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Quick Eye UAVs are Chinese UAVs developed by (Institute of Remote Sensing and Digital Earth (RADI, 中国科学院遥感与数字地球研究所) ) of Chinese Academy of Sciences via its wholly owned companies including Tianjin ((ChinaRS, 中科遥感信息技术有限公司) ) and Beijing (NCG Information Technology Co., Ltd. (NCG, 北京国遥万维信息技术) ).Most of these UAVs are intended for aerial photography, survey and remote sensing missions. ==Quick Eye I== Quick Eye I is a fixed wing UAV developed by RADI for aerial photography, survey and remote sensing missions, and it is the first member of Quick Eye series fixed wing UAV developed by RADI. Quick Eye I is in conventional layout with high wing configuration and landing gear consists of a pair of skids. Propulsion is provided by a two-blade driven tractor engine mounted in the nose. Specification:〔(【引用サイトリンク】 title=Quick Eye )〕 *Wingspan (m): 2.6 *Length (m): 1.8 *Height (m): 0.5 *Wing area (m2): 0.9 *Payload (kg): 2.5 *Empty weight (kg): 10 *Fuel (L): 2.2 *Max take-off weight (kg): 14 *Propeller diameter (m): 0.6 *Max speed (km/h): 140 *Cruise speed (km/h): 97 *Ceiling (km): 3.5 *g-overload: 3.5 g *Rate of climb (m/s): 5 *Endurance (min): 100 *Max range (km): 150 *Standard operational range (km): 110 *Engine: gasoline powered *Fuel consumption (ml/min): 22 *Max wind speed allowed for operation (m/s): 13 *Max wind scale allowed for launch and recovery: 5 *Launch: by hand *Recovery: parachute 抄文引用元・出典: フリー百科事典『 ウィキペディア（Wikipedia）』 ■ウィキペディアで「RADI Quick Eye」の詳細全文を読む スポンサード リンク
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