Transpiration cooling applied to C/C liners of cryogenic liquid rocket engines

40th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Volumn , Issue , 2004, Pages

  Greuel, D ^a   Herbertz, A ^a   Haidn, O J ^a   Ortelt, M ^b   Hald, H ^b  

^a Institute of Space Propulsion   (Germany)

^b GERMAN AEROSPACE CENTER DLR   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

COMMON MODELS; COOLING EFFICIENCY; ENGINE MASS; EXPERIMENTAL STUDIES; MASS FLOW; MASS FLOW RATE; MATERIAL PROPERTY; MIXED APPROACH; OPTIMISATIONS; POROUS STRUCTURES; SYSTEM ANALYSIS; THERMAL PROTECTION; THRUST CHAMBER; TRANSPIRATION COOLING;

BOOSTERS (ROCKET); CERAMIC MATRIX COMPOSITES; COOLANTS; COOLING; FLOW RATE; LIQUIDS; MASS TRANSFER; PIPE FLOW; PROPULSION;

TRANSPIRATION;

EID: 77957841580     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

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