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SAT 200kg Tandem Rotor Helicopter with a gray fuselage and blue landing skids on grassSAT 200kg Tandem Rotor Helicopter with a gray fuselage and blue landing skids on grass

SAT 200kg Tandem Rotor Helicopter

The SAT 200kg Tandem Rotor Helicopter is an unmanned helicopter for long-distance transportation, rescue and surveillance. Its carbon fiber and aluminum alloy body houses a tandem rotor platform with vertical take-off and landing capability. Mission configurations accommodate radar, pods and sensors, with an optional photoelectric pod for imaging and laser ranging.

SATInspection drone
Endurance
1h@200 kg payload
Maximum speed
≥150 km/h
Size
3.9m×1.1×1.65m
Body material
Carbon fiber + aluminum alloy

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Product overview

The SAT 200kg Tandem Rotor Helicopter combines multiple rotors connected in series with a carbon fiber and aluminum alloy body. Designed around customer mission requirements, it supports logistics, heavy-object handling, rescue and surveillance. Vertical take-off and landing removes the need for long runways or complicated take-off and landing facilities, supporting deployment in cities, alpine areas and temporary work sites. The helicopter measures 3.9m×1.1×1.65m, has a maximum take-off weight of 600kg and weighs 380kg without payload.

A 160L maximum fuel tank capacity supports endurance of ≥4hrs with a 50kg payload or 1h with a 200kg payload. With a 120kg commercial payload, cruising speed is 110-130km/h. Navigation combines GPS+BDS+GLONASS+GEO, while optional line-of-sight control radii are 50km, 100km, 150km and 200km. Mission payloads include radar, pods and sensors. An optional photoelectric pod provides 30× zoom, 640×512 thermal resolution and a 3km laser rangefinder. SAT can customize the design and configuration to suit mission requirements.

Surveying & inspectionCargo & deliveryFire & rescueOEM & customization

Specifications

SAT 200kg Tandem Rotor Helicopter specifications
SpecificationValue & conditions
ProductSAT 200kg Tandem Rotor Helicopter; unmanned helicopter with multiple rotors connected in series.
ApplicationsLong-distance transportation, rescue and surveillance.
Take-off and landingVertical take-off and landing; no long runways or complicated take-off and landing facilities required.
Size3.9m×1.1×1.65m
Body materialCarbon fiber + aluminum alloy
Maximum take-off weight600kg
UAV mass380kgWithout payload.
Container weight±10kg3kg/25kg drop container.
Maximum fuel tank capacity160L
Maximum speed≥150km/h
Maximum flight altitudeASL ≥4500mAbove sea level.
Endurance1h@200kg payload200kg payload.
Endurance≥4hrs @50kg payload50kg payload.
Cruising speed110-130km/h120kg commercial payload.
Control radiusLOS: 50km/100km/150km/200km, OptionalOptional line-of-sight configurations.
Maximum flight time±8hrs @ 50-1000m ASLWithout payload; 50-1000m ASL.
Maximum flight time±3hrs @ 3000-4200m ASL120kg payload; 3000-4200m ASL.
Maximum flight distance≥700km@ 50-1000m ASLWithout payload; 50-1000m ASL.
Maximum flight distance≥250km@ 3000-4200m ASL120kg payload; 3000-4200m ASL.
Maximum climbing rate4m/sWith full tank only; ISA.
Maximum descent rate6m/s
U-turn radius100m15m/s speed; 120kg payload.
Control distance≥200km
Photoelectric pod30× zoom; 640×512 thermal resolution; 3km laser rangefinder; optional.Optional photoelectric pod.
Fuel consumptionTake-off & hover: ±30L/h, Cruise: ±20L/hTake-off and hover; cruise.
Navigation systemGPS+BDS+GLONASS+GEO
Task payloadRadar, pod, sensors, etc.
StandardMeets US standard: R grade of DO-160.