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词条 Nikitin MU-4
释义

  1. Development

  2. Specifications (MU-4)

  3. See also

  4. References

  5. External links

name=MU-4 image= caption=

}}{{Infobox Aircraft Type

type=Amphibian trainer aircraft national origin=USSR manufacturer= designer= Vasilii Vasilyevich Nikitin & N.G. Mikhelson first flight= 1936 introduced= retired= status= primary user= number built=1 developed from= variants with their own articles=
}}

The Nikitin MU-4 was an amphibian trainer aircraft produced in the USSR in 1936.

Development

The flying boat style MU-4 training amphibian was a single-engined side-by-side two-seat biplane. The single engine was supported in front of the upper mainplane by a short nacelle and the cabane struts of the wing. The upper wing was supported on dural interplane and cabane struts which were braced with flying and landing wires. Built predominantly of wood the wings and strut braced tail surfaces were part plywood and part fabric covered, whilst the fuselage was built up from wooden frames and plywood skinning. The manually retractable Ski/wheel undercarriage was attached either side of the fuselage forward of the wings. Flight testing was carried out successfully, demonstrating good flying qualities and adequate performance, however after prolonged testing the aircraft crashed due to a glue failure

Specifications (MU-4)

{{aerospecs
|ref=Gunston, Bill. "Encyclopedia of Russian Aircraft 1875-1995". London:Osprey. 1995. {{ISBN|1-85532-405-9}}
|met or eng?=met
|crew=2
|capacity=
|length m=
|length ft=
|length in=
|span m=12
|span ft=39
|span in=4-1/2
|swept m=
|swept ft=
|swept in=
|rot number=
|rot dia m=
|rot dia ft=
|rot dia in=
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m=
|height ft=
|height in=
|wing area sqm=33
|wing area sqft=355
|swept area sqm=
|swept area sqft=
|rot area sqm=
|rot area sqft=
|volume m3=
|volume ft3=
|aspect ratio=
|wing profile=
|empty weight kg=900
|empty weight lb=1,984
|gross weight kg=1,200
|gross weight lb=2,646
|lift kg=
|lift lb=
|eng1 number=1
|eng1 type=MG-11F
|eng1 kw=134.23
|eng1 hp=180
|eng1 kn=
|eng1 lbf=
|eng1 kn-ab=
|eng1 lbf-ab=
|eng2 number=
|eng2 type=
|eng2 kw=
|eng2 hp=
|eng2 kn=
|eng2 lbf=
|eng2 kn-ab=
|eng2 lbf-ab=
|max speed kmh=168
|max speed mph=104
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|stall speed kmh=
|stall speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=
|ceiling ft=
|g limits=
|roll rate=
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}

See also

{{aircontent
|see also=
|related=
|similar aircraft=
  • F.B.A. 271
  • Lioré et Olivier LeO H-221

|lists=
  • List of aircraft

}}

References

{{refbegin}}
  • Gunston, Bill. "Encyclopedia of Russian Aircraft 1875-1995". London:Osprey. 1995. {{ISBN|1-85532-405-9}}
{{refend}}

External links

  • https://web.archive.org/web/19991004085143/http://www.aviation.ru/Nikitin/
{{Nikitin aircraft}}

7 : Soviet military trainer aircraft 1930–1939|Nikitin aircraft|Flying boats|Amphibious aircraft|Sesquiplanes|Single-engined tractor aircraft|Aircraft first flown in 1936

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