The integration of turbo-ramjet engines for hypersonic transport vehicles operating in the Mach 0 to 6+ regime represents one of the most important development tasks. A survey over the variety of interacting problem areas and faculties, which have to be integrated to lead to an optimized propulsion/airframe system, is presented
Integration of Turbo-Ramjet Engines for Hypersonic Aircraft
1992
7 pages
Report
No indication
English
Spacecraft Trajectories & Flight Mechanics , Jet & Gas Turbine Engines , Aerodynamics , Engine airframe integration , Hypersonic aircraft , Propulsion system configurations , Turboramjet engines , Transport vehicles , Aerodynamic characteristics , Mach number , Systems integration , Foreign technology
Integration of Turbo-Expander and Turbo-Ramjet Engines in Hypersonic Vehicles (92-GT-204)
Online Contents | 1994
|Inegration of turbo-expander- and turbo-ramjet-engines in hypersonic vehicles
Tema Archive | 1992
|HYPERSONIC RAMJET ENGINES AND CORRESPONDING AIRCRAFT AND METHOD
European Patent Office | 2019
|Experimental Studies on Air Turbo Ramjet Engines for Hypersonic Flight Vehicles
British Library Conference Proceedings | 1997
|Experimental Studies on Air Turbo Ramjet Engines for Hypersonic Flight Vehicle (Part II)
British Library Conference Proceedings | 1999
|