Passenger transport system propelled by a space launcher, having a seat with variable inclination based on the load factor

An assembly comprising a space launcher and a vehicle installed on said space launcher, the vehicle comprising at least one seat intended to receive a passenger, said seat or each of said seats being movable in rotation about an axis perpendicular to the direction of movement of the vehicle and including:

• an acceleration sensor to measure the acceleration of each at least one seat,
• a passenger interface comprising a screen intended to display images to the passenger installed on said seat, the screen being coupled to the seat with which it is associated so as to remain in a fixed position relative to said seat, and
• a control unit which is connected to the acceleration sensor and to the associated seat, the control unit being configured, on the one hand, to calculate a load factor experienced by the passenger installed on the corresponding seat from the acceleration of said seat and, on the other hand, to monitor the rotation of said seat during the operation of the transport system in order to maintain the position of the seat fixed relative to the load factor experienced by the passenger throughout the flight,
• the screen being configured to cover the entire field of vision of the passenger installed on the seat.