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Dimensions: |
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Wing span 4.17 m, length 2.36 m, height 0.87 m
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Weight: |
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Take-off weight < 40 kg
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Power Plant: |
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2-cylinder 2-stroke fuel injection engine, electrical power supply by battery backed generator
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Performance: |
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Typical reconnaissance air speed 70 km/h (37 KIAS). Certified to 3.500m ISA altitude
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Endurance: |
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exceeding 6 (optional 8) hours, dependent on payload and mission profile
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Guidance: |
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Preprogrammed (3D waypoint list) and/or remotely controlled. Mission program can be altered in flight. Differential GPS navigation and/or data link auto tracking (via range and azimuth data)
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Avionics: |
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Navigation, autopilot and aircraft system management are fully digital. Sensor package includes attitude gyro, rate of turn sensors, magnetic compass, air data sensors and accelerometers
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Reconnaissance Sensors: |
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one color video CCD camera for pilot view; one tiltable three-axis stabilized modular sensor platform, as standard platform with four downward looking color video (zoom) CCD cameras. The standard platform can be fitted with optional sensors
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Optional Sensors: |
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Medium wave thermal imager video camera, near-IR video (zoom) CCD cameras, monitor camera for wing ice build-up
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Data Link: |
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Two-way microwave link (C-band), tracking antennas in air vehicle and ground station. Command uplink, real-time video/flight and systems data downlink
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Data Link range: |
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exceeding 100 km (dependent on line of sight)
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Data Link Relay: |
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Modular payload for LUNA to extend reconnaissance beyond line of sight conditions
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Certifications for air vehicle and data link: |
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Military type certification category 2, (airworthiness certificate for flights over thinly populated areas)
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Ground control station: |
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Military operation certificate
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Launch: |
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Light-weight bungee catapult, foldable for transport
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Recovery: |
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Net landing with autonomous landing approach via differential GPS; or autonomous parachute landing |
