General: Flexible platform option for the LUNA TUAS.

MTOW: Max. 125 kg.

Abmessungen: Length: 3,2 m, Height 1,1 m, Wideth 0,9 m.

Antrieb: 30 KW Heavy-Fuel Turbo-shaft.

Rotor: 3-Bladesystem, Rotordiameter 350 cm.

Enrurance: ca. 3 hours.

Guidance:

Preprogrammed (3D waypoint list) using high resolution digital maps or high resolution aerial images; 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), option for automatic return flight to base.

Avionik:

Inertial Navigation System, autopilot and aircraft system management are fully digital. Sensor package includes attitude gyro, rate of turn sensors, magnetic compass, air data sensors and accelerometers.

Payloads: Cameras: Tiltable sensor platform with up to 7 color zoom and IR zoom video, -arrays, -turrets, -high-definition, -hyperspectral, forward looking pilot color video. Synthetic Aperture Radar (SAR), SIGINT-sensors, CBRN-sensors.

Optional payloads:

Data link relay payload for beyond line-of-sight reconnaissance and communication, Encryption, GCS hand off function.

Data link:

Microwave link (C-band), tracking antennas in air vehicle and ground station. Command uplink, control and video/telemetry in real-time, jamming resistant.

Data link Range: > 100 km.

Take off and landing: ATOL, vertical.

Ground Control Station:

Modular LUNA TUAS GCS design to fit in any vehicle or container. Advanced human-machine-interface (HMI).