2022 AirDotShow Live Tour

Tour Destinations

Fort Lauderdale

April 30 – May 1, 2022

 
Space Coast

May 21-22, 2022

 
Ocean City

June 11-12, 2022

 
Newport

June 25-26, 2022

 
New York

September 10-11, 2022

 
Orlando

October 29-30, 2022

 
Atlanta

November 5-6, 2022

 

Giving Back

AirDotShow partners with the National Air, Sea and Space Foundation to give back through hosting STEM Education Programs to inspire the next generation to pursue careers in aerospace. AirDotShow also support the NASSF’s Cajun Scholarship founded to honor fallen Thunderbird pilot Stephen “Cajun” Del Bagno

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Fokker DR-1 (Replica)

The Fokker Dr.I (Dreidecker, “triplane” in German), often known simply as the Fokker Triplane, was a World War I fighter aircraft built by Fokker-Flugzeugwerke. The Dr.I saw widespread service in the spring of 1918. It became famous as the aircraft in which Manfred von Richthofen gained his last 19 victories, and in which he was killed on 21 April 1918.

In February 1917, the Sopwith Biplane began to appear over the Western Front. Despite its single Vickers machine gun armament, the Sopwith swiftly proved itself superior to the more heavily armed Albatros fighters then in use by the Luftstreitkräfte. In April 1917, Anthony Fokker viewed a captured Sopwith Biplane while visiting Jasta 11. Upon his return to the Schwerin factory, Fokker instructed Reinhold Platz to build a triplane, but gave him no further information about the Sopwith design. Platz responded with the V.4, a small, rotary-powered triplane with a steel tube fuselage and thick cantilever wings, first developed during Fokker’s government-mandated collaboration with Hugo Junkers.

Initial tests revealed that the V.4 had unacceptably high control forces resulting from the use of unbalanced ailerons and elevators. Instead of submitting the V.4 for a type test, Fokker produced a revised prototype designated V.5. The most notable changes were the introduction of horn-balanced ailerons and elevators, as well as longer-span wings. The V.5 also featured interplane struts, which were not necessary from a structural standpoint, but which minimized wing flexing. On 14 July 1917, Idflieg issued an order for 20 pre-production aircraft. The V.5 prototype, serial 101/17, was tested to destruction at Adlershof on 11 August 1917.

specifications:

DIMENSIONS AND CAPACITY

CREW: 1

Length: 5.77 m (18 ft 11 in)
Upper wingspan: 7.19 m (23 ft 7 in)
Height: 2.95 m (9 ft 8 in)
Wing area: 18.7 m2 (201 sq ft)
Aspect ratio: 4.04
Empty weight: 406 kg (895 lb)
Gross weight: 586 kg (1,291 lb)
Powerplant: 1 × Oberursel Ur.II 9-cylinder air-cooled rotary piston engine, 82 kW (110 hp)
Propellers: 1 – 2-bladed fixed-pitch wooden propeller

PERFORMANCE

SPEED: 160 km/h (99 mph, 86 kn) at 2600m

SERVICE CEILING: 6,100 m (20,000 ft)

RANGE: 300 km (190 mi, 160 nmi)

Armament:

  • Guns: 2 × 7.92 mm (0.312 in) Maschinengewehr 08 “Spandau” machine guns