High Wind Resistance Tandem Helicopter with 200kg High Altitude Payload

• Customization: Available
• Certification: Industry Standard
• Height: High Altitude
• Model NO.: HF101K
• Operating Radius: Medium Range
• Size: Large
• Usage: Industrial
• Structure: Unmanned Helicopter
• Maximum Take-off Weight: 260kg
• Control Distance: 50-100km
• Duration of Flight: 2-4 Hours
• Ceiling Altitude: 6500m
• Maximum Flying Speed: 160km/H
• Aircraft Size: 400*130*190 Cm
• Classification of Wind Resistance: Level 7
• Transport Package: Aviation Box Packaging
• Specification: HF101K
• Trademark: HFHW
• Origin: China
• Production Capacity: 20

Product Description

 

Product Description

  HF101K Vertical double-paddle unmanned helicopter, adopts vertical dual-rotor structure, the body structure is increased to 4000x1300x1900mm, stronger wind resistance, the maximum take-off weight is increased to 650 Kg, and the rated mission load is 260 Kg.
The main advantage of the longitudinal double rotor configuration is that the longitudinal range of the center of gravity is large, so the fuselage mounting space is large, especially in the delivery of materials. Compared with other configurations of helicopters, there are usually strict requirements for cargo loading. After replacing the load, it is necessary to adjust the load position. Center of gravity deviation is a very dangerous factor for conventional configuration helicopters, which brings great trouble to users. The vertical dual rotor configuration helicopter has a wide center of gravity, and has a high adaptability to the changes of load position and load size. It does not need for users to accurately balance the center of gravity, which can save precious time in emergency rescue, material delivery and other scenarios, and greatly improve the rescue efficiency.

Product Parameters

  

classify	content	parameter	explain
helicopter platform	maximum take-off weight	650Kg
	actual load	<260 KG, <200 KG below 3000 m and below 4500 m	Includes fuel oil
	duration of flight	2-4 Hours	Maximum endurance of 10 hours
	ceiling altitude	At 6,500 meters above sea level
	maximum flying speed	160Km/h	Cruising at 140 Km / h
	aeroplane engine	141HP, and was water-cooled
	Rotary wing diameter	400 C M	Vertical double rotor
	classification of wind resistance	Adventitia level 7
	Aircraft size	400/130/190 CM	Long / wide / high
Ling Xiang OH Flight control system	control model	Remote control, command navigation, automatic navigation, automatic return, out of control protection
	Flight mode	Fixed point hover, fixed speed / fixed height cruise, coordinated turn, oblique climb / hover climb, steady take-off / landing, automatic take-off / landing
	GPS / Beidou / Galileo	The RTK differential GPS
	positioning accuracy	Less than 10CM
	Control radius	≥50KM	Up to 200K M
	Control the ground station	Windows System, with electronic map, virtual instrument, comprehensive display, command panel, route setting, status monitoring and alarm functions.
Task load	Support integrated photoelectric pod, seawater sampler, loudspeaker, toss device, etc		The default load is a dual-light pod

Detailed Photos