Abstract With the aim of placing Europe among the world's space players in the strategic area of atmospheric re-entry, several studies on experimental vehicle concepts and improvements of critical re-entry technologies have paved the way for the flight of an experimental space craft. The successful flight of the Intermediate eXperimental Vehicle (IXV), under ESA's Future Launchers Preparatory Programme (FLPP), is definitively a significant step forward from the Atmospheric Reentry Demonstrator flight (1998), establishing Europe as a key player in this field. The IXV project objectives were the design, development, manufacture and ground and flight verification of an autonomous European lifting and aerodynamically controlled reentry system, which is highly flexible and maneuverable. The paper presents, the role of aerodynamics aerothermodynamics as part of the key technologies for designing an atmospheric re-entry spacecraft and securing a successful flight.
Intermediate experimental vehicle, ESA program aerodynamics–aerothermodynamics key technologies for spacecraft design and successful flight
Acta Astronautica ; 124 ; 31-38
2016-04-02
8 pages
Article (Journal)
Electronic Resource
English
Space program , ESA , IXV , AED , ATD , Flight experiment , Reentry trajectory , AEDB , Aerodynamic Data Base , ATDB , AeroThermodynamic Data Base , IFE , In Flight Experiment , CFD , Computational Fluid Dynamic , FES , Flight Engineering System , WTT , Wind Tunnel Tests , TAS-I , Thales Alenia Space Italy , European Space Agency , FQA , Flying Quality Analysis , GNC , Guidance Navigation and Control , ETE , End to End , SWBLI , Shock Wave Boundary Layer Interaction , TPS , Thermal Protection System
ARV Reentry Module Aerodynamics and Aerothermodynamics
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