A landing gear for a flight vehicle is used during landing. The landing gear for a flight vehicle includes a first cylinder structure configured to have an upper end which is coupled to be able to roll with respect to the flight vehicle; and a second cylinder structure configured to have a lower end which is able to come into contact with the ground, configured to be able to relatively move in an axial direction along a reference axis with respect to the first cylinder structure, and configured to be able to relatively rotate about the reference axis with respect to the first cylinder structure. The first cylinder structure and the second cylinder structure switch the landing gear between a stowed state and a released state by means of the relative movement and the relative rotation.
Landing gear for flight vehicle
2024-07-09
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
Landing of flight vehicles without the landing gear
Online Contents | 2014
|Landing of flight vehicles without the landing gear
Springer Verlag | 2014
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