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词条 Yakovlev Yak-100
释义

  1. Design and development

  2. Specifications (Yak-100)

  3. See also

  4. References

  5. Further reading

name = Yak-100image = Yakovlev Yak-100.svgcaption =

}}{{Infobox Aircraft Type

type = Transport helicoptermanufacturer =designer =Yakovlevfirst flight = November 1948introduced =retired =produced = Moscow Plant No. 115number built = 2status = Project cancelledunit cost =primary user =more users =developed from =variants with their own articles =
}}

The Yakovlev Yak-100 was a single-engine, transport helicopter developed in the USSR in 1948. This was the Yakovlev Design Bureau's second helicopter.

Design and development

The Yak-100 (initially designated Yak-22) was developed in direct competition with Mikhail Mil's Mi-1. Bearing a striking resemblance to the Sikorsky H-5, the Yak-100 had a conventional main and anti-torque rotor configuration, driven by an Ivchenko AI-26GRFL radial piston engine. The pilot and crewman/passenger sat under a long greenhouse-style canopy, with very good visibility.[1]

Flight trials progressed quickly, with the almost ubiquitous vibration being tackled by moving the centre of gravity of the main rotor blades behind their flexural axes. Manufacturer's trials were completed in June 1950, with successful State acceptance trials following later that year.[1]

Although successful in trials, the Yak-100 was not put into production because the equally successful Mi-1 had already been prepared for production before the Yak-100 had completed acceptance trials. The second prototype had three seats as well as other minor improvements.[1]

Specifications (Yak-100)

{{Aircraft specs
|ref=OKB Yakovlev[1]
|prime units?=met


|crew=2
|capacity=+ 3rd seat in second prototype
|length m=13.91
|height m=
|empty weight kg=1690
|empty weight note=first prototype; {{cvt|1805|kg}} second prototype
|gross weight kg=
|max takeoff weight kg=2090
|max takeoff weight note=first prototype; {{cvt|2180|kg}} second prototype
|fuel capacity=
|more general=


|eng1 number=1
|eng1 name=Ivchenko AI-26GRFL
|eng1 type=
|eng1 kw=313
|rot number=1
|rot dia m=14.5
|rot dia ft=
|rot dia in=
|rot area sqm=
|rot area sqft=
|rot area note=3-bladed


|max speed kmh=170
|cruise speed kmh=
|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=
|range km=325
|endurance=
|ceiling m=5250
|ceiling note=

  • Hovering ceiling: {{cvt|2720|m}}

|g limits=
|roll rate=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|fuel consumption kg/km=
|fuel consumption lb/mi=
|power/mass=
|more performance=
}}

See also

{{aircontent|
|related=
|similar aircraft=
  • Sikorsky H-5
  • Bristol Sycamore
  • Weir W.9
  • Bell 48

|lists=
|see also=
}}

References

{{commons category|Yakovlev aircraft}}
1. ^{{cite book |last=Gordon |first=Yefim |title=OKB Yakovlev |year=2005 |publisher=Midland Publishing |location=Hinkley |isbn=1-85780-203-9 |author2=Dmitry |author3=Sergey Komissarov| pages=351-352}}

Further reading

  • {{cite book |last1=Gordon |first1=Yefim |last2=Gunston |first2=Bill| title=Yakovlev aircraft since 1924 |date=1997 |publisher=Putnam |location=London |isbn=0851778720 |edition=1st |page=126}}
{{Yakovlev aircraft}}

7 : Soviet military transport aircraft 1940–1949|Abandoned military aircraft projects of the Soviet Union|Military helicopters|Yakovlev aircraft|Soviet helicopters 1940–1949|Single-engined piston helicopters|Aircraft first flown in 1948

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