Aeroheating thermal model correlation for mars global surveyor (MGS) solar array

36th AIAA Thermophysics Conference

Volumn , Issue , 2003, Pages

  Amundsen, Ruth M ^a   Dec, John A ^a   George, Lt Benjamin E ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b AIR FORCE RESEARCH LABORATORY   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FLUX BOUNDARY CONDITIONS; GOOD CORRELATIONS; LARGE SURFACE AREA; MARS GLOBAL SURVEYOR; MAXIMUM TEMPERATURE; MODELING PROCESS; PREDICTED MODELS; THERMAL BEHAVIORS;

AERODYNAMIC HEATING; DRAG; HEAT FLUX; MARTIAN SURFACE ANALYSIS; SENSOR NODES; SOLAR CELL ARRAYS; SPACECRAFT; THERMAL LOAD; THERMOANALYSIS; THERMOGRAPHY (TEMPERATURE MEASUREMENT);

AEROBRAKING;

EID: 84896793394     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Dec, John A., and Amundsen, Ruth M., A Thermal Analysis Approach for the Mars Odyssey Spacecraft's Solar Array, AIAA 2003 Thermophysics Conference, Orlando, Florida, June 2003.
2. Thermal Desktop user manual, Cullimore and Ring Technologies, Inc., Version 3.2, August 2000.
3. MSC/PATRAN User Manual, MacNeal-Schwendler Corporation, Version 2000 (r2), August 2000.
4. Internal memo, Lockheed Martin, "Solar Array Thermal Model", May 27, 1999 from Mike Griffin to Susan Bathras.
5. Internal NASA LaRC communication, "MGS /Odyssey LaRC Aeroheating Analysis", R.G. Wilmoth, June 21, 2001.