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词条 Kamov Ka-118
释义

  1. Design and development

  2. Specifications (as designed)

  3. References

  4. External links

{{update|date=November 2010}}
name= Kamov Ka-118caption=

}}{{Infobox Aircraft Type

type= light multirole helicopter with NOTARmanufacturer= Kamovfirst flight=introduction=retired=status= Design in researchmore users=produced =number built=unit cost=developed from=variants with their own articles =
}}

The Kamov Ka-118 is a projected light multirole helicopter with the NOTAR (NO TAil Rotor) configuration based on the McDonnell Douglas design.

Design and development

The first test of this concept took place on the Ka-26SS helicopter, a modified version of the Ka-26 equipped with experimental tail jet beams. The main concept of the Ka-118 features a single 4-blade main rotor, V-tail with upper tailplane, and a skid undercarriage. Pilot and copilot seated in side-by-side configuration, and four passengers in the rear cabin.

Since 1993, engine has not been selected and the NOTAR design is still in research.

Specifications (as designed)

{{aerospecs
|ref=
|met or eng?= met
|crew= One-two pilots
|capacity= 4-5 passengers, or up to 700 kg (1,540 lb) of cargo carried internally or externally.
|length m= 10.00
|length ft= 32
|length in= 10
|span m=
|span ft=
|span in=
|swept m=
|swept ft=
|swept in=
|rot number= 1
|rot dia m= 11.00
|rot dia ft= 36
|rot dia in= 1
|dia m=
|dia ft=
|dia in=
|width m=
|width ft=
|width in=
|height m= 2.60
|height ft= 8
|height in= 6
|wing area sqm=
|wing area sqft=
|swept area sqm=
|swept area sqft=
|rot area sqm= 95.0
|rot area sqft= 1,020
|volume m3=
|volume ft3=
|aspect ratio=
|empty weight kg=
|empty weight lb=
|gross weight kg= 2,150
|gross weight lb= 4,730
|lift kg=
|lift lb=
|eng1 number= 1
|eng1 type= Omsk TVO-100
|eng1 kw= 522
|eng1 hp= 700
|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=300
|max speed mph=190
|max speed mach=
|cruise speed kmh=
|cruise speed mph=
|range km=
|range miles=
|endurance h=
|endurance min=
|ceiling m=6,150
|ceiling ft=20,200
|glide ratio=
|climb rate ms=
|climb rate ftmin=
|sink rate ms=
|sink rate ftmin=
|armament1=
|armament2=
|armament3=
|armament4=
|armament5=
|armament6=
}}

References

Bill Gunston "The Osprey's Encyclopedia of Russian Aircraft", 2000

External links

{{commons category|Kamov}}
  • [https://web.archive.org/web/20080503101636/http://www.armscontrol.ru/atmtc/Arms_systems/Avia/Russia/Kamov_Design_bureau.htm www.armscontrol.ru]
{{Kamov aircraft}}

4 : Kamov aircraft|Soviet and Russian helicopters|Proposed aircraft of Russia|NOTAR helicopters

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