 mm

   -

Kit weight 1.0 kgs

   -

Fuselage fiberglass with elevator tubes installed.

   -

Wings and elevators:

   fiber glass sandwich with built in wing connector tubes

 

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Price:  695 US $

 


 

we ship worldwide

ask for shipping cost

 

 

This kit is still in in development stage

and will be available soon.

Please check back often or

contact us for more details

 

Northrop F-20 Tigershark

- Background information on the original -


The Northrop F-20 Tigershark (initially F-5G) was a privately financed fighter aircraft, designed and built by Northrop in the USA, starting in 1975 and offered for sale starting in the 1980s and formally ending in the early 1990s.
It began as a further evolution of Northrop's F-5 Freedom Fighter/Tiger II, although ultimately it shared little more than a strong family resemblance to that aircraft. It was originally designated F-5G, which was approved by the USAF in May 1981. The initial request for F-20 was initially turned down in 1982, the USAF proposing F-19 which ended up not being used at all. The USAF gave approval for F-20 designation use in November 1982 and of the extra name Tigershark in March 1983.
The main change was the replacement of the F-5's two General Electric J85 engines with a single General Electric F404 turbofan, increasing its total thrust by 60%. Like the F-5, however, it was designed as a low-cost, high-performance fighter plane that was easy to maintain. It could reach speeds of Mach 2.1 and had a ferry range of 1,715 miles (2,760 km). The aircraft was armed with General Electric AN/APG-67 radar that offered significant performance improvement over the original Emerson AN/APQ-159 radar of the original F-5E/F.
An air-to-air left side view of a Northrop F-20 Tigershark aircraft dropping practice bombs during a
demonstration.The F-20 made its first flight on August 30, 1982, and a total of three prototypes were created. It was intended for sale to foreign countries and militaries, but the market for the plane never developed, as President Ronald Reagan relaxed the restrictions on selling fighters such as the F-16 Fighting Falcon to other countries. Also, in 1986, the United States government had not placed an order for the aircraft, but instead use the F-16 as the replacement aircraft for the continental U.S. air defense requirement, had a large effect on the decisions of other countries not to buy the F-20. The Pakistan Air Force was offered the F-20 and A-10 Thunderbolt II, but insisted on choosing the F-16 because it was felt that it would give them a technological advantage.
After six years and no major buyers, Northrop cancelled the $1.2 billion project. Some felt that the U.S. Air Force was biased against the aircraft due to its unconventional development which reflected poorly on the air force management style in procuring aircraft. Air forces that could afford the F-20 bought the F-16, while ones which could buy neither, purchased the cheaper F-5E/F Tiger II or the Russian MiG-21. While its performance was comparable to the Block 1/5/10 F-16 and superior to the turbojet-powered export-variant F-16/79, the F-20 airframe had virtually no remaining expansion capability, as it was built on essentially a 20 year old airframe at the limits of its capabilities. The F-20's low-set wing and wing-mounted undercarriage also limited the size and number (four underwing hardpoints on the F-20 vs. six on the F-16) of underwing stores that could be used; whereas the F-16 would often be seen with very large stores. The F-16 was a brand-new jet that had not even begun to approach its eventual capabilities. There was speculation within the F-20 development team that the US Air Force influenced foreign militaries to buy the F-16, in order to make spare parts more available.
The last existing F-20 is on display at the California Science Center. The other two prototypes were lost due to crashes during world sales tours. The crashes were caused by pilot error, and were not linked to any malfunction of the planes.
Aerospace legend Chuck Yeager, who worked as a spokesperson for Northrop during the F-20's development, frequently touted the plane and was regularly featured in its advertising.



 

DIMENSIONS

- Length 54.75 ft (14.42 m)
- Wingspan 21.92 ft (8.13 m)
- Height 13.50 ft (4.20 m)
 

- Empty weight 5965 kg
- Max Takeoff weight 12,700 kg
- Max Payload 3,650 kg
- General Electric F404-GE-100

  Thrust    81KN

 

PERFORMANCE

    - Max Level Speed at altitude: 1,450 mph (2,334 km/h) at 42,650 ft (13,000 m), Mach 2.2
    - Initial Climb Rate 50,000 ft (15,239 m) / min
    - Service Ceiling 57,000 ft (17,315 m)
    - Range ferry: 1,800 nm (3,000 km)

 

ARMAMENT

    - Two M39 20-mm cannons
  
   




 

 

 

 

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