Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the Armstrong Whitworth Atlas I Army Liaison / Co-Operation Biplane Aircraft.
1 x Armstrong Siddeley "Jaguar" IVC 14-cylinder twin-row, air-cooled, radial engine developing 450 horsepower driving two-bladed propeller unit at the nose.
Propulsion
143 mph
230 kph | 124 kts
Max Speed
16,798 ft
5,120 m | 3 miles
Service Ceiling
401 miles
645 km | 348 nm
Operational Range