Preliminary thermal analysis of a mars sample return earth entry vehicle

34th Thermophysics Conference

Volumn , Issue , 2000, Pages

  Amundsen, Ruth M ^a   Dec, John A ^a   Mitcheltree, Robert A ^a   Lindell, Michael C ^a   Dillman, Robert A ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

THERMOANALYSIS; VEHICLES;

ADVANCED MODELING TECHNIQUES; EARTH ENTRY VEHICLES; HIGH HEATING RATES; MARS SAMPLE RETURN; MARS SAMPLE RETURN MISSIONS; MATHEMATICAL SOLUTIONS; ORTHOTROPIC MATERIAL PROPERTIES; THERMAL CONDITION;

EARTH ATMOSPHERE;

EID: 85088756978     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-2584     Document Type: Conference Paper

References (11)

1. th AIAA/ASME Joint Thermodynamics and Heat Transfer Conference, Albuquerque, New Mexico, AIAA 98-2851, June 15-18, 1998.
2. Mars Sample Return Earth Entry Vehicle Conceptual Design Assessment, NASA Langley Research Center, November 3-4, 1999, MSR EEV Project Office.
3. Pro/ENGINEER Fundamentals Manual, Parametric Technology Corporation, Release 20.0 (June 1998).
4. MSC/PATRAN User Manual, MacNeal-Schwendler Corporation, Version 9.0 (May 1999).
5. User Manual, Thermal Synthesizer System, Release 6.1, Lockheed Martin Space Mission Systems, NAS9-19100, October 1997.
6. TPSX, Thermal Protection Systems Expert and Material Properties Database, February 1998, NASA Ames Research Center (http://asm.arc.nasa.gov/tpsx/).
7. C. W. Ohlhorst, W. L. Vaughn, P. O. Ransone, H. Tsou, "Thermal Conductivity Database of Various Structural Carbon-Carbon Composite Materials, " NASA TM-4787, NASA Langley Research Center, November 1997.
8. E. M. Silverman, "Composite Spacecraft Structures Design Guide, " NASA Contractor Report 4708, Contract NAS 1-19319, March 1996.
9. D. G. Gilmore, Satellite Thermal Control Handbook, The Aerospace Corporation Press. El Segundo, California, 1994.
10. J. H. Henninger, "Solar Absorptance and Thermal Emittance of Some Common Spacecraft Thermal Control Coatings, " NASA Reference Publication 1121, Goddard Space Flight Center, April 1984.
11. Y. K. Chen and F. S. Milos, "Ablation and Thermal Response Program for Spacecraft Heatshield Analysis, " Journal of Spacecraft and Rockets, Vol. 36, No. 3, 1999, pp. 475-482.