ZFWT Solar Eagle
Solar Eagle (Guang-fu-Ying or Guangfuying, 光伏鹰) is a series of UAVs developed by Beijing ZFWT Spatial Technology Co., Ltd. (ZFWT, 北京中飞万通有限公司), some of which has entered service with Chinese law enforcement and military. ZFWT Solar Eagle A1. Solar Eagle A1 is a miniature UAV of conventional design, powered by a two-blade propeller driven by a pusher engine mounted at the end of empennage. Constructed of composite material with flexible wings, Solar Eagle A1 can be stored in a six-inch diameter tube. Specification: Solar Eagle A2. Solar Eagle A2 is a micro air vehicle  (MAV) powered by a two-blade propeller driven by an electric motor mounted in the nose. Solar Eagle is constructed of carbon fiber and has a flying wing configuration. Specification: Solar Eagle A3. Solar Eagle A3 is a MAV of modular design for rapid deployment and operated by a 2 people crew. Solar Eagle 3 is in twin-boom configuration and the vertical rudders are joined at the top instead of at the root like most UAVs of twin boom configuration. Propulsion is provided by a two-blade propeller driven by a tractor motor installed in the nose of the  fuselage. Specification: Solar Eagle A4. Solar Eagle A4 is a MAV of conventional layout with V-tail, powered by a two-blade propeller driven by a pusher engine installed at empennage. The electro-optical payload is the entire nose section, instead of padded version like in most UAVs. Specification: Solar Eagle A5. Solar Eagle A5 is a quadrotor MAV. Solar Eagle A5 has a unique feature in that its rotors are installed below the arm instead above the arm like most multirotors. Specification: Solar Eagle A6. Solar Eagle A6 is a long range MAV resembles a scaledown version of AASI  Jetcruzer, except Solar Eagle A6 is powered by a two-blade propeller instead of five-blade propeller on Jetcruzer. Specification: Solar Eagle C1. Solar Eagle C1 is an UAV of flying wing design. The flying wing is shaped into an isosceles trapezoid with downward pointing winglets. Propulsion is provided by two-blade propeller driven by a tractor engine mounted in the nose. Specification: Solar Eagle C2. Solar Eagle C2 is a smaller cousin of Solar Eagle C1 and both share the identical layout. Specification: Solar Eagle C3. Solar Eagle C3 is an UAV of twin-boom configuration with inverted v -tail, powered by a propeller driven by a pusher engine mounted at the rear end of the fuselage, and has a tricycle landing gear system. Specification: Solar Eagle C4. Solar Eagle C4 is the larger cousin of Solar Eagle C3 with similar twin-boom configuration powered by a propeller driven by a pusher engine mounted at the rear end of the fuselage, and it has a tricycle landing gear system. Specification: Solar Eagle C5. Solar Eagle C5 is an octocopter. At first glance, Solar Eagle C5 might be easily mistaken as a quadcopter because there are only four arms, but  a closer look reveals that at the tip of each arm, there are two rotors installed, one above the arm and the other below, bringing the total rotors to eight. Specification: Solar Eagle C6. Solar Eagle C6 is an unmanned helicopter of conventional layout, and it is electrically powered. Specification: See also. List of unmanned aerial vehicles of the People's Republic of China