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 TERMINÉ 

Aero-Thermodynamic Loads on Lightweight Advanced Structures II (ATLLAS II)

Date du début: 1 mai 2011, Date de fin: 31 oct. 2015,

ATLLAS II is a logical follow-up of a recently finalized FP6 project which has as objectives the identification and assessment of advanced light-weight and high-temperature resistant materials for high-speed vehicles up to Mach 6.The material requirements are first defined through an in-depth feasibility study of a Mach 5-6 vehicle. The consortium has now this capability at hand as they can rely o ...
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 16

 TERMINÉ 

Engine Representative Internal Cooling Knowledge and Applications (ERICKA)

Date du début: 1 juil. 2009, Date de fin: 30 juin 2014,

"The goal of ERICKA is to directly contribute to reductions in aircraft engine fuel consumption with a targeted contribution of 1% reduction in SFC relative to engines currently in service. The fuel efficiency of a jet engine used for aircraft propulsion is dependent on the performance of many key engine components. One of the most important is the turbine whose efficiency has a large influence ...
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 20

 TERMINÉ 

Long-Term Advanced Propulsion Concepts and Technologies II (LAPCAT-II)

Date du début: 1 oct. 2008, Date de fin: 31 déc. 2013,

"Lacpat II is a logical follow-up of the previous EC-project which has as objective to reduce antipodal flights to less than 2 to 4 hours. Among the several studied vehicles, only two novel aircraft for a Mach 5 and 8 flight are retained in the present proposal. Starting from the available Mach 5 vehicle and its related precooled turboramjet, assumed performance figures of different components ...
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 16