elsbro13002-bram-A301_a Take full control of the sky. bramor-i UNMANNED AERIAL Developed in Italy by Eurolink Systems srl - via Piedicavallo, 51 - 2/B - 00166 Roma (ITALY) - Tel. +39.06.619140.1 Mail: [email protected] - www.eurolinksystems.com Developed in Italy by VEHICLE TECHNICAL SPECIFICATIONS WINGSPAN LENGHT AIRCRAFT TYPE & AIRFRAME AVIONICS PROPULSION MTOW bramor-i UNMANNED AERIAL PAYLOAD VEHICLE CRUISE SPEED Vne TAKE OFF SYSTEM LANDING AREA The BRAMOR-I airframe is manufactured from an advanced composite mix of Kevlar/Carbon/Vectran and when appropriate provides low radar detection probability and a high level of survivability. An ADS-B transponder can be fitted into the airframe for airspace integration purposes. The sensor modularity [classical EO/IR interchangeable gimbaled turret, fixed visible light and IR spectra orthophotography, hyperspectral imaging, advanced environmental monitoring sensors] is ensured by the modular construction of the airframe, which allows for multiple payload configurations and endurance/range options, including an on board video and data recorder. The BRAMOR-I UAV is based on a blended wing body modular airframe, with the emphasis on the smallest possible T/O weight, advanced aerodynamics, electric propulsion, endurance, ergonomic and user friendly ground control station, durability and mobility. The system consists of the air vehicle with the chosen sensor configuration middle section, a foldable take off low temperatures pneumatic or above 0 deg celsius temperature range elastic catapult, a communications package tripod with antennae and the optional ASTRALTRACK tracking antenna system and the ground control station (GCS). The whole system fits into a MILSPEC, rain resistant backpack with the GCS embedded in an industry standard rugged package and is flight ready in less than five minutes. The system can be safely operated by one operator/pilot in command, but a crew of two is desirable for situational awareness purposes. LANDING Ground Station SERVICE CEILING OPERATIONAL TEMPERATURES VIDEO & DATALINK RANGE ENDURANCE T/O READINESS Launcher 96 cm fixed wing, blended wing body configuration, kevlar reinforced carbon composite airframe Lockheed Martin (ITAR controlled) and C-ASTRAL ORTHOelectronics brushless electric 4,2 kg 0,6 - 1,0 kg 58 km/h 105 km/h ELASTIC CATAPULT / PNEUMATIC CATAPULT 10 m x 10 m PARACHUTE or BELLY LANDING up to 4300 m AMSL -40°C - 80°C Up to 30 km LOS with ASTRALTRACK tracking antenna 180 min with rechargeable batteries, enhaceable with one-time power sources System T/O ready in less than 5 minutes OPTIONS many possibilities ( based on user’s needs ) TRANSPORT 1 MILSPEC backpack and/or rugged case OPERATION REQ FLYING GIMBAL CONTROL ORTOPHOTO CONTROL MANUAL FLIGHT CONTROL GCS ENDURANCE Eye gimbal 230 cm EMERGENCY FAILSAFES RUGGEDIZZATION one or two operators 100% autonomous from takeoff to landing flight stick control 100% autonomous, multiple ortophoto mission geometries possible in 1 flight, reprogrammable on the fly while vehicle in the air optional light stick up to 10 h yes, user configured IP66 compliant Developed in Italy by