Power & Performance
Those special qualities that separate one aircraft design from another. Performance specifications presented assume optimal operating conditions for the NCSIST Chien Hsiang Loitering Munition Unmanned Aircraft System (UAS).
1 x Conventional engine driving twin-bladed propeller unit at rear of fuselage.
Propulsion
115 mph
185 kph | 100 kts
Max Speed
4,003 ft
1,220 m | 0 miles
Service Ceiling