Petlyakov VI-100 Technical Specifications
Service Year: 1940
Type: Heavy Twin-Engine Interceptor Prototype Aircraft
National Origin: Soviet Union
Manufacturer(s): Petlyakov - Soviet Union
Production Total: 1
Structural (Crew Space, Dimensions and Weights)
Operating Crew (Typical): 2
Overall Length: 41.01 feet (12.5 meters)
Overall Width: 56.30 feet (17.16 meters)
Overall Height: 11.48 feet (3.50 meters)
Weight (Empty): 11,905 lb (5,400 kg)
Weight (MTOW): 16,006 lb (7,260 kg)
Installed Power and Standard Day Performance
Propulsion: 2 x Klimov M-105 turbocharged inline piston engines developing 1,050 horsepower each.
Maximum Speed: 332 mph (535 kph; 289 knots)
Maximum Range: 870 miles (1,400 km)
Service Ceiling: 40,026 feet (12,200 meters; 7.58 miles)
Rate-of-Climb: 2,415 feet-per-minute (736 m/min)
Armament / Mission Payload
2 x 20mm ShVAK cannons in fixed, forward-firing position at nose.
2 x 7.62mm ShKAS machine guns in fixed, forward-firing position at nose.
1 x 7.62mm ShKAS machine gun on flexible mount in rear cockpit.
Coventional drop bombs and rockets held at underwing racks.
Global Operators / Customers
Soviet Union (cancelled)
Model Variants (Including Prototypes)
VI-100 - Base Series Designation; single prototype completed.