- Design
- Design and development
- Specifications (Antoinette V)
- See also
- Notes
- References
- Further reading
- External links
name=Antoinette V | image=Antoinette V.jpg | caption=The Antoinette V recognisable by the revised undercarriage }}{{Infobox Aircraft Type | type=Pioneer aircraft | national origin=France | manufacturer=Antoinette | designer=Léon Levavasseur | first flight=20 December 1908[1] | introduced= | retired= | status= | primary user= | more users= | produced= | number built=1 | program cost= | unit cost= | developed from= Antoinette IV | variants with their own articles=Antoinette VI }} |
The Antoinette V was an early French aircraft, first flown on 20 December 1908. DesignFollowing closely to the winning formula that Levavasseur had introduced, the Antoinette V introduced a revised undercarriage, with a closely spaced pair of mainwheels at the rear of a carriage/skid which extended forward of the propeller, a tail-skid attached to the lower fin framework prevented damage to the tail section. Lateral stability on the ground was provided by outrigger wheels supported by a wire-braced framework at about half-span. Design and developmentA development of the Antoinette IV, the Antoinette V differed somewhat in having increased upper vertical tail area with no fabric covering the lower fin framework. The fuselage consisted of a wooden framework of triangular section covered with fabric, except in the cockpit area abreast the wing trailing edge. The wings were built in a similar fashion and were also covered in fabric. Control was affected by wheels either side of the pilot's seat for roll and pitch, and a rudder bar for yaw. The pilot operated a triangular elevator hinged to the tailing edge of the large tailplane, rhomboidal ailerons hinged from the trailing edges of the wingtips, and two triangular rudders above and below the tailplane. Delivered to Réné Demanest, the Antoinette V proved easy to fly and enjoyed some success.[1] Specifications (Antoinette V) {{Aircraft specs |ref=[1] |prime units?=met |genhide= |crew=1 |capacity= |length m=11.5 |length ft= |length in= |length note= |span m=12.8 |span ft= |span in= |span note= |upper span m= |upper span ft= |upper span in= |upper span note= |mid span m= |mid span ft= |mid span in= |mid span note= |lower span m= |lower span ft= |lower span in= |lower span note= |swept m= |swept ft= |swept in= |swept note= |dia m= |dia ft= |dia in= |dia note= |width m= |width ft= |width in= |width note= |height m= |height ft= |height in= |height note= |wing area sqm=34 |wing area sqft= |wing area note= |swept area sqm= |swept area sqft= |swept area note= |volume m3= |volume ft3= |volume note= |aspect ratio= |airfoil= |empty weight kg= |empty weight lb= |empty weight note= |gross weight kg=520 |gross weight lb= |gross weight note= |max takeoff weight kg= |max takeoff weight lb= |max takeoff weight note= |fuel capacity= |lift kg= |lift lb= |lift note= |more general=
|eng1 number=1 |eng1 name=Antoinette 8V |eng1 type=V-8 water-cooled piston engine |eng1 kw= |eng1 hp=50 |eng1 kn= |eng1 lbf= |eng1 note= |power original= |thrust original= |eng1 kn-ab= |eng1 lbf-ab= |eng2 number= |eng2 name= |eng2 type= |eng2 kw= |eng2 hp= |eng2 kn= |eng2 lbf= |eng2 note= |eng2 kn-ab= |eng2 lbf-ab= |eng3 number= |eng3 name= |eng3 type= |eng3 kw= |eng3 hp= |eng3 kn= |eng3 lbf= |eng3 note= |eng3 kn-ab= |eng3 lbf-ab= |more power= |prop blade number=2 |prop name=Antoinette paddle-bladed |prop dia m=2.2 |prop dia ft= |prop dia in= |prop dia note= |rot number= |rot dia m= |rot dia ft= |rot dia in= |rot area sqm= |rot area sqft= |rot area note=
|perfhide= |max speed kmh=72 |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh= |cruise speed mph= |cruise speed kts= |cruise speed note= |stall speed kmh= |stall speed mph= |stall speed kts= |stall speed note= |never exceed speed kmh= |never exceed speed mph= |never exceed speed kts= |never exceed speed note= |minimum control speed kmh= |minimum control speed mph= |minimum control speed kts= |minimum control speed note= |range km= |range miles= |range nmi= |range note= |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= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |time to altitude= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |disk loading kg/m2= |disk loading lb/sqft= |disk loading note= |power/mass= |thrust/weight= |more performance=
|armament= |guns= |bombs= |rockets= |missiles= |hardpoints= |hardpoint capacity= |hardpoint rockets= |hardpoint missiles= |hardpoint bombs= |hardpoint other= |other armament= |avionics= }}
See also{{Portal|Aviation}}{{aircontent |see also= |related=- Antoinette III
- Antoinette IV
- Antoinette VI
- Antoinette VII
- Antoinette military monoplane
|similar aircraft= |lists= }}Notes1. ^1 2 {{harvnb|Jane|1909}}
References{{refbegin}}- {{cite book|last=Jane|first=Fred T.|title=Jane's all the World's Airships 1909|year=1909|publisher=Sampson, Low & Marston|location=London|isbn=0-7153-4649-0|ref=harv}}
{{refend}}Further reading- {{cite book |last= Taylor |first= Michael J. H. |title=Jane's Encyclopedia of Aviation |year=1989 |publisher=Studio Editions |location=London |pages=63 }}
- Munson, Kenneth. Pioneer Aircraft 1903-14
- World Aircraft Information Files. Brightstar Publishing: London. File 889 Sheet 63.
External links{{commons category|Antoinette aircraft}}- [https://web.archive.org/web/20070715125049/http://www.hubertlathamwindkiller.com/Monoplane.htm Hubert Latham: Windkiller]
- [https://web.archive.org/web/20080412070458/http://www.latham77.fsnet.co.uk/Hubert%20Latham.htm Hubert Latham]
{{Antoinette aircraft and aero engines}} 5 : French experimental aircraft 1900–1909|Antoinette aircraft|Single-engined tractor aircraft|High-wing aircraft|Aircraft first flown in 1908 |