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ST Aerospace Skyblade
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ST Aerospace Skyblade : ウィキペディア英語版
ST Aerospace Skyblade
The Skyblade is a man-portable mini-UAV developed by ST Aerospace, designed to be used by two operators for short-range battlefield or tactical reconnaissance and artillery spotting.
==Models==

*Skyblade I: Prototype version. Jointly developed with local research house (DSO National Laboratories)
*Skyblade II: Advance Production exploration, gasoline engine. Completely in-house developed. Didn't make it to full production.
*Skyblade III: Production version, all electric systems. Jointly developed with local research house (DSO National Laboratories)
The Skyblade III is designed for rapid 2-man deployment to support military and civilian applications. Developed for fully autonomous flight operations, it delivers quick and accurate intelligence in real-time to tactical commanders in the field.
*Skyblade IV: New tactical UAV
The SkyBlade IV is completely new a close-range tactical UAV unveiled in Asian Aerospace 2006, with a takeoff weight of 50 kilograms (110 pounds), including a 12 kilogram (26 pound) payload, a torpedo-like fuselage, a straight high-mounted wing with upturned wingtips, cruciform tailfins and a pusher prop driven by a piston engine with an endurance of up to 12 hours. The UAV carries an EO-IR sensor system with STA working on a miniaturized SAR. The vehicle is catapult launched and is recovered via parachutes or catch nets.
Skyblade IV can perform a variety of operational missions such as surveillance, reconnaissance, fire support and battle damage assessment.

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「ST Aerospace Skyblade」の詳細全文を読む



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