STINGRAY VTOL HYBRID UAS

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STINGRAY VTOL

"STINGRAY VTOL HYBRID UAS"的最小数量是1.

Carbon Fiber Frame
Wingspan: 5680 mm
Empty Weight: 496 kg
Max Takeoff Weight: 2,250 lbs
Powerplant: 1 x Drake Engine
Fuel Cap: 35 gal
Maximum Speed: 145 mph
Range: 520 mi
Endurance: 4 hours
Service Ceiling: 11,000 ft
Payload: External Hard Point 150lbs per side

Characteristics

• Wingspan: 5680 mm / 18 ft 7.6 in
• Length: 5266.5 mm / 17 ft 3.3 in
• Height: 2337mm / 7 ft 8 in
• Empty Weight: 1,088 LBS / 496 Kg
• Max Takeoff Weight: 2,250 LBS / 1.157 Kg
• Powerplant: o 1 x Drake Engine (Diesel, JP-4) o 278 hp (207kW)
• Fuel Cap: 35 Gal / 132.5 L
• Maximum Speed: 145 mph
• Cruise Speed: 130 mph
• Range: 520 mi
• Endurance: 4 Hours
• Service Ceiling: 3353 m / 11,000 ft
• Payload: External Hard Point 150 LBS per side

Description

The Stingray is a vertical takeoff the aircraft VTOL it was designed for battlefield use, is a force multiplier, is designed to support ground troops. It has superior hover performance, It is field deployable is aircraft transportable to the battlefield, it can take off and land in extreme environments

  
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