Long Endurance Heavy Load and Low Speed Target Drone B-50
SKU: MD-P00521·UAV Platforms·Под заказ


Обзор
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
Технические характеристики
Specifications. Основные характеристики: 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.
Технические характеристики — 1 groups
Основные характеристики: 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.
Технические характеристики
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