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SAT HS-150 two-seat gyrocopter with an open cockpit on a runwaySAT HS-150 two-seat gyrocopter with an open cockpit on a runway

SAT 2 Seat Gyrocopter

The SAT HS-150 2 Seat Gyrocopter is an open-cockpit aircraft with switchable manned and unmanned configurations. Built with three-point landing gear and supplied with an ejection parachute, it supports agricultural spraying, patrol, search and rescue, surveying and aerial photography, with task-specific equipment options.

SATAgricultural drone

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Product overview

The SAT HS-150 2 Seat Gyrocopter combines an open cockpit with three-point landing gear and an included ejection parachute. Its rotor has no periodic pitch changes, and the aircraft has no main rotor power drive system. The gyrocopter measures 5.1m in overall length and 2.81m in height, with seating for two. Switchable manned and unmanned configurations support different operational roles, while photoelectric, radar, relay, remote control and telemetry link equipment can be fitted according to the task.

Applications include agricultural spraying, forest fire protection, police patrol, anti-terrorism, field search and rescue, infrastructure patrol, disaster survey, aerial photography, aerial survey and air travel. The HS-150 has a cruising speed of 100-150km/h, a maximum flight speed of 172km/h and a minimum flight speed of 50km/h. Flight distance is 500km and the ceiling is 3000m. Takeoff ground distance is ≤90m and landing ground distance is ≤30m. Climb rate is 4.5m/s with one person and 3.2m/s with two people.

AgricultureSurveying & inspectionFire & rescue

Specifications

SAT 2 Seat Gyrocopter specifications
SpecificationValue & conditions
Product identitySAT HS-150 2 Seat Gyrocopter with an open cockpit
Whole length5.1m
Height2.81m
Maximum flight speed172km/h
Ceiling3000m
Minimum flight speed50km/h
Seats2
Takeoff ground distance≤90m
Landing ground distance≤30m
Fuel tank68L@95#
Flight distance500km
Cruising speed100-150km/h
Climb rate with one person4.5m/sOne person.
Climb rate with two people3.2m/sTwo people.
Included emergency equipmentEjection parachute
Landing gearThree-point landing gear
Rotor constructionRotor without periodic pitch changes; no main rotor power drive system
Operating configurationsSwitchable manned and unmanned configurations
Optional mission equipmentPhotoelectric, radar, relay, remote control and telemetry link equipmentEquipment selected according to the task.
ApplicationsAgricultural spraying, forest fire protection, police patrol, anti-terrorism, field search and rescue, power line patrol, oil pipeline patrol, disaster survey, aerial photography, aerial survey and air travel