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词条 Polikarpov SPB (D)
释义

  1. Development

  2. Specifications

  3. References

     Notes  Bibliography 

  4. External links

name=Polikarpov SPB (D) image=PolikarpovSPB(D).jpg caption=A SPB (D) in a wind tunnel

}}{{Infobox Aircraft Type

type=Dive bomber national origin=Soviet Union manufacturer=Polikarpov designer= first flight=18 February 1940 introduced= retired= status=Cancelled primary user= number built=6 developed from= Polikarpov VIT-2 variants with their own articles=
}}

The Polikarpov SPB (D) (Skorostnoy Pikiruyushchy Bombardirovshchik (Dalnost)—High Speed Dive Bomber (Distance)) was a Soviet twin-engined dive bomber designed before World War II. A single prototype and five pre-production aircraft were built, but two crashed and the program was cancelled in favor of the Petlyakov Pe-2.

Development

The SPB (D) closely resembled the Polikarpov VIT-2, which had been recommended for production as a dive bomber, but the former actually was an entirely new design. It was smaller than the VIT-2 and had a monocoque fuselage. The main gears of the conventional undercarriage retracted aft into the rear of the engine nacelles and the tail wheel retracted into the rear fuselage. Two {{convert|783|kW|0|abbr=on}} liquid-cooled Klimov M-105 V12 engines were slung underneath the wings.[1] It retained its predecessor's prominent canopy and nose glazing, but reduced the armament to a single {{convert|7.62|mm|abbr=on}} ShKAS machine gun for the bombardier/navigator while the rear gunner had a retractable {{convert|12.7|mm|abbr=on}} Berezin UB dorsal gun and a ventral ShKAS to protect the aircraft's underside. The bomb bay could carry up to 800 kg (1,764 lbs) internally and an additional 700 kg (1,543 lbs) of bombs could be carried underneath the wings.[2]

In addition to the SPB (D) prototype, five pre-production machines were ordered even before the prototype made its first flight. This flight, piloted by Boris Kudrin,[3] occurred safely on 18 February 1940, but on 27 April 1940 the first prototype crashed for unknown causes, killing test pilot Pavel Golovin.[3]

On 2 June 1940 test pilot Mikhail Lipkin barely survived when, landing with engines out, his SPB (D) clipped a parked Tupolev SB. On 30 June the second SPB (D) disintegrated in flight. Lipkin and flight engineer Bulychov, instructed to test wing flutter at an extreme 600-km/h (373-mph) diving speed, were killed in the crash; the aircraft actually disintegrated in horizontal flight. Investigators initially blamed the accident on Polikarpov's deputy Zhemchuzhin, who allegedly failed to fit the balance weights into the leading edges of the ailerons, causing wild flutter.[3] Later they also blamed Lipkin, already dead, for the alleged reckless increase of speed.[3] TsAGI engineers and airfield staff voiced suspicion that other factors could have been involved, but these were not examined at all.

The third prototype, piloted by Kudrin, lost horizontal trim tab in flight; the pilot managed to land the plane but refused to fly on SPB (D) prototypes anymore.[3][8] On 29 July 1940 the project was cancelled; tests required for proper crash examination were not completed. The government preferred to build twin-engined dive bombers on a simplified Petlyakov VI-100 platform,[3] – the conversion, named Petlyakov Pe-2, took over the roles originally intended for the SPB (D).[4]

Specifications

{{Aircraft specs
|ref=Gunston, The Osprey Encyclopaedia of Russian Aircraft 1875–1995
|prime units?=met


|crew=5
|capacity=
|length m=11.2
|length ft=
|length in=
|length note=
|span m=17
|span ft=
|span in=
|span note=
|height m=
|height ft=
|height in=
|height note=
|wing area sqm=42.93
|wing area sqft=
|wing area note=
|airfoil=
|empty weight kg=4480
|empty weight lb=
|empty weight note=
|gross weight kg=6850
|gross weight lb=
|gross weight note=
|max takeoff weight kg=
|max takeoff weight lb=
|max takeoff weight note=
|fuel capacity=
|more general=


|eng1 number=2
|eng1 name=Klimov M-105
|eng1 type=V-12 inline engines
|eng1 kw=783
|eng1 hp=
|eng1 note=
|prop blade number=3
|prop name=
|prop dia m=
|prop dia ft=
|prop dia in=
|prop note=


|max speed kmh=520
|max speed mph=
|max speed kts=
|max speed note=at {{convert|4500|m|0}}
|cruise speed kmh=
|cruise speed mph=
|cruise speed kts=
|cruise speed note=
|range km=2200
|range miles=
|range nmi=
|range note=
|ceiling m=9000
|ceiling ft=
|ceiling note=
|climb rate ms=
|climb rate ftmin=
|climb rate note=
|time to altitude=
|wing loading kg/m2
|wing loading lb/sqft=
|wing loading note=
|disk loading kg/m2=
|disk loading lb/sqft=
|disk loading note=
|power/mass=
|thrust/weight=
|more performance=


|guns=

  • 1x 12.7 mm Berezin UB machine gun
  • 2x 7.62 mm ShKAS machine guns

|bombs=up to {{convert|1500|kg|0}} (800 internal, 700 external)
|avionics=
}}{{aircontent
|see also=
|related=
|similar aircraft=
  • Petlyakov Pe-2

|lists=
}}

References

Notes

1. ^Gunston, p. 306
2. ^Gordon, pp. 282–83
3. ^Shavrov, chapter on Polikarpov's multi-role aircraft
4. ^Gordon, p. 283

Bibliography

{{refbegin}}
  • Gordon, Yefim. Soviet Airpower in World War 2. Hinckley, England: Midland Publishing, 2008 {{ISBN|978-1-85780-304-4}}
  • Gunston, Bill. The Osprey Encyclopaedia of Russian Aircraft 1875–1995. London, Osprey, 1995 {{ISBN|1-85532-405-9}}
  • Vadim Shavrov (2002, in Russian). Istoria konstrukcii samolyotov v SSSR, 1938-1950 (История конструкций самолетов в СССР 1938-1950), vol. 2. {{ISBN|5-217-03103-4}}
{{refend}}

External links

{{commons category|Polikarpov}}
  • SPB, D, D-3
{{Polikarpov aircraft}}{{DEFAULTSORT:Polikarpov Spb (D)}}

5 : Polikarpov aircraft|Soviet attack aircraft 1940–1949|Abandoned military aircraft projects of the Soviet Union|Twin-engined tractor aircraft|Aircraft first flown in 1940

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