Vought-Sikorsky VS-300: Difference between revisions
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|manufacturer=Vought-Sikorsky |
|manufacturer=Vought-Sikorsky |
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|designer=Igor Sikorsky |
|designer=Igor Sikorsky |
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|first flight=14 September 1939 <ref>First takeoff and landing on the same helipad. - ''US Warbirds''. 1985 </ref> |
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|first flight=13 May 1940 |
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|introduced= |
|introduced= |
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|retired= |
|retired= |
Revision as of 10:13, 2 April 2010
VS-300 | |
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File:Sikorsky vs-300.jpg | |
Igor Sikorsky in the VS-300, at the end of 1941 | |
Role | Experimental |
Manufacturer | Vought-Sikorsky |
Designer | Igor Sikorsky |
First flight | 14 September 1939 [1] |
Variants | Sikorsky R-4 |
The Vought-Sikorsky VS-300 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 flight of the VS-300 was on 13 May 1940,[2] powered by a larger, 90 horsepower (67 kW) engine. While not the first successful helicopter to fly, it was the first successful helicopter in the United States and the first successful helicopter to use a single vertical tail rotor configuration for antitorque.
Development
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.[3] On 6 May 1941, the VS-300 beat the world endurance record held by the Fw 61 by staying aloft for 1 hour 32 minutes and 26.1 seconds.[2]
Specifications (VS-300)
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Data from {name of first source}
General characteristics
Performance
See also
Related development
References
- Notes
- Bibliography
- Munson, Kenneth. Helicopters and Other Rotorcraft Since 1907. London: Blandford, 1968. ISBN 0-7137-06104.