A system for creating thrust for flying machines with Vertical Take Off and Landing (VTOL) including a first propulsion unit, a second propulsion unit, a top winget, a bottom winget, two or more tracks running over said first and second propulsion units, and wherein the two or more tracks are configured to mount said top and bottom wingets.
System for Horizontal Take-off and Landing
2023-08-10
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Reusable horizontal take-off and landing two-stage aerospace vehicle
European Patent Office | 2024
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