Thermostructural analysis of X-34 wing leading-edge tile thermal protection system

Journal of Spacecraft and Rockets

Volumn 36, Issue 2, 1999, Pages 189-198

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

^a NASA AMES RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

AIRCRAFT MATERIALS; COMPUTER SIMULATION; FINITE ELEMENT METHOD; HEAT SHIELDING; LOADS (FORCES); MECHANICAL PROPERTIES; SILICONES; STRESS ANALYSIS; THERMOANALYSIS; THERMODYNAMIC PROPERTIES; TILE; WINGS;

SILICONE IMPREGNATED REUSABLE CERAMIC ABLATOR; THERMAL PROTECTION SYSTEM; THERMOSTRUCTURAL ANALYSIS;

AEROSPACE VEHICLES;

EID: 0033097532     PISSN: 00224650     EISSN: None     Source Type: Journal    
DOI: 10.2514/2.3449     Document Type: Article

References (9)

1. Palmer, G., and Polsky, S., "Heating Analysis of the Nosecap and Leading Edges of the X-34 Vehicle," Journal of Spacecraft and Rockets, Vol. 36, No. 2, 1999, pp. 199-205.
2. Tran, H., Johnson, C., Rasky, D., Hui, F., and Hsu, M., "Silicone Impregnated Reusable Ceramic Ablators for Mars Follow-on Missions," AIAA Paper 96-1819, June 1996.
3. Marschall, J., and Milos, F. S., "Gas Permeability of Rigid Fibrous Refractory Insulations," AIAA Paper 97-2479, June 1997.
4. Milos, F. S., and Squire, T. H., "X-34 Tile Analysis Annual Report for FY97," X-34 Project Rept., NASA Ames Research Center, Oct. 1997.
5. Lashkari, M., "COSMOS/M User's Guide, Volume 1," Structural Research and Analysis Corp., Santa Monica, CA, April 1992.
6. Chen, Y.-K., and Milos, F. S., "Ablation and Thermal Response Program for Spacecraft Heatshield Analysis," AIAA Paper 98-0273, Jan. 1998.
7. Squire, T. H., Milos, F. S., Hartlieb, G. C., and Rasky, D. J., "TPSX: Thermal Protection Systems Expert and Material Property Database," ICCE/4 Fourth International Conference on Composites Engineering, edited by D. Hui, ICCE, and College of Engineering, Univ. of New Orleans, New Orleans, LA, 1997, pp. 937, 938.
8. McGrory, D. M., Stack, D. C., Applebaum, M. P., and Walters, R. W., GASP Version 2.2 User's Manual, Aerosoft, Inc., Blacksburg, VA, 1993.
9. Chen, Y.-K., and Milos, F. S., "Solution Strategy for Thermal Response of Nonablating Thermal Protection Systems at Hypersonic Speeds," AIAA Paper 96-0615, Jan. 1996.