Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Grigorovich I-Z Cannon-Armed Fighter Prototype.
1 x M-22 air-cooled radial piston engines developing 480 horsepower and driving a two-bladed propeller at the nose.
Propulsion
162 mph
260 kph | 140 kts
Max Speed
22,966 ft
7,000 m | 4 miles
Service Ceiling
373 miles
600 km | 324 nm
Operational Range
1,170 ft/min
357 m/min
Rate-of-Climb
City-to-City Ranges
Operational range when compared to distances between major cities (in KM).