Design studies of the JAPHAR experimental vehicle for dual mode ramjet demonstration

10th AIAA/NAL-NASDA-ISAS International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 2001, Pages

  Eggers, Th ^a   Novelli, Ph ^b   Haupt, M ^c  

^a GERMAN AEROSPACE CENTER DLR   (Germany)

^b ONERA   (France)

^c TECHNICAL UNIVERSITY OF BRAUNSCHWEIG   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

AERODYNAMIC STABILITY; COMBUSTION; FLUID STRUCTURE INTERACTION; RAMJET ENGINES; SPACECRAFT PROPULSION; SUPERSONIC AIRCRAFT;

AIR-BREATHING PROPULSION; COMPONENT PERFORMANCE; EXPERIMENTAL VEHICLE; FLUID STRUCTURE COUPLINGS; IN-FLIGHT PERFORMANCE; LEVEL OF INTEGRATIONS; LONGITUDINAL STABILITY; SUPERSONIC COMBUSTION;

HYPERSONIC VEHICLES;

EID: 85087593201     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2001-1921     Document Type: Conference Paper

References (11)

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