The Unmanned Little Bird H-6U is the unmanned variant of the AH-6i manned scout helicopter. Its unique design combines the autonomous flight capability, networked payloads and communications of an unmanned aerial vehicle with a combat-proven rotorcraft platform. The unmanned system provides over-the-horizon search, re-supply and retrograde, communications relay and surveillance capabilities. All with a low-risk approach, low operational costs and high flight readiness on a proven platform.
Quick Facts
Has 27.5-foot (8.38-meter) main rotor diameter with blade fold capability
Based on an FAA and military-qualified manned platform
Can demonstrate compliance to be under CAT I and II MTRC levels
Capable of flying missions autonomously from takeoff to landing with very high precision and accuracy
Features an open architecture design that allows U.S.-government-appr
oved design enhancements to be incorporated easily
Leverages existing logistics, documentation and training of the manned helicopter platform
Technical Specifications
Rotor Diameter
27.5 ft (8.38 m)
Max Speed
145 KTAS
Ceiling
20,000 ft (6,100 m)
Empty weight
2,200 lbs (998 kg) manned, 1,900 lbs (862 kg) unmanned
Useful payload
1,200 lbs (544 kg) manned, 1,400 lbs (635 kg) unmanned
Command Link
Ku-band TCDL
Electrical Power
11kW @ 28VDC
Command and Control
STANAG 4586 Compliant
Endurance
About 6 hours
Mission Planning
Pre-launch and dynamic during mission
Autonomy
Waypoint control from take-off to landing
Navigation
Fixed (land-based) or relative (sea-based)
The Unmanned Little Bird H-6U is the unmanned variant of the AH-6i manned scout helicopter. Its unique design combines the autonomous flight capability, networked payloads and communications of an unmanned aerial vehicle with a combat-proven rotorcraft platform. The unmanned system provides over-the-horizon search, re-supply and retrograde, communications relay and surveillance capabilities. All with a low-risk approach, low operational costs and high flight readiness on a proven platform.
Quick Facts
- Has 27.5-foot (8.38-meter) main rotor diameter with blade fold capability
- Based on an FAA and military-qualified manned platform
- Can demonstrate compliance to be under CAT I and II MTRC levels
- Capable of flying missions autonomously from takeoff to landing with very high precision and accuracy
- Features an open architecture design that allows U.S.-government-approved design enhancements to be incorporated easily
- Leverages existing logistics, documentation and training of the manned helicopter platform
Technical Specifications
Rotor Diameter | 27.5 ft (8.38 m) |
Max Speed | 145 KTAS |
Ceiling | 20,000 ft (6,100 m) |
Empty weight | 2,200 lbs (998 kg) manned, 1,900 lbs (862 kg) unmanned |
Useful payload | 1,200 lbs (544 kg) manned, 1,400 lbs (635 kg) unmanned |
Command Link | Ku-band TCDL |
Electrical Power | 11kW @ 28VDC |
Command and Control | STANAG 4586 Compliant |
Endurance | About 6 hours |
Mission Planning | Pre-launch and dynamic during mission |
Autonomy | Waypoint control from take-off to landing |
Navigation | Fixed (land-based) or relative (sea-based) |