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Educational

Notes
High Speed Propulsion: Engine Design - Integration and Thermal Management

RTO-EN-AVT-185

The objective of the Lecture Series is to provide clear guidelines regarding the design of the propulsion unit and integration into the airframe. First the intake physics, design and optimization was addressed. Turbine based cycles and rocket based cycles was considered. An important issue discussed was the thermal management of both the engine and vehicle. Issues related to the potential use of new synthetic fuels were also addressed. The Lecture Series was a unique opportunity to bring together experts from different horizons and raise fruitful discussions.

Published9/16/2010
STOAuthorExternalMultiple
STOPublicationTypeEducational Notes RDP
Publication_ReferenceRTO-EN-AVT-185
DOI10.14339/RTO-EN-AVT-185
ISBNISBN 978-92-837-0138-5
STOPublisherRTO
AccessOpen Access
STOKeywordspropulsion; hypersonic; transport; intakes; thermal management

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$EN-AVT-185-COVER.pdf$EN-AVT-185-COVERCover Pages9/16/2010Open Access
$EN-AVT-185-ES.pdf$EN-AVT-185-ESExecutive Summary and Synthèse9/16/2010Open Access
$EN-AVT-185-PC.pdf$EN-AVT-185-PCProgramme Committee9/16/2010Open Access
$EN-AVT-185-Preface.pdf$EN-AVT-185-PrefacePreface9/16/2010Open Access
EN-AVT-185-01.pdfEN-AVT-185-01Engineering Engine/Airframe Integration for Fully Reusable Space Transportation Systems9/16/2010Open Access
EN-AVT-185-02.pdfEN-AVT-185-02The Mission Defines the Cycle: Turbojet, Turbofan and Variable Cycle Engines for High Speed Propulsion9/16/2010Open Access
EN-AVT-185-03.pdfEN-AVT-185-03Design Rules and Issues with Respect to Rocket Based Combined Cycles9/16/2010Open Access
EN-AVT-185-04.pdfEN-AVT-185-04Pulse Detonation Propulsion9/16/2010Open Access
EN-AVT-185-05.pdfEN-AVT-185-05Ramjet Intakes9/16/2010Open Access
EN-AVT-185-06.pdfEN-AVT-185-06Ramjets: Airframe Integration9/16/2010Open Access
EN-AVT-185-07.pdfEN-AVT-185-07Ramjets: Thermal Management – An Integrated Engineering Approach9/16/2010Open Access
EN-AVT-185-08.pdfEN-AVT-185-08Proof-of-Principle Experiment of a Shock-Induced Combustion Ramjet9/16/2010Open Access
EN-AVT-185-09.pdfEN-AVT-185-09Scramjet Inlets9/16/2010Open Access
EN-AVT-185-10.pdfEN-AVT-185-10Scramjet Isolators9/16/2010Open Access
EN-AVT-185-11.pdfEN-AVT-185-11Scramjet Combustion Processes9/16/2010Open Access
EN-AVT-185-12.pdfEN-AVT-185-12Scramjet Nozzles9/16/2010Open Access
EN-AVT-185-13.pdfEN-AVT-185-13Scramjet Thermal Management9/16/2010Open Access
EN-AVT-185-14.pdfEN-AVT-185-14Structural Design of Dual-Mode Ramjets and Associated System Issues9/16/2010Open Access
EN-AVT-185-15.pdfEN-AVT-185-15Hypersonic Technology Developments with EU Co-Funded Projects9/16/2010Open Access
EN-AVT-185-16.pdfEN-AVT-185-16The Engineering Design of Engine/Airframe Integration for the SÄNGER Fully Reusable Space Transportation System9/16/2010Open Access
EN-AVT-185-17.pdfEN-AVT-185-17French Flight Test Program LEA Status9/16/2010Open Access

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