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CTLEThe future of f l ight
Low Purchase Price
Low Operating Costs
Useful Load - 600 lbs
BRS - Standard
Camera Gimbal Systems
Cloud Cap Technology
TASE 200, 300, 400
L-3 Wescam MX-10
FeaturesFull motion EO imager and 640 x 480 LWIR camera• Onboard GPS/INS• Common Control & Operator Interface across TASE family• Optional external VPS provides Target Tracking, Scene Steering and Electronic Image Stabilization. Other operation modes include Path Tracking and Geo Pointing• ViewPoint software with moving map, mosaicing, Path-Track, and video recording
High performance and low SWAP at 7.5 lbs• Full motion EO imager and continuous zoom MWIR camera• Flexible 3rd bay for additional payload options• Onboard image processing provides Target Tracking, Scene Steering and Electronic Image Stabilization. Other operation modes include Path Tracking and Geo Pointing• Common Control & Operator Interface across TASE family• Fiber Optic Gyros• ViewPoint software with moving map, mosaicing, Path-Track, video recording, etc.
Full motion EO imager and 640 x 480 LWIR camera• Onboard GPS/INS• Common Control & Operator Interface across TASE family• Optional external VPS provides Target Tracking, Scene Steering and Electronic Image Stabilization. Other operation modes include Path Tracking and Geo Pointing• ViewPoint software with moving map, mosaicing, Path-Track, and video recording
Cloud Cap Technology TASE stabilized cameras are available which meet many application needs in defense, security, automated inspection and spectroscopy
TASE200 TASE300 TASE400
CTLE Features / Capabilities / Equipment
The CTLE also has digital downlink capabilities using 3G and 4G systems that streams real-time images from the camera to a secure IP address. This allows command centers, the on-scene commander and field officers access to what the flight crew of the CTLE are seeing.
Key Features• Fast, comfortable, ideal flight characteristics• >90% carbon composite structure with some Aramid – high tech, strong, lightweight• 100 hp Rotax 912 ULS engine – auto fuel or 100LL avgas – 3 to 6 GPH• Typical Empty Weight 770 lbs. – large useful load • “Safety Cell” energy absorbing cockpit design – increased safety margin• Roomy cabin – accommodates large, fully-equipped crew• Gullwing doors – easy entry/exit• Strutless, cantilevered wing – unobstructed horizontal & vertical view• Airframe parachute recovery system & 4-point harness restraints
Engines100–hp Rotax 912S with slipper clutch and 2.000hrs. TBOFuel: Premium unleaded auto fuel or 100 LL Avgas
100–hp Rotax 912iS with electric fuel injection and 2.000hrs. TBO Slipper clutchFuel: Premium unleaded auto fuel or 100 LL Avgas
SystemsElectronic flap control with pre-selection switchDual controls, conventional, three axisThree axis trim available, combination key switchOptimized fuel system with 2 wing tanks 17 Gal each = 34 Gal total fuelBRS airframe parachute recovery system standard
ExteriorHigh quality polyurethane exterior finishRugged composite landing gear with superior damping abilityHydraulic disc brakes – Optional Tundra tiresSteerable nose wheel110 lbs luggage capacity – 55 lbs each side plus storage shelf
InteriorLarge window area provides excellent visibilityAttractive and durable two-tone interiorSpacious cabin comfortable for large and tall occupantsLarge gullwing doors for easy entry/exitAdjustable seats with 4-point restraint harnesses“Safety Cell” composite cockpit design
Aircraft Specifications
Garmin G3X Panel
Dynon SkyView Panel CTLE
The future of f l ight
This information is for marketing purposes only. It is representative of the aircraft when published and may be changed by Flight Design at any time without notice.
Performance at MTOW 1320 lb/600 kgVh: maximum horizontal speed 120* kt 222 km/hVne: maximum permissible airspeed (red line) 162 kt 300** km/hTake-off run (flap +15 degree) 820 ft 250 mTake-off distance over 50 ft obstacle 1476 ft 450 mMax. range (30 min reserve) 974 NM 1800 km
* ASTM LSA certification** The never-exceed speed (Vne) limit is defined by the capabilities of the airframe parachute systemWeights, Dimensions and CapacitiesTypical Empty Weight, well-equipped including Airframe Parachute Recovery System (APRS)
720 lb 326 kg
Max. take off weight 1320 lb 600 kgFuel capacity 34 US Gal 130 lMaximum weight per seat 265 lb 120 kg110 lbs max (55 lbs max each side) 110 lb 50 kg
Flight Design GmbHSielminger Str. 51D-70771 L.-EchterdingenGERMANYemail: [email protected]: www.flightdesign.com
Flight Design USAP.O. Box 325South Woodstock, CT 06267USAemail: [email protected]: www.flightdesignusa.com
