Thermostructural analysis of SIRCA tile for X-34 wing leading edge TPS

36th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 1998, Pages

  Milos, Frank S ^a   Squire, Thomas H ^a  

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AEROSPACE ENGINEERING;

AEROTHERMAL; FAILURE CRITERIA; MECHANICAL LOADS; SAFETY MARGIN; STRUCTURAL MODELS; STRUCTURAL REQUIREMENTS; THERMO-STRUCTURAL ANALYSIS; WING LEADING EDGES;

FINITE ELEMENT METHOD;

EID: 84983140559     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (9)

1. Palmer, G. and Polsky, S., "A Heating Analysis of the Nosecap and Leading Edges of the X-34 Vehicle," Paper AIAA 98-0878, Jan. 1998.
2. F. S. Milos and T. H. Squire, "Thermal Stress Analysis of X-34 Wing Leading Edge TPS," Paper AIAA 96-1821, June 1996.
3. Tran, H., Johnson, C., Rasky, D., Hui, F., and Hsu, M., "Silicone Impregnated Reusable Ceramic Ablators for Mars Follow-on Missions," Paper AIAA 96-1819, June 1996.
4. J. Marschall and F. S. Milos, "Gas Permeability of Rigid Fibrous Refractory Insulations," Paper AIAA 97-2479, June 1997.
5. F. S. Milos and T. H. Squire, "X-34 Tile Analysis Annual Report for FY97," X-34 Project Report, NASA Ames, Oct. 1997.
6. Lashkari, M., "COSMOS/M User's Guide, Volume I," Structural Research and Analysis Corp., Santa Monica, CA, April 1992.
7. Chen, Y.-K., and Milos, F. S., "Ablation and Thermal Response Program for Spacecraft Heatshield Analysis," Paper AIAA 980273, Jan. 1998.
8. McGrory, D. M., Stack, D. C., Applebaum, M. P., and Walters, R. W., GASP Version 2. 2 User's Manual, Aerosoft, Inc., 1993.
9. Y.-K. Chen and F. S. Milos, "Solution Strategy for Thermal Response of Nonablating Thermal Protection Systems at Hypersonic Speeds," Paper AIAA 96-0615, Jan. 1996.