Kamov Ka-118

{{update|date=November 2010}}

__NOTOC__

{{Infobox Aircraft Begin

|name= Kamov Ka-118

|image = Ка-118.svg

|caption=

}}{{Infobox Aircraft Type

|type= light multirole helicopter with NOTAR

|manufacturer= Kamov

|first flight=

|introduction=

|retired=

|status= Design in research

|more 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)

{{Aircraft specs

|ref=Jane's All the World's Aircraft 1992–93{{harvnb|Lambert|1992|pp=213–214}}

|prime units? = met

|crew= One-

|capacity= 4 passengers, or {{convert|1000|kg|lb|abbr=on}} of cargo carried externally

|length m= 10.00

|height m=2.60

|rot number= 1

|rot dia m= 11.00

|rot area sqm= 95.03

|rot area sqft=

|gross weight kg= 1950

|max takeoff weight kg= 2250

|max takeoff weight note=(external load)

|fuel capacity={{convert|700|L|impgal USgal|abbr=on}}

|eng1 number= 1

|eng1 name= Omsk TVO-100

|eng1 type=turboshaft

|eng1 kw= 530

|eng1 hp=

|max speed kmh=300

|max speed mph=

|cruise speed kmh=270

|climb rate ms=11

|ceiling m=6150

|ceiling ft=

|range km=950

|range note=with normal fuel

}}

References

{{reflist}}

  • Bill Gunston "The Osprey's Encyclopedia of Russian Aircraft", 2000
  • {{cite book |editor-last=Lambert |editor-first=Mark |title=Jane's All the World's Aircraft 1992–93 |year=1992 |location=Coulsdon, UK |publisher=Jane's Data Division |isbn=0-7106-0987-6}}