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Hi-Lite Lynx-us

Lynx-us
Hi-Lite Aircraft LLC
Bannister, Michigan, USA
www.vtolcruze.com

The Hi-Lite Lynx-us was designed to fit the U.S. military's Future Vertical Lift needs, as its "Integrated Power Package" can be applied to all different models of the Lynx-us platform. The Lynx-us can be scaled up or down, depending on if the needs are civilian, emergency, or military. In 2018, Hi-Lite submitted patents for the Leading Edge Articulating Propulsion (LEAP) and the Propulsor Thrust Ring (PTR).

Specifications:

Model Passengers Speed Range
Leap 1 pilot, 4 seats 280 kts

 

518.6 km/h

25-300 nm

 

46-556 km

Leap EMS 2 pilots, 2 stretchers 280 kts

 

518.6 km/h

25-300 nm

 

46-556 km

Patriot - 10 1 pilot, 12 seats 280 kts

 

518.6 km/h

300 nm

 

556 km

 

 

Patriot - 15
1 pilot, 16 seats 280 kts

 

518.6 km/h

300 nm

 

556 km


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