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=

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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:Fournier aircraft

Category:1960s French sailplanes

Category:Motor gliders

Category:Low-wing aircraft

Category:Single-engined tractor aircraft

Category:Aircraft first flown in 1968