CHRDI AV500W
In development by the Chinese Helicopter Research and Development Institute (CHRDI), the AV500W is an armed variant of the civilian AV500 unmanned aircraft (UAV). Maximum payload is 160 kg (352.74 lbs). The aircraft can be equipped with an EO/IR sensor and target detection and tracking.
Overview
Data on design, manufacture and statusDesign authority: Chinese Helicopter Research & Development Institute
Primary manufacturer: Chinese Helicopter Research & Development Institute
Parent type: No type defined
Aircraft status: In development
Configuration
Primary flight and mechanical characteristicsVTOL type: Helicopter
Lift configuration: Single main rotor
Dedicated control device: Tail rotor
Crew required: 0
Crew seating: Not applicable
Landing gear: Skids
Layout and Dimensions
Data on aircraft size| Overall Dimensions | ||
|---|---|---|
| Overall Height: | ||
| Overall Length: | ||
| Overall Width: | ||
| Airframe Dimensions | ||
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| Airframe Length: | ||
| Airframe Width: | ||
| Airframe Height: | ||
| Landing Gear Dimensions | ||
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| Landing Gear Base: | ||
| Landing Gear Track: | ||
| Cabin Dimensions | ||
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| Cabin Internal Height: | ||
| Cabin Internal Length: | ||
| Cabin Internal Width: | ||
Weights and Performance
Data on aircraft weight and flight characteristicsCruise Speed: 170 km/h Max Endurance (fully outfitted): 4 h; Operating Radius: 200 km
| Weights | ||
|---|---|---|
| Max Gross Weight (ground): | 470 kg | 1,036 lb |
| Max Gross Weight (airborne): | ||
| Max Take-off Weight: | 470 kg | 1,036 lb |
| Empty Weight: | ||
| Useful Load: | ||
| Empty Weight Fraction: | ||
| Climb Performance | ||
|---|---|---|
| Max Rate of Climb: | ||
| Hover Performance | ||
|---|---|---|
| Hover Ceiling IGE: | ||
| Hover Ceiling OGE: | ||
| Limitations | ||
|---|---|---|
| Max Level Flight Speed: | ||
| Never Exceed Speed: | ||
| Service Ceiling: | 4,000 m | 13,123 ft |
| Range and Endurance | ||
|---|---|---|
| Max Range: | ||
| Max Endurance: | 8 hrs | 8 hrs |
Engine Details
Aircraft powerplant (lift and/or propulsion)Provided powerplant data is for uninstalled, sea level, static operations.
| Powerplant | ||
|---|---|---|
| Number of engines: | 1 | |
| Normal Ratings | ||
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| Max continuous: | ||
| Take-off / rated: | ||
| Intermediate: | ||
| Maximum: | ||
| OEI Ratings | ||
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| OEI contingency: | ||
| OEI continuous: | ||
| OEI 30-second: | ||
| OEI intermediate: | ||
Primary Lift Device
Data on primary lift devices such as main rotors| Main Rotor Characteristics | ||
|---|---|---|
| Diameter: | ||
| RPM: | ||
| Direction of Rotation: | Unknown | |
| Hub Type: | ||
| Main Rotor Blade Characteristics | ||
|---|---|---|
| Blade Construction: | ||
| Blade Chord: | ||
| Blade Tip Geometry: | ||
| Blade Twist: | ||
| Number of Blades: | ||
| Main Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | ||
| Disc Loading: | ||
| Solidity: | ||
| Main Rotor Blade Derived Characteristics | ||
|---|---|---|
| Blade area per blade: | ||
| Tip Speed: | ||
Primary Control Device
Data on primary control devices such as tail rotors| Tail Rotor Characteristics | ||
|---|---|---|
| Diameter: | ||
| Configuration: | Unknown | |
| Direction of Rotation: | Unknown | |
| RPM: | ||
| Tail Rotor Blade Characteristics | ||
|---|---|---|
| Number of Blades: | ||
| Blade Construction: | N/A | |
| Blade Chord: | ||
| Blade Twist: | ||
| Tail Rotor Derived Characteristics | ||
|---|---|---|
| Disc Area: | ||
| Solidity: | ||
| Tail Rotor Blade Derived Characteristics | ||
|---|---|---|
| Tip Speed: | ||
| Blade Area (per blade): | ||
