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
2024-02-07
Patent
Electronic Resource
French
EADS envisage le transport hypersonique de 2050
Online Contents | 2011
TECHNOLOGIE - Hypersonique: coup double pour Hyshot
Online Contents | 2006
Hypersonique : la Darpa remet le couvert
Online Contents | 2012