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- Dual-purpose system for military and civilian use.
- Components include the HIRRUS unmanned aircraft, Ground Control Station (GCS), Data Link, and Launcher.
- Maximum Take Off Weight (MTOW): 7 kg
- Cruise Speed: 130 km/h
- Operating Range: 15 km (classical), 30 km (autopilot)
- Service Ceiling: 3000 m
- Propulsion: Electric engine
- Payload Weight: 0.7 kg
- Endurance: 180 minutes
- Launching System: Automatic catapult
- Recovery System: Parachute
- Retractable gyro-stabilized payload
- Portable GCS with user-friendly interface
- "Camera follow" navigation
- Flexible configuration for one or two propulsion engines
- Antenna tracking system and high-resolution imagery
- Carbon fiber and composite materials body
- GIS support and automatic navigation
- Extended operational range with multiple Ground Data Terminals
- Mission planning software
- Reconnaissance missions in disaster-affected areas
- Search and rescue operations
- Photography and cartography
- Monitoring borders and critical infrastructures
- Aircraft Wingspan: 2350 mm, Length: 1070 mm
- GCS Dimensions: 638 mm x 363 mm x 152 mm, Weight: 5.35 kg
- Launcher Dimensions: 3600 mm x 100 mm x 100 mm, Weight: 20 kg
- Includes Soim 1 and Soim 2 unmanned aircraft, Ground Control Station (GCS), and Data Link.
- Soim 1 MTOW: 25 kg, Maximum Speed: 230 km/h, Cruise Speed: 160 km/h, Operating Range: 32 km, Service Ceiling: 3000 m, Endurance: 1 hour, Payload: 5 kg
- Soim 2 MTOW: 140 kg, Maximum Speed: 280 km/h, Cruise Speed: 130 km/h, Operating Range: 100 km, Service Ceiling: 3000 m (6000 m optional), Endurance: 6 hours (10 hours optional), Payload: 50 kg
- Robust construction for vehicle-based transportation
- Portable GCS with user-friendly interface
- Day and night operation in difficult weather conditions
- Launching/landing on grass or dirt runways
- Safety system with parachute
- Rapid configuration as a target or target towing
- GIS support and automatic navigation
- Carbon fiber and composite materials parts
- Mission planning software
- Aerial targets system for military and special forces training
- Soim 1 Wingspan: 3.2 m, Length: 2.6 m
- Soim 2 Wingspan: 5.3 m, Length: 4.6 m
Catalog excerpts
Key features • Composite materials technology used in building Unmmaned Aerial Vehicule • Aerodynamic structures research & development • Software for management & flight control • Electronics related to monitoring, stability & control systems for UAV’s Components • Aerial target - rigid (towed) and unmmaned • Telemetry system • Stabilization system with Infrared detection • Stabilization system for longitudinal channel • Towing winch • GPS algorithm with improved positioning • Stabilization system with gyroscopes with Coriolis effect • Engine Management System • Auto tracking system for ground antennas ___L I i strategic partner TeamNet collaborate authonomous flight technology TeamNet International S.A. 319 Spl. Independentei, RIVER Place, RIVERVIEW House, 8 floor. District 6,060044 Bucharest Phone:+4 021 311 66 31 | Fax:+4 021 311 66 36 | E-mail: [email protected] | www.teamnet.ro
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strategic partner TeamNet G AFT AUTHONOMOUS FLIGHT TECHNOLOGY strategic partner TeamNet GAFT AUTHONOMOUS FLIGHT TECHNOLOGY TECHNICAL SPECIFICATIONS Maximum Take Off Weight (MTOW): Cruise speed: Operating range: Service ceiling: Propulsion: Payload weight: Endurance: Launching system: Recovery system: 7 kg; 130 km/h; 15 km in classical regime; 30 km in autopilot regime; 3000 m; electric engine; 0,7 kg; 180 minute; automatic catapult; parachute. Hirrus. Mini UAV system Hirrus is a compact system with double purposes, used both in military and civilian applications. Structure: - HIRRUS unmanned...
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Key features • Composite materials technology used in building Unmmaned Aerial Vehicule • Aerodynamic structures research & development • Software for management & flight control • Electronics related to monitoring, stability & control systems for UAV’s Components • Aerial target - rigid (towed) and unmmaned • Telemetry system • Stabilization system with Infrared detection • Stabilization system for longitudinal channel • Towing winch • GPS algorithm with improved positioning • Stabilization system with gyroscopes with Coriolis effect • Engine Management System • Auto tracking system for ground...
Open the catalog to page 3
TeamNet strategic partner TeamNet TeamNet collaborate strategic partner TeamNet ©AFT AUTHONOMOUS FLIGHT TECHNOLOGY FEATURES Maximum Take Off Weight (MTOW) Maximum speed Cruise speed Operating range Service ceiling Propulsion Endurance Safety system Payload optional STRUCTURE APPLICATION » Soim 1 unmanned aircraft; » Aerial targets system for » Soim 2 unmanned aircraft; » Ground Control Station (GCS); » Data Link. STRUCTURE » Robust construction for vehicle based transportation; » Operation based on a portable GCS equipped with a friendly man-machine interface; » Day and night operation...
Open the catalog to page 4All Autonomous Flight Technology catalogs and technical brochures
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