Tectang UAV

Tectang UAVs are Chinese UAVs developed by Beijing Tectang Science and Technology Co., Ltd. (Tectang, 北京德可达科技有限公司). Tectang markets most of its products as Telicopter (Rui-Long or Ruilong, 瑞龙)series, which is also alternatively referred to as Intelligent Eagle (Zhi Ying or Zhiying, 智鹰) series.

TC-2130 Telicopter TT (Intelligent Eagle I)
TC-2130 Telicopter TT, also known as Intelligent Eagle I, is a twin-engine unmanned helicopter of conventional helicopter layout, and the landing gear system consists of a pair of skids. TC-2130 is constructed of carbon fiber and powered by a turbocharged kerosene engine. Specification:
 * Main rotor diameter: 3.3 m
 * Length: 2.9 m
 * Height: 0.9 m
 * Empty weight: 45 kg
 * Max take-off weight: 90 kg
 * Payload: 30 kg
 * Ceiling: 2 km
 * Cruise speed: 72 km/hr

TC-1235 Telicopter 35 (Intelligent Eagle II)
TC-1235 Telicopter 35, also known as Intelligent Eagle II, is a single-engine unmanned helicopter of intermeshing rotors layout. TC-1235 is powered by a gasoline engine and has a pair of skids as landing gear system. TC-1235 is the larger cousin of the smaller TC-1210.
 * Main rotor diameter: 2.8 m
 * Length: 19.8 m
 * Height: 0.86 m
 * Empty weight: 40 kg
 * Max take-off weight: 76 kg
 * Payload: 35 kg
 * Fuel: 20 L
 * Endurance: 4 hr
 * Cruise speed: 100 km/hr

TC-1210 Telicopter 10 (Intelligent Eagle III)
TC-1210 Telicopter 10, also known as Intelligent Eagle III, is a single-engine unmanned helicopter of intermeshing rotors layout. TC-1235 is powered by a gasoline engine and has a pair of skids as landing gear system. TC-1210 is the smaller cousin of larger TC-1235, and it is powered by kerosene engine instead of gasoline engine of TC-1235.
 * Main rotor diameter: 2.3 m
 * Length: 1.7 m
 * Height: 0.66 m
 * Empty weight: 17 kg
 * Max take-off weight: 35 kg
 * Payload: 10 kg
 * Fuel: 6 L
 * Cruise speed: 100 km/hr
 * Endurance: 40 min

PAMS
PAMS UAV is a hand-held fixed-wing micro air vehicle (MAV) of flying wing layout with winglets. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the rear end of empennage. Specification:
 * Normal operating altitude: 150 – 200 m
 * Length: 1.2 m
 * Empty weight: 1 kg
 * Endurance: 1 hr
 * Power plant: electric motor