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.
HYPERSONIC TRANSPORT SYSTEM
2025-03-06
Patent
Electronic Resource
English
Hypersonic transport propulsion
Online Contents | 1996
Hypersonic transport technology
NTRS | 1977
|A hypersonic executive transport
NTRS | 1989
|Propulsion for hypersonic transport aircraft.
NTRS | 1965
|Propulsion for Hypersonic Transport Aircraft
NTIS | 1964
|