Ilyushin IL-1 Technical Specifications
Service Year: 1944
Type: Ground Attack Fighter Prototype
National Origin: Soviet Union
Manufacturer(s): Ilyushin Design Bureau - Soviet Union
Production Total: 1
Structural (Crew Space, Dimensions and Weights)
Operating Crew (Typical): 1
Overall Length: 36.48 feet (11.12 meters)
Overall Width: 43.96 feet (13.40 meters)
Overall Height: 13.39 feet (4.08 meters)
Weight (Empty): 9,447 lb (4,285 kg)
Weight (MTOW): 11,729 lb (5,320 kg)
Installed Power and Standard Day Performance
Propulsion: 1 x Mikulin AM-42 V12 inline piston engine developing 1,973 horsepower.
Maximum Speed: 360 mph (580 kph; 313 knots)
Maximum Range: 621 miles (1,000 km)
Service Ceiling: 28,215 feet (8,600 meters; 5.34 miles)
Rate-of-Climb: 625 feet-per-minute (190 m/min)
Armament / Mission Payload
2 x 23mm VYa-23 cannons, one per wing.
Up to 440 pounds of conventional drop ordnance or air-to-surface rockets.
Global Operators / Customers
Soviet Union (cancelled)
Model Variants (Including Prototypes)
IL-1 - Base Product Designation; sole prototype example completed.