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Vought Sikorsky VS 300

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Top speed
  
80 km/h

Length
  
8.53 m

First flight
  
May 13, 1940

Wingspan
  
9.14 m

Manufacturer
  
Sikorsky Aircraft

Designer
  
Vought-Sikorsky VS-300 VoughtSikorsky VS300 helicopter development history photos

Engine types
  
Reciprocating engine, Franklin 4 series

Vought sikorsky vs 300 1941


The Vought-Sikorsky VS-300 (or S-46) was a single-engine helicopter designed by Igor Sikorsky. It had a single three-blade rotor originally powered by a 75 horsepower (56 kW) engine. The first "free" flight of the VS-300 was on 13 May 1940. The VS-300 was the first successful single lifting rotor helicopter in the United States and the first successful helicopter to use a single vertical-plane tail rotor configuration for antitorque. With floats attached, it became the first practical amphibious helicopter.

Contents

Vought-Sikorsky VS-300 Sikorsky VS300 Aircraft

Design and development

Vought-Sikorsky VS-300 Sikorsky VS300 Helicopter

Igor Sikorsky's quest for a practical helicopter began in 1938, when as the Engineering Manager of the Vought-Sikorsky Division of United Aircraft Corporation, he was able to convince the directors of United Aircraft that his years of study and research into rotary-wing flight problems would lead to a breakthrough. His first experimental machine, the VS-300, was test flown by Sikorsky on 14 September 1939, tethered by cables. In developing the concept of rotary-wing flight, Sikorsky was the first to introduce a single engine to power both the main and tail rotor systems. The only previous successful attempt at a single-lift rotor helicopter, the Yuriev-Cheremukhin TsAGI-1EA in 1931 in the Soviet Union, used a pair of uprated, Russian-built Gnome Monosoupape rotary engines of 120 hp each for its power. For later flights of his VS-300, Sikorsky also added a vertical airfoil surface to the end of the tail to assist anti-torque but this was later removed when it proved to be ineffective.

Vought-Sikorsky VS-300 Untitled Document

The cyclic control was found to be difficult to perfect, and led to Sikorsky locking the cyclic and adding two smaller vertical-axis lifting rotors to either side aft of the tailboom. By varying pitch of these rotors simultaneously, fore and aft control was provided. Roll control was provided by differential pitching of the blades. In this configuration, it was found that the VS-300 could not fly forward easily and Sikorsky joked about turning the pilot's seat around.

Operational history

Vought-Sikorsky VS-300 httpsuploadwikimediaorgwikipediacommonsthu

Sikorsky fitted utility floats (also called pontoons) to the VS-300 and performed a water landing and takeoff on 17 April 1941, making it the first practical amphibious helicopter. On 6 May 1941, the VS-300 beat the world endurance record held by the Focke-Wulf Fw 61, by staying aloft for one hour 32 minutes and 26.1 seconds.

Vought-Sikorsky VS-300 VoughtSikorsky VS300 helicopter development history photos

The final variant of the VS-300 was powered by a 150 hp Franklin engine. The VS-300 was one of the first helicopters capable of carrying cargo. The VS-300 was modified over a two-year period, including removal of the two vertical tail rotors, until 1941 when a new cyclic control system gave it much improved flight behavior.

Survivor

Vought-Sikorsky VS-300 VoughtSikorsky VS300 Stingrays List of Rotorcraft

In 1943, the VS-300 was retired to the Henry Ford Museum in Dearborn, Michigan. It has been on display there ever since, except for a trip back to the Sikorsky Aircraft plant for restoration in 1985.

Specifications (VS-300)

Data from

General characteristics

  • Crew: one
  • Length: 28 ft 0 in (8.53 m)
  • Height: 10 ft 0 in (3.05 m)
  • Gross weight: 1,150 lb (522 kg)
  • Powerplant: 1 × Franklin 4AC-199-E , 90 hp (67 kW) at 2,500 rpm
  • Main rotor diameter: 30 ft 0 in (9.14 m)
  • Performance

  • Maximum speed: 50 mph (80 km/h; 43 kn)
  • Range: 75 mi (65 nmi; 121 km)
  • Endurance: 1 hour 30 minutes
  • References

    Vought-Sikorsky VS-300 Wikipedia