- Development
- Specifications
- See also
- References Notes Bibliography
- External links
| name=T-411 Aist | image=T-411 at Oshkosh.jpg | caption= }}{{Infobox Aircraft Type | type=Light utility monoplane | national origin=Russia | manufacturer=Krunichev OKB | designer= | first flight=10 November 1993 | introduced= | retired= | status= | primary user= | number built= | developed from= | variants with their own articles=Washington T-411 Wolverine
}} |
The Krunichev T-411 Aist (en: Stork) is a Russian light utility monoplane designed by the Russian company Aeroprogress and placed into production by the Khrunichev State Research and Production Space Center.[1][2] A version is marketed in the United States as the Aeroprogress T-411 Wolverine powered by a Continental TSIO-550-B. A homebuilt derivative design is the Washington T-411 Wolverine.[2] DevelopmentThe ROKS-Aero corporation was set up in Moscow in 1990 to design and manufacture general aviation aircraft, but was renamed Aeroprogress in 1993.[3] In 1992 ROKS-Aero started design of a single-engined light aircraft, the T-411 Aist 2. Construction of the prototype T-411 started in April 1993, making its maiden flight on 10 November 1993.[4] Specifications{{Aircraft specs
|ref=Jane's All The World's Aircraft 2003–2004[5]
|prime units?=met
|genhide=
|crew=2
|capacity=3 passengers or 361 kg (795 lb)
|payload=
|length m=9.45
|length ft=
|length in=
|length note=
|span m=13.02
|span ft=
|span in=
|span note=
|height m=2.60
|height ft=
|height in=
|height note=
|wing area sqm=24.30
|wing area sqft=
|wing area note=
|aspect ratio=7.0:1
|airfoil=NACA 23011
|empty weight kg=544
|empty weight lb=
|empty weight note=
|gross weight kg=
|gross weight lb=
|gross weight note=
|max takeoff weight kg=1650
|max takeoff weight lb=
|max takeoff weight note=
|more general=
|eng1 number=1
|eng1 name=VOKBM M14X
|eng1 type=9-cylinder air-cooled radial engine
|eng1 kw=268
|eng1 hp=
|eng1 kn=
|eng1 lbf=
|eng1 note=
|power original=
|thrust original=
|prop blade number=3
|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=204
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|stall speed kmh=93
|stall speed mph=
|stall speed kts=
|stall speed note=(flaps down)
|never exceed speed kmh=
|never exceed speed mph=
|never exceed speed kts=
|never exceed speed note=
|range km=1200
|range miles=
|range nmi=
|range note=
|endurance=
|ceiling m=3000
|ceiling ft=
|ceiling note=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|lift to drag=
|more performance=
|avionics=
}}
See also{{aircontent
|see also=
|related=
|similar aircraft=
|sequence=
|lists=- List of seaplanes and amphibious aircraft
}}ReferencesNotes1. ^1 Jackson 2003, p. 381.
2. ^Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 294. BAI Communications, 15 July 1998. {{ISBN|0-9636409-4-1}}
3. ^Gunston 1995, p. 316.
4. ^Jackson 2003, p. 381.
5. ^Jackson 2003, pp. 381–382.
6. ^1 2 {{cite journal |last= |first= | title = World Directory of Leisure Aviation 2004/2005 |publisher = Pagefast Ltd, England | year = 2004 | issn = 1368-485X}}
[6]
}}Bibliography{{refbegin}}- {{cite book|last=Gunston|first=Bill|title=The Osprey Encyclopedia of Russian Aircraft 1875-1995|publisher=Osprey|location=London|date=1995|isbn=1-85532-405-9}}
- {{cite book |last=Jackson |first=Paul |title=Jane's All The World's Aircraft 2003–2004 |year=2003 |publisher= Jane's Information Group|location=Coulsdon, UK |isbn=0-7106-2537-5 }}
- {{cite book |last=Taylor |first= Michael J. H.|authorlink= |coauthors= |title= Brassey's World Aircraft & Systems Directory|year=1996 |publisher= Brassey's|location= London, England |isbn=1-85753-198-1|pages=}}
{{refend}}External links{{commons category|T-101 Grach}}{{Aeroprogress aircraft}} 6 : Khrunichev aircraft|Soviet and Russian civil utility aircraft 1990–1999|High-wing aircraft|Single-engined tractor aircraft|Floatplanes|Aircraft first flown in 1993 |