DI-3

The Grigorovich DI-3 (Russian: Григорович ДИ-3), (Dvukhmyestnyi Istrebitel - two-seat fighter), was a prototype two-seat fighter developed in the Soviet Union in the 1930s. It was intended to be a long-range escort fighter developed from the DI-2 with improved range and performance comparable to single-seat fighter aircraft of the time. DI-3 was a single-bay biplane of mixed construction with a twin-rudder tailplane of variable incidence. Although initial tests demonstrated flight characteristics comparable to Polikarpov I-5, the addition of armament and operational equipment caused significant degradation in performance and DI-3 did not enter mass production. The prototype was subsequently fitted with an enclosed cockpit and used as a VIP transport.
Summary from Wikipedia, photo via Wikimedia Commons, licensed under CC BY-SA.
- Manufacturer
- Dmitry Pavlovich Grigorovich
- Category
- Fighters
- Country of origin
- Soviet Union
- First flight
- 1931-08-01
Specifications
- Max speed
- 138 kt
- Service ceiling
- 20,700 ft
- Max takeoff weight
- 4,678 lb
- Empty weight
- 3,278 lb
- Powerplant
- BMW VI 7.3z
- Engines
- 1
- Seats
- 2
- Length
- 25 ft
- Wingspan
- 38 ft
Specifications are approximate and may vary by variant. Compiled from Wikipedia (CC BY-SA).
Reference and training only. Specifications vary by variant — consult the manufacturer and the official documents.