Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the SAF Atlas Army Co-operation Aircraft.
1 x Armstrong Siddeley Jaguar IVC 14-cylinder twin-row air-cooled radial piston engine developing 450 horsepower and driving a two-bladed propeller unit at the nose.
Propulsion
84 mph
135 kph | 73 kts
Max Speed
15,420 ft
4,700 m | 3 miles
Service Ceiling
395 miles
635 km | 343 nm
Operational Range
855 ft/min
261 m/min
Rate-of-Climb