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The Focke-Wulf Triebflügel (wing-driven) fighter was a German tail-sitter project during the Second World War. Three wings were mounted radially as a rotor on a rotating section of the fuselage and driven by small jet engines on the wingtips. The aircraft was to be propelled by this wing rotation. For takeoff and landing it would fly vertically as a helicopter, then tilt over horizontally to fly as a self-propelled wing generating both lift and thrust. The contemporary Heinkel Lerche project had an annular wing forming a duct around a conventional propeller, and in the transition from vertical to forward flight the lift would have transferred to the wing. 
The SNECMA Coléoptère was a postwar French development of the annular wing concept, but powered by a turbojet. It flew in both vertical and horizontal flight modes but never achieved the transition between the two.
Meanwhile, the USA was experimenting with propeller-driven design configurations with relatively conventional fixed wings. The Convair XFY Pogo had a delta wing with cruciform tail and successfully demonstrated the full transition between flight modes, while the Lockheed XFV Salmon had a straight wing with X tail but never achieved the flight transition.
A later jet-powered design, the Ryan X-13 Vertijet, first flew in 1955. Two prototypes were made, both flew, made successful transitions to and from horizontal flight, and landed. The final test flight was near Washington DC in 1957.
An inherent problem with all these tail-sitter designs was poor pilot visibility, especially of the ground, during vertical descent and landing. This led to the concept being abandoned once a more practical form of VTOL appeared, in the form of thrust vectoring.
A UAV does not suffer the problem of pilot attitude. The Dornier Aerodyne is of ducted-fan configuration similar to a coleopter, and a test UAV flew successfully in hover mode in 1972, before development was discontinued.
Studies and wind tunnel models were made of a tail-sitting version of the F-16 that would be ship based, but any further development was abandoned due to the large thrust requirement, and the need for extensive apparatus to handle take-off and landing.
List of tail-sitters
|Bachem Ba 349||Germany||1944||Interceptor||Prototype||Launched up a vertical tower, landed using parachutes.|
|Sukhoi Shkval||Soviet Union||1960||Interceptor||Development ceased,partial Mockup||equipped with a conventional Landing gear.side-by-side afterburner engines.|
|Convair XFY-1 Pogo||USA||1954||Fighter||Prototype|
|Focke-Wulf Triebflügel||Germany||1944||Interceptor||Project||Rotor wing around middle of fuselage. In-flight transition never resolved.|
|Rotary Rocket Roton ATV||USA||1999||Experimental||Prototype||Rotorcraft test vehicle for proposed SSO space launcher.|
|Ryan X-13 Vertijet||USA||1955||Experimental||Prototype|
|SNECMA Coléoptère||France||1959||Experimental||Prototype||Never achieved transition.|
|Tactically Exploited Reconnaissance Node||USA||2014||UAV||Project|
- "Nikola Tesla U.S. Patent 1,655,114 - Apparatus for Aerial Transportation". 2015-03-01. Retrieved 2016-08-07., Tesla Universe.
- Dan Sharp, Luftwaffe: Secret Weapons of the Third Reich, Mortons, 2015
- Darling, Jeff (2011-06-13). "Ryan X-13 Vertijet". Diseno. Archived from the original on 2014-01-28. Retrieved 2014-02-09.
- Newsom, William A.; Anglin, Ernie L. (September 1975). "FREE-FLIGHT MODEL INVESTIGATION OF A VERTICAL-ATTITUDE VTOL FIGHTER" (PDF). National Aeronautics and Space Administration. Retrieved October 16, 2016.
- Choi, Charles Q. (2010-01-19). "Electric Icarus: NASA Designs a One-Man Stealth Plane". Scientific American. Retrieved 2010-02-27.
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