Movatterモバイル変換


[0]ホーム

URL:


Jump to content
WikipediaThe Free Encyclopedia
Search

Kochyerigin DI-6

From Wikipedia, the free encyclopedia
DI-6/TsKB-11
Kochyerigin DI-6i
RoleFighter
Type of aircraft
National originSoviet Union
ManufacturerFactory No.39
DesignerSergei Aleksandrovich Kochyerigin
First flight30 September 1934
Primary userSoviet Air Force
Number built222

Kochyerigin DI-6 (internal designationTsKB-11;Russian:Кочеригин ДИ-6/ЦКБ-11) was a two-seat fighter biplane produced in the Soviet Union in the 1930s.

Design and development

[edit]

The DI-6 was a conventional single-bay biplane of mixed construction with cable-retracted main landing gear. The pilot and the tail gunner sat in tandem cockpits, the pilot's open, and the gunner's partially enclosed. To maximize the gunner'sarc of fire, the rear cockpit was set lower in the fuselage than the pilot's.

The DI-6 was developed atTsKB as a fighter that would also be capable of ground attack when fitted with different armament. Originally intended to use a liquid-cooled V-12 engine, problems with its development led to the choice of theWright R-1820radial engine instead. The first flight took place on 30 September 1934, and testing began in earnest in early 1935, with State Acceptance Trials following between May and November. Despite a number of weaknesses discovered during testing, the type was ordered into production, and deliveries to the Soviet Air Force commenced in the spring of 1937. Problems including excessive vibration, and a poor field of fire for the gunner, were never adequately resolved, and the various fixes implemented to cure these and other problems eventually added around 160 kg (350 lb) to the aircraft's weight. Production continued until 1939.

Operational history

[edit]

Pre-GlasnostWestern sources often reported these aircraft as having participated in theBattle of Khalkhin Gol against Japan in 1939, and even in theWinter War againstFinland in 1939–1940, but more recent scholarship has failed to uncover any evidence that it was deployed in either case.[1]

Surviving examples

[edit]

A replica DI-6 is displayed in Victory Park, at theMuseum of the Great Patriotic War inMoscow.

Variants

[edit]
DI-6bis
Trainer with fixed landing gear.
DI-6Sh (TsKB-11Sh, TsKB-38)
Ground attack variant with armored pilot's seat and four forward-firingPV-1 machine guns under the bottom wing; 60 built.
DI-6MMSh
One prototype with M-300X engine, did not enter production.

Operators

[edit]
 Soviet Union

Specifications (DI-6)

[edit]

Data fromShavrov 1985[2]

General characteristics

  • Crew: 2
  • Length: 6.87 m (22 ft 6 in)
  • Wingspan: 9.94 m (32 ft 7 in)
  • Height: 3.2 m (10 ft 6 in)
  • Wing area: 25.15 m2 (270.7 sq ft)
  • Empty weight: 1,360 kg (2,998 lb)
  • Gross weight: 1,955 kg (4,310 lb)
  • Powerplant: 1 ×Shvetsov M-25 9-cylinder air-cooled radial piston engine, 522 kW (700 hp)
  • Propellers: 2-bladed variable-pitch propeller

Performance

  • Maximum speed: 372 km/h (231 mph, 201 kn)
  • Range: 500 km (310 mi, 270 nmi)
  • Service ceiling: 7,700 m (25,300 ft)
  • Time to altitude: 5,000 m (16,000 ft) in 10 minutes
  • Wing loading: 78 kg/m2 (16 lb/sq ft)
  • Power/mass: 0.27 kW/kg (0.16 hp/lb)
  • Horizontal turn time: 12 seconds

Armament

  • Guns: 3× 7.62 mm (0.3 in)ShKAS machine guns, two unsynchronized firing forward and one on a rear-facing mount, 750 rounds/gun
  • Bombs: Up to 40 kg (88 lb) of bombs

References

[edit]
Wikimedia Commons has media related toKochyerigin DI-6.
  1. ^Mellinger
  2. ^Shavrov V.B. (1985).Istoriia konstruktskii samoletov v SSSR do 1938 g. (3 izd.) (in Russian). Mashinostroenie.ISBN 5-217-03112-3.
Aircraft designed bySergei Aleksandrovich Kochyerigin or his design bureau
Aircraft designed byTsKB
Sovietfighter designations, 1923–1940
Fighters (I)
Two-seat fighter (DI)
Multi-seat fighter (MI)
Cannon fighter (IP)
Descriptors
1 Unknown/not assigned
Retrieved from "https://en.wikipedia.org/w/index.php?title=Kochyerigin_DI-6&oldid=1263309966"
Categories:
Hidden categories:

[8]ページ先頭

©2009-2025 Movatter.jp