The sharp edge flight experiment SHEFEX II, a mission overview and status

15th AIAA International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2008, Pages

  Weihs, H ^a   Longo, J ^a   Turner, J ^a  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMICS; ANTENNAS; HYPERSONIC VEHICLES; MECHANICAL ACTUATORS;

ACTIVE CONTROL SYSTEMS; ADVANCED SENSORS; AERODYNAMIC CONTROL; ELECTRONIC CONTROL UNITS; HIGH TEMPERATURE; SHARP EDGE FLIGHT EXPERIMENT; TEST VEHICLE; THERMAL PROTECTION;

FLIGHT CONTROL SYSTEMS;

EID: 77958500802     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2008-2542     Document Type: Conference Paper

References (12)

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3. Korfanty, M., CFD based Dynamic Analysis of Atmospheric Re-Entry Vehicles, 2nd International ARA Days, Arcachon, October 2008.
4. Weihs, H., Longo, J., Gülhan, A.: The sharp edge flight experiment SHEFEX. 4th European Workshop on Hot Structures and TPS for Space Vehicles, Palermo, Italien, 26-29 November 2002, ESA/ASI/DLR/CNES, (2002)
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11. th ESA Symposium on European Rockets and Balloon Programmes and Related Research, ESA 2005.
12. Weihs H., Turner J., Hörschgen M., "SHEFEX II - The Next Step within Flight Testing of Re-Entry Technology", 57th International Astronautical Congress, Valencia, Oct. 2006.