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词条 Yokosuka R2Y
释义

  1. Design and development

  2. Specifications (R2Y1)

  3. See also

  4. References

     Notes  Bibliography 

  5. External links

name = Yokosuka R2Yimage = Yokosuka R2Y.jpgcaption =

}}{{Infobox Aircraft Type

type = Reconnaissance, Fightermanufacturer = Yokosukadesigner =first flight = 8 May 1945introduced =retired =produced =number built = 3 (1 completed)status = Cancelledunit cost =primary user = Imperial Japanese Navy (intended)more users =developed from =variants with their own articles =
}}

The Yokosuka R2Y Keiun (景雲 - "Cirrus Cloud") was a prototype reconnaissance aircraft built in Japan late in World War II.

Design and development

Commissioned for the Imperial Japanese Navy after the R1Y design was cancelled due to its disappointing performance estimates, the R2Y used coupled engines driving a single propeller and also featured a tricycle undercarriage.

Completed in April 1945, the prototype made a short flight on 8 May, but was destroyed in a US air raid only a few days later, thus ending development.

A proposal was also made to develop the R2Y into a turbojet-powered light bomber by replacing its piston engines with two Mitsubishi Ne-330s. Designated the R2Y2 Keiun Kai, it did not enter construction before the end of the war.

Specifications (R2Y1)

{{Aircraft specifications
|plane or copter?=plane
|jet or prop?=prop
|ref=Japanese Aircraft of the Pacific War[1]
|crew= 2
|capacity=
|length main= 13.05 m
|length alt= 42 ft 10 in
|span main= 14.00 m
|span alt= 45 ft 11 in
|height main= 4.24 m
|height alt= 13 ft 9 in
|area main= 34.0 m²
|area alt= 366 ft²
|airfoil=
|empty weight main= 6,015 kg
|empty weight alt= 13,261 lb
|loaded weight main= 8,100 kg
|loaded weight alt= 17,857 lb
|useful load main=
|useful load alt=
|max takeoff weight main= 9,400 kg
|max takeoff weight alt= 20,723 lb
|more general=
|engine (prop)= Aichi Ha-70 (Two 1,300 kW (1,700 hp) Aichi Atsuta engines coupled to a gearbox)
|number of props= 1
|power main= 2,500 kW
|power alt= 3,400 hp
|power original=
|max speed main= 770 km/h
|max speed alt= 416 kn, 480 mph
|cruise speed main=
|cruise speed alt=
|stall speed main=
|stall speed alt=
|never exceed speed main=
|never exceed speed alt=
|range main= 3,610 km
|range alt= 1,949 nmi, 2,251 mi
|ceiling main= 12,700 m
|ceiling alt= 38,376 ft
|climb rate main= 1100 m/min
|climb rate alt= 3609 ft/min
|loading main= 238 kg/m²
|loading alt= 49 lb/ft²
|thrust/weight=
|power/mass main= 31 W/kg
|power/mass alt= 0.19 hp/lb
|more performance=
|armament=
|avionics=
}}

See also

{{aircontent
|related=
|similar aircraft=
  • Heinkel He 119 (tandem-engine with single propeller)
  • Kawasaki Ki-64 (tandem-engine with single propeller)
  • Messerschmitt Me 509

|sequence=
|lists=
  • List of aircraft of World War II

}}

References

Notes

1. ^{{Harvnb|Francillon|1979|p=475.}}

Bibliography

{{refbegin}}
  • Francillon, Ph.D., René J. Japanese Aircraft of the Pacific War. London: Putnam & Company Ltd., 1970 (2nd edition 1979). {{ISBN|0-370-30251-6}}.
{{refend}}

External links

{{commons category-inline|Yokosuka R2Y Keiun}}{{Yokosuka aircraft}}{{Japanese Navy Reconnaissance Aircraft}}{{DEFAULTSORT:R2Y, Yokosuka}}

5 : Japanese experimental aircraft 1940–1949|Japanese military reconnaissance aircraft 1940–1949|Yokosuka aircraft|Aircraft first flown in 1945|Mid-engined_aircraft

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