Soviet Union's Ilyushin Il-10 Shturmovik close support, ground attack
Design
The Ilyushin Il-10 Shturmovik was designed to replace the Il-2.1 Sergei Vladimirovich Ilyushin designed the Il-10.2
There were two designs that came out of the Ilyushin Design Bureau.1 The Il-8 resembled the Il-2 with a Mikulin AM-42 engine.1 It also had new wings, horizontal tail surfaces, and undercarriage.1,2
The Il-10 was smaller and more streamlined.1 It also used the more powerful Mikulin AM-42 engine.1 The cockpit was improved for the crew as armor was added.1,2 The undercarriage was also modified.1 It was more maneuverable and had better performance.1
Prototype
The Il-8 and Il-10 prototypes each flew in April 1944.1,2
Production
Production began in October 1944.1 The last Il-10 was delivered in 1955.1
- Ilyushin Il-10: 4,9661
- Soviet Union1
- B-33, CB-33: ~2,0001
- by Avia in Czechoslovakia1
Variants
- Ilyushin Il-10: Main version.1
- Ilyushin Il-10M: Postwar version that had new wing.1 The fuselage was longer.1 It could also carry more fuel.1
- Ilyushin Il-10U: Trainer.1
- B-33: Avia produced Il-10.1
- CB-33: Avia produced Il-10U.1
Usage
The Il-10 was first used operationally in February 1945.1 By May 1945 the Il-10 had replaced the Il-2s in many regiments.1
The Il-10 was used against the Japanese in Manchuria and Korea in August 1945.1
Post World War II
The Il-10 was supplied to Albania, Bulgaria, China, Czechoslovakia, East Germany, Hungary, North Korea, and Romania.2
North Korea used them in the Korean War.1,2
Specifications
| Ilyushin Il-10 Shturmovik1,2 | |
|---|---|
| Type | Attack2, Ground attack1 |
| Crew | 21,2 |
| Engine (Type) | Mikulin AM.422 Mikulin AM-421 |
| Cylinders | V 121,2 |
| Cooling | |
| HP | 2,0001,2 |
| Propeller blades | 31 |
| Fuel capacity | |
| Dimensions | |
| Span | 43' 11.5"1, 45' 7"2 13.4 m1 |
| Length | 36' 9"1, 40'2 11.2 m1 |
| Height | 11' 6"1,2 3.5 m1 |
| Wing area | |
| Weight | |
| Empty | 9,920 lb1 4,500 kg1 |
| Loaded | 13,968 lb2, 14,409 lb1 6,536 kg1 |
| Performance | |
| Speed at sea level | 311 mph1 500 kph1 |
| Speed @ 7,875' / 2,400 m |
329 mph1 529 kph1 |
| Speed @ 9,180' | 311 mph2 |
| Cruising speed | |
| Climb | |
| Climb to 9,840' / 3,000 m |
5 minutes1 |
| Service ceiling | 23,795'1 7,250 m1 |
| Range | 497 miles1 800 km1 |
| Armament | |
| Wings | 2: 7.62 mm MG1 2 or 4: 20 mm1 |
| OR | 2 or 4: 23 mm1 |
| Rear cockpit | 1: 12.7 mm MG1 1: 20 mm1 |
| Wing - racks - bombs | 2,205 lb1 1,000 kg1 |
| Wing - racks - rockets | 8: 82 mm1 |
| OR | 8: 132 mm1 |
Sources:
- Aircraft of WWII, Stewart Wilson, 1998
- World War II Airplanes Volume 2, Enzo Angelucci, Paolo Matricardi, 1976

