Development of a high-fidelity thermal/ablation response model for SLA-561V

41st AIAA Thermophysics Conference

Volumn , Issue , 2009, Pages

  Laub, Bernard ^a   Chen, Yih Kanq ^a   Dec, John A ^b  

^a NASA AMES RESEARCH CENTER   (United States)

^b NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

A-THERMAL; ABLATION MECHANISMS; CYLINDRICAL SAMPLES; DEPTH MODELS; HIGH FIDELITY; RESPONSE MODEL; SURFACE ABLATION; SURFACE RECESSION; SURFACE TEMPERATURES; TEMPERATURE RESPONSE;

NASA;

ABLATION;

EID: 77958451553     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (5)

1. Beck, R.A.S., User's Manual, Code to Fit TGA Data (TGAFIT), Acurex Corporation, Aerotherm Division, Mountain View, California, July 1981.
2. Chen, Y.-K., and Milos, F.S., "Ablation and Thermal Analysis Program for Spacecraft Heatshield Analysis," J. Spacecraft and Rockets, Vol. 36, No. 3, pp. 475-483, 1999.
3. Laub, B., Chen, Y-K., and Dec, J.A., "Development of a High-Fidelity Thermal/Ablation Response Model for SLA-561V," NASA TM-xxxx, to be published.
4. User's Manual, Aerotherm Chemical Equilibrium Computer Program (ACE81), Acurex Corporation, Aerotherm Division, Mountain View, California, August 1981.
5. Bethe, H.A. and Adams, M.C., "A Theory for the Ablation of Glassy Materials," J. of Aerospace Sciences, Vol. 26, No. 6, June 1959, pp. 321-328.