Kochyerigin DI-6

Kochyerigin DI-6

The Kochyerigin DI-6 had a limited and largely peripheral operational history during World War II, reflecting its obsolescence by the time hostilities intensified

Design Origins

Developed in the mid-1930s by Sergei Kochyerigin as a two-seat fighter and ground-attack biplane, the DI-6 was intended to fill a dual-role niche for the Soviet Air Force.

It featured a mixed-construction airframe, tandem cockpits for pilot and gunner, and retractable landing gear.

Production and Deployment

Approximately 222 units were built, but by the outbreak of WWII, the DI-6 was already outdated compared to newer monoplane designs.

It was primarily used for training and second-line duties rather than frontline combat.

Combat Use

There is no substantial evidence of the DI-6 participating in major combat operations during WWII.

Its performance and armament were insufficient for the evolving demands of aerial warfare, and it was quickly superseded by more modern aircraft like the I-15, I-16, and later Yak and LaGG series fighters.

Legacy

The DI-6’s operational relevance had faded by the early 1940s.

It served more as a transitional design in Soviet aviation development, bridging the gap between early biplanes and more advanced monoplanes.

The Variants

DI-6bis

Role

Trainer aircraft

Features

Simplified version of the DI-6 with fixed landing gear, optimised for pilot instruction and familiarisation.

Operational Use

Primarily used in training units; not intended for combat.

Its fixed gear reduced complexity and maintenance for student pilots.

DI-6Sh

(also designated TsKB-11Sh, TsKB-38)

Role

Ground-attack variant

Armament

Equipped with four forward-firing PV-1 machine guns mounted under the lower wing.

Protection

Featured an armoured pilot’s seat to enhance survivability in low-altitude attack missions.

Production

Approximately 60 units built.

Operational Use

Intended for close air support and battlefield interdiction; however, its performance and survivability were limited by its biplane configuration and light armour.

DI-6MMSh

Role

Experimental ground-attack prototype

Engine

Fitted with the M-300 X engine, a more powerful but ultimately unsuccessful power plant.

Outcome

Only one prototype was constructed; it did not enter serial production due to technical and performance shortcomings.

Specifications

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 lbs)

Gross weight

1,955 kg (4,310 lbs)

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 lbs./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 unsynchronised firings forward

&

one on a rear-facing mount, 750 rounds/gun

Bombs

Up to 40 kg (88 lbs) of bombs.

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