Frag Out! Magazine
Issue link: https://fragout.uberflip.com/i/693549
C-UAS WARMATE Specs Sheet: Take-off Cassette pneumatic launcher Radius of action 10 km LOS Maximum flight height 500 m over ground, 3000 m AMSL Operating height 30–200 m over ground Sustainability of flight 30 minutes Take-off mass 4 kg Maximum horizontal speed 150 km/h Payloads: stabilized observation, observation and combat with cumulative or fragmentation charge – net mass of the combat charge: 700 g Full autonomy of flight Immediate and continuous readiness for combat or surveillance missions Aided targeting in combat mission mode Parameters of payloads: Cumulative and fragmentation GK-1 payload de- signed for striking light tanks and armored transport- ers. It is attached to the carrier (UAV), prepared for in- tegration with WARMATE Basic parameters of GK-1: @ armor penetration – 100–120 mm RHA @ SAD protection system (Save – Arm – Disarm); @ full information on the status of payload activation and change of the payload activation status is avail- able through the operator's control panel. Fragmentation and high-explosive GO-1 is de- signed for striking unarmored targets: sharpshooters, machine gun positions, points of resistance. It is attached to the carrier (UAV), prepared for integration with WARMATE. Basic parameters of GO-1: @ radius of efficient strike – 10 m; @ explosive – 300 g of TNT; @ SAD protection system (Save – Arm – Disarm); @ full information on the status of payload activation and change of the payload activation status is available through the operator's control panel. The system consists of the following base compo- nents: @ air vehicle, @ observation payload GS9 (as in VIRTUS system), @ combat and observation payload with fragmentation warhead (GO-1), @ combat and observation payload with cumulative warhead (GK-1), @ ground control station (SKiK), @ ground data terminal with antenna tracker (NTD), @ pneumatic launcher, @ transport case. The system has been equipped with in control modules that allow fully automatic operation of the majority of flight stages and strong support for the operator when targeting. The operator has full control and responsibility for activating the charge to allow striking action. The presentation in Toruń included a demonstration of surveillance capabilities of WARMATE, automatic flight, targeting, a simulated attack on a selected target, and landing with recovery of the air vehicle. Is should be added, that the presentation concerned the newest version of the system with a fully compo - site airframe, an improved launcher, a system of airfra- me stabilization, and payloads with thermal imaging cameras. UAV & UGV