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【2/1～利用可先着順クーポン配付中】【2/5に発送予定※早まる場合有り】エクエルパウチ 120粒 × 3袋【正規販売店】大塚製薬 3個セット [大塚製薬エクエルパウチ 120 3個…

80s Grocery Store: The Detergent Aisle

Wisk will start testing of electric vertical take-off and landing aircraft in New Zealand FlyDragon FDG-25 electric VTOL long endurance drone 3 hours VTOL V tail for mapping surveillance FlyDragon FDG-25 electric vertical take-off and landing fixed wing, wingspan 2.5 meters,it iss electric version . This model combines the characteristics of long-endurance, high-speed and long-distance of fixed-wing UAVs and the vertical take-off and landing of rotor-wing drones. It does not require runway but only small space for take-off and landing, and can be operated smoothly on ship deck, narrow airspace, mountain, complex terrain and densely populated areas such as hills, jungles. The whole process of autonomous flight can be completed without operator intervention for cruise, flight state transition and vertical take-off and landing. The equipment compartment is a replaceable hatch cover, and different mounting hole positions can be designed for different load requirements of the user. The fuselage is designed as quick release structure, with reliable electrical connection, plug and play; unfolding and withdrawal time is less than 10 minutes. The engine is rear-mounted and the load is placed forward to provide a larger field of view for the photoelectric load without obstruction. Feature: Easy to assemble and operate Vertical take-off and landing, without limitation of space Resistance to harsh weather conditions Diesel-electric version and electric version optional All carbon fiber composite material, industry standard architecture Compatible with PC station, suitable for open source of autopilot system. 1. Body material: carbon fiber, glass fiber, Kevlar, pvc interlayer, etc. 2. Body length: 1.26m 3. Wingspan: 2.5m 4. Landing gear height: 19.5cm 5. Landing gear installation position: below the rotor rod 6. Task compartment size: 260mm*172mm*90mm 7. Battery compartment size: 260mm*150mm*85mm (can hold 2*5300mah and 1*32000mah at the same time) 8. Position of mission compartment: directly below the center of gravity of the aircraft 9. Structure weight: about 3.2kg 10. Maximum take-off weight: less than 13kg 11. Maximum payload: 2kg (standard load: 1-1.5kg) 12. Endurance time: 170min/1.5kg (standard power configuration) (fixed wing power can be equipped with 18650 batteries to increase endurance time) 13. Maximum control distance: manual control by remote control/1km, ground station/standard 30km 14. Standard cruising speed: 65km/h (about 18m/s) 15. Maximum cruising speed: 108km/h (30m/s) 16. Stall speed: 16m/s 17. Minimum circling radius: 150m 18. Maximum level flight limit: 4000m above sea level 19. Wind resistance of fixed-wing mode: no less than 7 wind (17.1m/s) 20. Maximum wind resistance in rotor take-off and landing mode: no less than class 4 wind (7.9m/s) 21. Operating environment: -20℃~45℃; can fly in light rain 22. Power battery: 2*5300mah (vertical take-off and landing) 2*25000mah (fixed wing cruise) 23. Rotor emergency operation time: not less than 6.5min 24. Take-off and landing method: vertical take-off and landing 25. Vertical power blade size: 16 inches (recommended) 26. Fixed wing tail thruster blade: 14~16 inches (recommended) long endurance drone 3 hours VTOL V tail for mapping surveillance FlyDragon FDG-25 electric vertical take-off and landing fixed wing, wingspan 2.5 meters,it iss electric version . This model combines the characteristics of long-endurance, high-speed and long-distance of fixed-wing UAVs and the vertical take-off and landing of rotor-wing drones. It does not require runway but only small space for take-off and landing, and can be operated smoothly on ship deck, narrow airspace, mountain, complex terrain and densely populated areas such as hills, jungles. The whole process of autonomous flight can be completed without operator intervention for cruise, flight state transition and vertical take-off and landing. The equipment compartment is a replaceable hatch cover, and different mounting hole positions can be designed for different load requirements of the user. The fuselage is designed as quick release structure, with reliable electrical connection, plug and play; unfolding and withdrawal time is less than 10 minutes. The engine is rear-mounted and the load is placed forward to provide a larger field of view for the photoelectric load without obstruction. Feature: Easy to assemble and operate Vertical take-off and landing, without limitation of space Resistance to harsh weather conditions Diesel-electric version and electric version optional All carbon fiber composite material, industry standard architecture Compatible with PC station, suitable for open source of autopilot system. 1. Body material: carbon fiber, glass fiber, Kevlar, pvc interlayer, etc. 2. Body length: 1.26m 3. Wingspan: 2.5m 4. Landing gear height: 19.5cm 5. Landing gear installation position: below the rotor rod 6. Task compartment size: 260mm*172mm*90mm 7. Battery compartment size: 260mm*150mm*85mm (can hold 2*5300mah and 1*32000mah at the same time) 8. Position of mission compartment: directly below the center of gravity of the aircraft 9. Structure weight: about 3.2kg 10. Maximum take-off weight: less than 13kg 11. Maximum payload: 2kg (standard load: 1-1.5kg) 12. Endurance time: 170min/1.5kg (standard power configuration) (fixed wing power can be equipped with 18650 batteries to increase endurance time) 13. Maximum control distance: manual control by remote control/1km, ground station/standard 30km 14. Standard cruising speed: 65km/h (about 18m/s) 15. Maximum cruising speed: 108km/h (30m/s) 16. Stall speed: 16m/s 17. Minimum circling radius: 150m 18. Maximum level flight limit: 4000m above sea level 19. Wind resistance of fixed-wing mode: no less than 7 wind (17.1m/s) 20. Maximum wind resistance in rotor take-off and landing mode: no less than class 4 wind (7.9m/s) 21. Operating environment: -20℃~45℃; can fly in light rain 22. Power battery: 2*5300mah (vertical take-off and landing) 2*25000mah (fixed wing cruise) 23. Rotor emergency operation time: not less than 6.5min 24. Take-off and landing method: vertical take-off and landing 25. Vertical power blade size: 16 inches (recommended) 26. Fixed wing tail thruster blade: 14~16 inches (recommended) RELATED NEWSCATEGORIESLATEST NEWSCONTACT US