• 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 a completely new close-range tactical UAV unveiled in
Asian Aerospace 2006, with a takeoff weight of , including a 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. == Military use in Singapore ==