UAV Loading and Performance

the rudder. the ailerons. the stabilizer. 

the CG is shifted rearward to the aft CG limit. the gross weight is reduced. the airplane is subjected to maneuvers other than straight and level flight.

It increases performance. It has no effect over performance. It decreases performance.

exceeds its critical angle of attack.  exceeds the maximum speed. exceeds maximum allowable operating weight.

have a tendency to spin. be more difficult to control. stall at a higher airspeed. 

Faster speed. Shorter endurance.  Increased maneuverability.

stalling at higher-than-normal airspeed. a longer takeoff run. difficulty in recovering from a stalled condition. 

can be easily removed without the use of tools. is visible to the visual observer or other crew members. does not adversely affect the center of gravity.

30 degrees. 15 degrees. 45-50 degrees.

  34 pounds. 38 pounds.  47 pounds.