Technical Data

Dimensions:Wing span 5.3 m, length 3.0 m, height 1.1 m.
Weight:Take-off weight 110 kg.
Power Plant: 10 kw, multi-fuel injection engine.
Performance:Typical reconnaissance air speed 90 km/h. Max. > 5.000m ISA altitude.
Endurance:exceeding 12 hours, dependent on payload and mission profile.
Guidance: Preprogrammed (3D waypoint list) mission profile. Mission program can be altered in flight via data link. Differential GPS navigation and/or data link auto tracking (via range and azimuth data).
Avionics:Inertial navigation system (INS), autopilot and aircraft system management are fully digital. Sensor package includes attitude gyro, rate of turn sensors, magnetic compass, air data sensors and accelerometers.
Sensors: Cameras: Tiltable sensor platform with up to 7 color and IR zoom video, -arrays, -turrets, -high-definition, -hyperspectral, -pilot color video. Syntethic Aperture Radar (SAR; incl. GMTI), SIGINT-sensors, ESM, CBRN-sensors.ndard platform can be fitted with optional sensors.
Optional payloads:Data link relay for BLOS operations, encryption, GCS hand-off function, transponder.
Data Link:Two-way microwave link (C-band), tracking antennas in air vehicle and ground station. Command uplink, real-time video/flight and systems data downlink.
Data Link range:more than 100 km.
Data Link Relay:Modular payload for LUNA to extend reconnaissance beyond line of sight conditions.
Ground Control Station (GCS): Modular LUNA TUAS GCS design to fit many vehicle or container demands. Advanced Human-Machine- Interface (HMI).
Launch:Light-weight bungee catapult, foldable for transport.
Recovery:Net landing with automatic landing approach via differential GPS; or automatic parachute landing.
Luna NG Flugzeug