Development of Real-Time Maneuver Library Generation Technique for Implementing Tactical Maneuvers of Fixed-Wing Aircraft

Table 5

Configuration data of KLA-100 aircraft.

Maximum weight	620 kg
Maximum engine power	100 hp
Propeller diameter	1,700 mm
Propeller pitch angle at 0.75R	28.527 deg
Main wing span	10.311 m
Main wing reference area	11.607 m^2