- Design and development
- Specifications
- References Notes Bibliography
name=VoWi 10 | image= | caption= }}{{Infobox Aircraft Type | type=Two-seat ultralight aircraft | national origin=Germany | manufacturer=Airconcept Fleugzeug und Gerätebau GmbH | designer=Helmut Wilden | first flight=16 April 1975 | introduced= | retired= | status= | primary user= | number built= | developed from= | variants with their own articles= }} |
The Airconcept VoWi-10 is a German two-seat ultralight monoplane designed by Helmut Wilden. Design and developmentThe single-seat prototype high-wing braced monoplane was built by Wilden and first flew 16 April 1975. Due to the interest raised by the prototype Wilden set about re-designing the type as a two-seater that would be capable of series production or in kit form for homebuilders. A new company Airconcept Fleugzeug und Gerätebau GmbH was formed to produce and market the type. The prototype production two-seater first flew in 1978. Specifications{{Aircraft specs |ref=Illustrated Encyclopedia of Aircraft |prime units?=met |genhide= |crew=2 |capacity= |length m=5.89 |length ft= |length in= |length note= |span m=11.00 |span ft= |span in= |span note= |height m= |height ft= |height in= |height note= |wing area sqm=13.00 |wing area sqft= |wing area note= |empty weight kg=265 |empty weight lb= |empty weight note= |gross weight kg= |gross weight lb= |gross weight note= |max takeoff weight kg=430 |max takeoff weight lb= |max takeoff weight note= |more general=
|eng1 number=1 |eng1 name=Limbach SL1700 |eng1 type=flat-four piston engine |eng1 kw= |eng1 hp=60 |prop blade number= |prop name= |prop dia m= |prop dia ft= |prop dia in= |prop note=
|perfhide= |max speed kmh= |max speed mph= |max speed kts= |max speed note= |max speed mach= |cruise speed kmh=110 |cruise speed mph= |cruise speed kts= |cruise 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=2 hours (with 15 min reserves) |ceiling m= |ceiling ft= |ceiling note= |g limits= |roll rate= |glide ratio= |climb rate ms= |climb rate ftmin= |climb rate note= |sink rate ms= |sink rate ftmin= |sink rate note= |lift to drag= |wing loading kg/m2 |wing loading lb/sqft= |wing loading note= |power/mass met= |power/mass imp= |power/mass note= |thrust/weight= |thrust/weight note= |more performance= }}{{aircontent |see also= |related= |similar aircraft= |lists= }}
Referenceshttp://www.airconcept-enterprises.com/ NotesBibliography{{refbegin}}- {{cite book |last= |first= |authorlink= |coauthors= |title= The Illustrated Encyclopedia of Aircraft (Part Work 1982-1985)|year= |publisher= Orbis Publishing|location= |issn=|pages=}}
{{refend}}{{Aero-1970s-stub}} 4 : German civil utility aircraft 1970–1979|German ultralight aircraft 1970–1979|High-wing aircraft|Aircraft first flown in 1975 |