“Beriev Be-8”的意思、由来-开放百科全书

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Beriev Be-8

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Specifications (Be-8)
References

name= Be-8

image=

caption=

}}{{Infobox Aircraft Type

type=Airliner

manufacturer=Beriev

designer=

[1]>introduced=

retired=

status=Did not enter mass-production

primary user=

more users=

produced=

number built=2

unit cost=

variants with their own articles=
}}

The Beriev Be-8 (USAF/DoD reporting name "Type 33",^[1] NATO reporting name "Mole"^[2]), was built by the Soviet Beriev OKB in 1947. It was a passenger/liaison amphibian aircraft with a layout similar to the Be-4 but substantially larger and heavier. It was a single engined parasol winged aircraft, with the wing installed on a thin pylon and a pair of short struts. Compared to the Be-4, the Be-8 was equipped with retractable landing gear, with cockpit and passenger cabins heated by an engine exhaust heat exchanger. The Be-8 was intended as a civil aircraft and carried no armament. First flight was on 3 December 1947, demonstrating good performance and of the two prototypes, one was demonstrated during the 1951 Soviet Aviation Day at Tushino.

One of Be-8 was equipped with hydrofoils, developed at TsAGI. These "Underwater Wings" were installed on landing gear struts and raised the aircraft above the water, well before the aerodynamic lift could support the aircraft. As a result, takeoff was much easier and imposed less punishment on the hull from the waves.

Despite being very effective during take-off, the hydrofoils resulted in increased drag and a reduction in maximum airspeed. Construction of retractable hydrofoils was not ready, and the concept did not find practical applications.

Specifications (Be-8)

{{Aircraft specs
|ref=The Osprey Encyclopedia of Russian Aircraft 1875–1995^[3]
|prime units?=met

|genhide=
|crew=2
|capacity=6 passengers
|length m=13.0
|span m=19.0
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=40
|aspect ratio=
|airfoil=
|empty weight kg=2815
|gross weight kg=3624
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity={{convert|352|kg|abbr=on}}
|more general=

|max speed kmh=266
|max speed note=at {{convert|1800|m|ft|abbr=on}}
|cruise speed kmh=220
|stall speed kmh=
|stall speed mph=
|stall speed kts=
|stall speed note=
|range km=1205
|ferry range km=
|ferry range miles=
|ferry range nmi=
|ferry range note=
|endurance=
|ceiling m=5500
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|more performance=
|avionics=
}}

References

1. ^{{cite web|url=http://www.designation-systems.net/non-us/soviet.html#_DOD_Type|title=Designations of Soviet and Russian Military Aircraft and Missiles|publisher=|accessdate=20 December 2014}}
2. ^{{cite web|url=http://www.designation-systems.net/non-us/soviet.html#_Listings_Misc|title=Designations of Soviet and Russian Military Aircraft and Missiles|publisher=|accessdate=20 December 2014}}
3. ^¹Gunston 1995, p. 50.

Gunston, Bill. The Osprey Encyclopedia of Russian Aircraft 1875–1995. London: Osprey, 1995. {{ISBN|1-85532-405-9}}.

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