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UAV Sci-Tech UAV
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UAV Sci-Tech UAV : ウィキペディア英語版
UAV Sci-Tech UAV
UAV Sci-Tech UAVs are Chinese UAVs developed by Beijing (UAV Sci-Tech Co., Ltd. (UAV Sci-Tech, 北京国遥星图航空科技有限公司) ), and these UAVs include both fixed-wing and rotary-wing UAVs.
==Delta-wing UAV==
Delta wing UAV is a fixed-wing micro air vehicle (MAV) developed by UAV Sci-Tech, and it does not have any vertical rudder. Propulsion is provided by a two-blade propeller driven by a pusher engine mounted at the empennage, and the UAV is usually launched via catapult. This MAV can either be gasoline or electrically powered, and is constructed of carbon fiber and fiber glass. Specification:〔(Delta-wing UAV )〕
*Length (m): 1
*Width (m): 2.1
*Power: Gasoline or electric
*Endurance: (min) 60 for electrically powered version, 90 – 120 for gasoline-powered version
*Payload (kg): 1.4
*Max take-off weight (kg): 7.5
*Remote control radius (km): 30
*Max speed (km/hr): 120
*Cruise speed (km/hr): 72
*Launch: catapult
*Recovery: parachute

抄文引用元・出典: フリー百科事典『 ウィキペディア(Wikipedia)
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