Monte Carlo analysis for spacecraft thermal protection system design

Collection of Technical Papers - 9th AIAA/ASME Joint Thermophysics and Heat Transfer Conference Proceedings

Volumn 1, Issue , 2006, Pages 486-500

  Chen, Yih Kanq ^a,b   Squire, Thomas ^a,b   Laub, Bernard ^a,b,c   Wright, Michael ^a,c,d  

^a NASA AMES RESEARCH CENTER   (United States)

^b Thermal Protection System and Materials Branch

^c AIAA   (United States)

^d MS 229 ^*

Author keywords

[No Author keywords available]

Indexed keywords

LEADING EDGES; MATERIAL RESPONSE; THERMAL PROTECTION SYSTEMS; THERMAL RESPONSE CODES;

COMPUTATION THEORY; COMPUTER SIMULATION; MATHEMATICAL MODELS; MONTE CARLO METHODS; PROBABILITY; SPACECRAFT EQUIPMENT; THERMAL EFFECTS;

THERMAL INSULATION;

EID: 33845538316     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Dec, J. A. and Mitcheltree, R. A., "Probabilistic Design of A Mars Sample Return Entry Vehicle Thermal Protection System," AIAA Paper 2002-0910.
2. Bose, D., Wright, M.J., and Gokcen, T., "Uncertainty and Sensitivity Analysis of Thermochemical Modeling for Titan Atmospheric Entry," AIAA paper 2004-2455.
3. Bose, D., Wright, M.J., and Chen, Y.-K., "Probabilistic Modeling of Aerothermal and Material Response Uncertainties for Aerocapture Using Rigid Aeroshells," JANNAF Joint Propulsion Meeting, December 5-8 2005.
4. Chen, Y.-K., and Milos, F.S., "Ablation and Thermal Analysis Program for Spacecraft Heatshield Analysis," Journal of Spacecraft and Rockets, vol. 36, No. 3, 1999, pp. 475-483.
5. Wright, M.J., Candler, G.V., and Bose, D., "Data-Parallel Line Relaxation Method for the Navier-Stokes Equations," AIAA Journal, Vol. 36, No. 9, 1998, pp. 1603-1609.