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NGD-HAWK-68 MILITARY LOITERING UAV
Key Features Reliable Day and Night Operation Autonomous precision strike with minimum collateral damage Tracking Moving Targets (optional) High Performance Navigation, Flight Control and Guidance Algorithms Deployable and Operable by Single Soldier In-Flight Mission Abort and Emergency Self-Destruction Modes (optional – within Data Link range and Autonomous) Indigenous Electronic Ammunition Safety, Setup and Trigger Systems Indigenous Propriety Embedded Hardware and Software Wide Lateral View Angle Image Processing-Based Control Applications ((optional) Embedded and Real-Time Object Tracking, Detection and Classification (optional)
NGD-HAWK-68 MILITARY LOITERING UAV
Summary of the system key features will be as follows:
- The entire system is completely designed by AD original design and production.
- 180 minutes airtime @cruise speed
- Cruise speed 40 m/sec
- Maximum speed 65 m/sec
- 12,000+ ft service ceiling
- 48 kg maximum take-off weight (inc. 18 kg payload)
- 30+ km range data + video link (optionally 100 Km)
- Take-off with “Pneumatic/Sling” launcher
- Take-off and control from moving ground or naval ship platforms.
- Fuselage and Structure produced with advanced composite technologies.
- Will be Compliant with MIL-STD-810F and MIL-STD-461 military standards.
- Fully autonomous flight and navigation with Ground Control Station (GCS), including takeoff and landing.
- Pre-programmed mission point definitions up to 255 mission points, ability to change during flight.
- Fleet (SWARM) Flight capability (up to 32 units)
- Mission Abort and landing on land or sea with parachute (optional)
- Automatic landing by arriving at a predetermined return home point with Return to Home and Emergency
Landing Modes
- Mission planning and control Portable Ground Control Station
- Real-time encrypted digital flight data recording and playback of rangefinders
NGD-HAWK-68 MILITARY LOITERING UAV
PAYLOAD SYSTEM
• 18kg Standard payload types
• Fuse and Security systems:
- Secured Launch protection,
- Impact Fuse System,
- Proximity Fuse System,
- Arm / Disarm Control,
- Autonomous Flight Mode Control integration,
- Double verification of Altitude to be ARMED/DISARMED.
KEY COMPONENTS below ARE produced in TURKIYE
• 4 Cylinder COMBUSTION ENGINE
• FLIGHT CONTROLLER with heavy duty threshold sensors
• ANTI-JAMMING Antenna (if required)
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