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SU-H2M Chinese Unmanned Aerial Vehicle (UAV)

SU-H2M

Tactical Unmanned Aerial Vehicle (UAV)
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SU-H2M Chinese Unmanned Aerial Vehicle (UAV)
Other
SU-H2M Chinese UAV (A)TRADOC ODIN WEG
Basic Information
Name
SU-H2M Chinese Unmanned Aerial Vehicle (UAV)
Designation
SU-H2M
Alternate Designation
SU-H2M
Equipment Type
Tactical Unmanned Aerial Vehicle (UAV)
Manufacturer
Sunic-Ocean System Tech
Date of Introduction
2017
Description

The SU-H2M Chinese Unmanned Aerial Vehicle (UAV) is capable of hovering and operating in wind speeds of up to 33 knots (61 km/h or 38 mph) and requires a take-off and landing area of 8×8 meters (26×26 feet). This UAV is particularly suited for maritime or naval applications. Its operational temperature range is from -20°C to +40°C. The SU-H2M features a faceted fuselage that houses the UAV's powerplant, ventral payload bay, avionics, and fuel tank. It is equipped with a twin skid undercarriage with wheels located at the front. The design includes a two-bladed main rotor with an opposing balancing surface, as well as a tailboom that ends with dorsal and ventral stabilizing fins and a two-bladed tail rotor mounted on the starboard side. The main rotor is constructed from carbon fiber composite material, while the tail rotor is made from aluminum alloy. Additionally, a water tank is positioned towards the forward section of the fuselage.

Air & Air Defense Specifications
Engine Four-stroke, rotary engine
Cruise Speed 32.0 km/h
Range 54.0 km
Endurance 3.00 hrs
Service Ceiling 3000 m
Rotor Diameter 3.20 m
Payload Capacity 35 kg
System
Alternate Designation SU-H2M
Type Unmanned Aerial Vehicle (UAV)
Manufacturer Sunic-Ocean System Tech
Payload Capacity 35 kg (77 lb) [without reserve tank]
Mission Payloads SU-H2M payload comprises an electro-optic (EO) imaging sensor and multispectral camera mounted in a ventral payload bay.
Guidance and Control SU-H2M guidance and control features include automatic take-off and landing, an automatic hover mode, and semi-autonomous route planning using user-defined waypoints. The controller of the UAV can be eight channels and above. The GPS is attached dorsally at the mid-section of tailboom. The controller receiver has a nine-channel 2.4 GHz frequency hopping mode at 0.4 W within 200 m. It additionally uses a GY520 gyroscope.
Launch Vertical take-off and landing (VTOL) requiring an area of 8×8 m.
Recovery VTOL requiring an area of 8×8 m with parachute emergency fault safety system provision to arrest the UAV's descent in the case of a catastrophic loss of control and/or propulsion.
Dimensions
Length 3.81 m
Height 1.01 m
Width 0.72 m
Rotor Diameter 3.2 m
Tail Rotor Diameter 0.56 m
Empty Weight 65 kg (143 lb)
Maximum Takeoff Weight 110 kg (242 lb), including a 10-liter (2.2 US gallons/2.6 Imp gallons) fuel load and a 35 kg (77 lb) payload.
Automotive
Engine Name INA
Engine Type Four-stroke, rotary engine
Engine Power INA
Maximum Speed INA
Cruise Speed 32 kt (60 km/h; 37 mph)
Maximum Range 54 n miles (100 km; 62 miles) [maximum LOS radio communication at above 1,000 m altitude]
Radius of Operation 27 n miles (50 km; 31 miles) [maximum video range at 400 m altitude]
Service Ceiling 3,000 m
Endurance 3 h [typical, 20-liter (5.3 US gallons/4.4 Imp gallons) fuel load]
Image Sources
Notes https://www.uasvision.com/2017/10/31/chinas-sunic-ocean-su-h2m-for-maritime-security/
Details
Country of Origin China
Category UAVs
Air > UAVs
Filter Label
S
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
3.81 m
Width
0.72 m
Height
1.01 m
Weight
49.9 kg
Operators (1)
China
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