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Long Endurance Heavy Load and Low Speed Target Drone B-50

SKU: MD-P00521·UAV Platforms·Auf Bestellung

Long Endurance Heavy Load and Low Speed Target Drone B-50
Long Endurance Heavy Load and Low Speed Target Drone B-50

Übersicht

The B-50 long endurance heavy load and low speed target drone adopts a conventional aerodynamic layout, is powered by a small piston engine, and is made of all-composite materials. The aircraft is equipped with an all-digital flight control system, a GPS navigation system and an integrated measurement and control system, enabling full autonomous flight. By carrying mission equipment such as radar reflector enhancers and infrared sources, the main technical characteristics of various air raid weapons can be simulated. The aircraft is mainly used for military aviation as a low and slow simulation target in the air, and can also be used to support training and live ammunition of air defense forces of land, sea and air force. Maximum flight speed: 55 m/s Flight altitude: 50~5500m Maximum take-off weight: 115Kg Take-off method: rocket-assisted launch or catapult launch Recovery method: Parachute Control and guidance methods: remote control, program control, full autonomous flight

Technische Daten

Specifications. Wichtige technische Daten: Maximum flight speed 55 m/s, Flight altitude 50~5500m, Cruising speed 40 m/s, Endurance time 1.5h, Maximum take-off weight 115Kg, Maximum load 25Kg, Captain 4.5m, Wingspan 6.2m, Control distance 100Km, Wind Resistance Class 6, Take-off method rocket-assisted launch or catapult launch, Recovery method Parachute, Control and guidance methods remote control, program control, full autonomous flight.

Technische Daten — 1 groups
Wichtige technische Daten: Maximum flight speed 55 m/s, Flight altitude 50~5500m, Cruising speed 40 m/s, Endurance time 1.5h, Maximum take-off weight 115Kg, Maximum load 25Kg, Captain 4.5m, Wingspan 6.2m, Control distance 100Km, Wind Resistance Class 6, Take-off method rocket-assisted launch or catapult launch, Recovery method Parachute, Control and guidance methods remote control, program control, full autonomous flight.

Technische Daten

Specifications

Maximum flight speed
55 m/s
Flight altitude
50~5500m
Cruising speed
40 m/s
Endurance time
1.5h
Maximum take-off weight
115Kg
Maximum load
25Kg
Captain
4.5m
Wingspan
6.2m
Control distance
100Km
Wind Resistance
Class 6
Take-off method
rocket-assisted launch or catapult launch
Recovery method
Parachute
Control and guidance methods
remote control, program control, full autonomous flight

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