Thermal robustness and Mass optimization of heat pipe shape for spacecraft panel using a combination of response surface methodology and Monte Carlo simulation

ASME 2002 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference, IDETC/CIE2002

Volumn 2, Issue , 2002, Pages 181-189

  Kobayashi, Takashi ^a   Nomura, Takehide ^a   Kamifuji, Masaki ^a   Yao, Akira ^a   Ogushi, Tetsurou ^a  

^a MITSUBISHI ELECTRIC CORPORATION   (Japan)

Author keywords

[No Author keywords available]

Indexed keywords

COMMERCIAL SPACECRAFT; DESIGN FACTORS; HEAT PIPE DESIGN; MASS OPTIMIZATION; MATRIX; MONTE CARLO SIMULATION; ON ORBIT; PIPE STRUCTURE; RESPONSE SURFACE METHODOLOGY; ROBUST DESIGNS; ROBUST OPTIMIZATION METHOD; THERMAL CONTROL; THERMAL DESIGNS; THERMAL OPTIMIZATION; THERMAL SUBSYSTEM;

COMPUTER AIDED DESIGN; COMPUTER SIMULATION; COOLING SYSTEMS; DESIGN OF EXPERIMENTS; MONTE CARLO METHODS; OPTIMIZATION; SPACECRAFT; SURFACE PROPERTIES; TECHNICAL PRESENTATIONS; HEAT PIPES; INTELLIGENT SYSTEMS; ORBITS;

HEAT PIPES; MONTE CARLO METHODS;

EID: 0036973884     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

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