Multidimensional effects on heatshield thermal response for the Orion Crew Module

Collection of Technical Papers - 39th AIAA Thermophysics Conference

Volumn 2, Issue , 2007, Pages 1090-1104

  Chen, Y K ^a,b,c   Milos, F S ^a,b,c  

^a NASA AMES RESEARCH CENTER   (United States)

^b Thermal Protection Materials and Systems Branch   (United States)

^c AIAA   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

FINITE-VOLUME CODES; ORION CREW MODULE; SURFACE RECESSION; THERMAL RESPONSE;

APPROXIMATION THEORY; COMPUTER SIMULATION; DIFFERENTIAL EQUATIONS; FINITE VOLUME METHOD; INTERFACIAL ENERGY; SPACE RESEARCH;

HEAT SHIELDING;

EID: 35748937360     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (10)

1. Chen, Y.-K., and Milos, F.S., "Three-Dimensional Ablation and Thermal Response Simulation System," AIAA Paper 2005-5064, June 2005.
2. 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.
3. Milos, F..S., Chen, Y.-K., and Squire, T.H., "Updated Ablation And Thermal Response Program For Spacecraft Heatshield Analysis," Paper TFA WS06-1008, The 17th Thermal and Fluids Analysis Workshop, University of Maryland, August 2006.
4. Squire, T.H., Milos, F.S., Hartlieb, G.C., and Rasky, D.J., "TPSX: Thermal Protection Systems Expert and Material Properties," ICCE Fourth International Conference on Composites Engineering, ICCE and College of Engineering, University of New Orleans, July 1997, pp. 937-938.
5. Moyer, C.B., and Rindal, R.A., "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator, Part II, Finite Difference Solution for the In-Depth Response of Charring Materials Considering Surface Chemical and Energy Balances," NASA CR-1061, 1968.
6. Kendall, R.M., "An Analysis of the Coupled Chemically Reacting Boundary Layer and Charring Ablator, Part V, A General Approach to the Thermochemical Solution of Mixed Equilibrium-Nonequilibrium Homogeneous or Heterogeneous Systems," NASA CR-1064, 1968.
7. Milos, F.S., and Chen, Y.-K., "Comprehensive Model for Multi-Component Ablation Thermochemistry," AIAA Paper 97-0141, January 1997.
8. Greathouse, J.S., Kirk, B.S., Lillard, R.P., Truong, T.H., Robinson, P., and Cerimele, C.J., "Crew Exploration Vehicle (CEV) Crew Module shape selection analysis and CEV Aeroscience Project Overview," AIAA Paper 2007-603, January 2007.
9. Kinney, D.J., "Aero-Thermodynamics for Conceptual Design," AIAA Paper 2004-31, January 2004.
10. Chen, Y.-K., and Milos, F.S., "Two-Dimensional Implicit Thermal Response and Ablation Program for Charring Materials," Journal of Spacecraft and Rockets, Vol. 38, No. 4, 2001, pp. 473-481.