Fournier RF 5
{{Short description|German touring motor glider, 1968}}
{{Infobox Aircraft Begin
| name=RF 5 | image=Fournier RF 5 (D-KBAN) 03.jpg | caption= }}{{Infobox Aircraft Type | type=Motorglider | national origin=France | manufacturer= | designer= {{ill|René Fournier (aircraft designer)|lt=René Fournier|fr|René Fournier}} | first flight= January 1968 | introduced= | retired= | status= | primary user= | number built= | developed from= | variants with their own articles= }} |
The Fournier RF 5 is a two-seat motor glider designed by {{ill|René Fournier (aircraft designer)|lt=René Fournier|fr|René Fournier}} .{{cite web|title=RF 5|url=http://www.sailplanedirectory.com/PlaneDetails.cfm?planeID=457|website=sailplanedirectory.com|accessdate=18 January 2015|url-status=dead|archiveurl=https://web.archive.org/web/20151112232928/http://www.sailplanedirectory.com/PlaneDetails.cfm?PlaneID=457|archivedate=12 November 2015}}{{cite web|title=Fournier aircraft history, performance and specifications|url=http://www.pilotfriend.com/aircraft%20performance/fournier/fournier.htm |website=pilotfriend.com|accessdate=18 January 2015}}
Design and development
The RF 5 is based on the single seater Fournier RF 4, and is a low-winged monoplane of all-wooden construction, with the crew of two sat in a tandem enclosed cockpit. It is semi-aerobatic with loops, stall turns, lazy eights, chandelles and spins approved.{{cite journal|journal=Flight International|date=11 June 1970|pages=974–977|url=http://www.flightglobal.com/pdfarchive/view/1970/1970%20-%201062.html|title=GROWN-UP ULTRA-LIGHT |accessdate=18 January 2015}}{{cite web | title=RF 5 Flight Manual |url=http://www.club-fournier.de/dev/wp-content/uploads/2012/09/RF5-POM-5111.pdf |accessdate=23 November 2017}} It has a manually retractable center landing gear, a steerable tailwheel and detachable outrigger landing gear. Spoilers are available to reduce lift. The wingtips of the parked aircraft can be unlocked and folded inwards by a single person to reduce required hangar space.
Variants
;RF 5B
:An improved high-performance version. Powered by a 50.7 kW (68 hp) Limbach SL 1700 E Comet engine.{{cite book|last1=Taylor|first1=Michael J H.|title=Jane's Encyclopedia of Aviation|date=1989|page=838|location=London|publisher=Portland House|isbn=0-517-69186-8}} One prototype build by Alpavia.
;RF 5B Sperber
:A high performance powered sailplane with {{convert|17.5|m|ft|abbr=on}} span wings. Build by Sportavia-Putzer Gmbh. U Co. Kg.
;AeroJaén RF5-AJ1 Serrania
:License built version produced by Aeronáutica del Jaén SA
;TZ-3
:Brazilian Air Force designation of the RF 5.{{Cite web |title=Brazilian Military Aircraft Designations |url=https://designation-systems.net/non-us/brazil.html |access-date=2025-03-17 |website=designation-systems.net}}
Specifications (RF 5)
File:Fournier RF5, Private JP7384079.jpg
{{Aircraft specs
|ref=Jane's All the World's Aircraft 1988-89,{{cite book |title=Jane's All the World's Aircraft 1988-89 |year=1988 |publisher=Jane's Information Group |location=London |isbn=0-7106-0867-5 |editor=John W.R. Taylor}} Jane's All The World's Aircraft 1976–77{{cite book |title=Jane's All the World's Aircraft 1976-77 |year=1976 |publisher=Jane's yearbooks |location=London |isbn=0-354-00538-3 |editor=John W.R. Taylor|pages=570–571}}
|prime units?=met
|crew=2
|length m=7.8
|span m=13.74
|height m=1.96
|wing area sqm=15.12
|width m=8.6
|width note=wings folded
|aspect ratio=12.5
|airfoil=root:NACA 23015, tip:NACA 23012
|empty weight kg=420
|max takeoff weight kg=650
|fuel capacity={{convert|60|L|USgal impgal|abbr=on|1}}
|more general=
|eng1 number=1
|eng1 name= Limbach L2000 EOI
|eng1 type=4-cyl. horizontally-opposed air-cooled piston engine
|eng1 hp=80
|prop blade number=2
|prop name=Hoffman HO-V-62-R/160 fixed pitch propeller
|prop dia m=
|prop dia ft=
|prop dia in=
|prop dia note=
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=113
|cruise speed note=
|stall speed kmh=
|stall speed mph=
|stall speed kts=43
|stall speed note=clean
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=135
|never exceed speed note=at max t/o weight
|range km=700
|range miles=
|range nmi=
|range note= to {{convert|900|km|nmi mi|abbr=on}}
|combat range km=
|combat range miles=
|combat range nmi=
|combat range note=
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=5000
|g limits=+6 -3
|glide ratio=20
|climb rate ms=3.29
|climb rate note=max
|time to altitude=
|sink rate ms=1.4
|sink rate note=power off
|wing loading kg/m2=42.99
|wing loading note=at max t/o weight
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|thrust/weight=
|more performance=
|avionics=
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==See also==
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References
{{commons category|Fournier RF 5}}
{{reflist}}
{{Fournier aircraft}}
{{Sportavia-Pützer aircraft}}
{{FAB aircraft designations}}
Category:1960s French sailplanes