Ryan XV-8
{{Short description|American experimental STOL aircraft}}
{{about|the US utility aircraft developed in the 1960's|the ground attack VTOL aircraft|AV-8 Harrier}}
{{Infobox aircraft
|name= XV-8 "Fleep"
|image= File:XV-8A_Fleep_Prototype_-_GPN-2000-001271.jpg
|caption= XV-8 "Fleep" tested in the Full Scale Tunnel at Langley, 1962
|type= Experimental STOL aerial utility vehicle
|manufacturer= Ryan Aeronautical Company
|designer=
|first_flight= 1961
|introduction=
|retired=
|status=
|primary_user=
|more_users=
|produced=
|number_built= 1
|variants=
}}
The Ryan XV-8 Flexible Wing Aerial Utility Vehicle (nicknamed Fleep, short for "Flying Jeep") was an improved version of the Flex-Wing. Both aircraft were built by Ryan Aeronautical Company in collaboration with NASA for the United States Air Force and the United States Army and tested in 1961 as a STOL patrol, reconnaissance, and light utility aircraft to transport people or freight when a more specialized aircraft is not required or available.
Design and development
The Fleep began as the Flex-Wing. The Flex-Wing had four-wheel landing gear, a smaller nose section behind which the pilot sat, and a single vertical tail/rudder.
The Fleep had tricycle landing gear, a larger nose section and a V tail/rudder. The wing was a fabric delta-shaped Rogallo wing with a foldable frame; the wing was attached to a pod-like cockpit on a four-wheeled cargo platform. It was tested with two tail configurations — vertical fin and V-tail. The aircraft wing could be folded into a relatively small package for transport.[http://www.globalsecurity.org/military/systems/aircraft/xv-8.htm Folding frame for transport][http://www.aerofiles.com/_ryan.html Specifications]{{usurped|1=[https://web.archive.org/web/20070817182221/http://www.strange-mecha.com/aircraft/VTOL/USAR-VTOL.htm Specifications]}}[http://apps.dtic.mil/dtic/tr/fulltext/u2/b253477.pdf DCIT performance report, 1964][https://web.archive.org/web/20160303211458/http://www.dtic.mil/dtic/tr/fulltext/u2/460405.pdf January 1965 performance report]
Specifications
{{Unreferenced section|date=June 2022}}{{Aircraft specs
|prime units? = imp
|crew=One pilot
|length m=5.94
|length ft=10
|length in=6
|span m=10.18
|span ft=33
|span in=5
|eng1 number=1
|eng1 name=Continental IO-360-A
|eng1 kw=157
|eng1 hp=210
|max speed kmh=105
|max speed mph=65
|range km=193
|range miles=120
}}
See also
{{aircontent
|related=
|similar aircraft=
|lists=
|see also=
- Francis Rogallo's airfoil
- John W. Dickenson
- History of hang gliding
- Ultralight trike aircraft
}}
References
{{reflist}}
- [http://www.flightglobal.com/pdfarchive/view/1963/1963%20-%201346.html FLEXIBLE WINGS AT WORK]
External links
{{Commons category|Ryan XV-8}}
- [https://books.google.com/books?id=KtwDAAAAMBAJ&pg=PA85 Popular Mechanics article by Ryan test pilot Lou Everett]
{{Ryan aircraft}}
{{US STOL and VTOL aircraft}}
Category:Tailless delta-wing aircraft