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 |
|||
Company Insights:
Resources:
- Website: Leap
Recent Pages
- Kitty Hawk Heaviside 2 (H2)
- AstroX Racer
- Highgate AeroDesign Targa VTOL
- TechXGeek Marie
- University of Illinois Illini Air Shuttle
- SASTRA University Mistral (concept design)
- Delft University of Technology Wigeon (concept design)
- DARPA Ancillary Tactical Drone (proposer)
- Alwinart (Sagstuen) Tesla eVTOL Concept
- AeroMech Incorporated AM-20 (research eVTOL)
