Embodiments of the invention relate to a hypersonic transport system including: an aircraft which includes a hypersonic lift-to-drag ratio greater than or equal to 2.5, wherein the aircraft includes a secondary propulsion device and position sensors, and wherein the aircraft also includes a variably shaped aerodynamic surface; a main propulsion device which is removably attached to the aircraft; and a control unit which is configured to monitor the aircraft and the main propulsion device.
SYSTEME DE TRANSPORT HYPERSONIQUE
HYPERSONIC TRANSPORT SYSTEM
HYPERSCHALLTRANSPORTSYSTEM
07.02.2024
Patent
Elektronische Ressource
Französisch
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