Preliminary thermal-mechanical sizing of a metallic thermal protection system

Journal of Spacecraft and Rockets

Volumn 41, Issue 2, 2004, Pages 173-182

  Poteet, Carl C ^a,c   Abu Khajeel, Hasan ^b   Hsu, Su Yuen ^b  

^a NASA LANGLEY RESEARCH CENTER   (United States)

^b LOCKHEED MARTIN   (United States)

^c Metals and Thermal Structures Branch   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

DEBRIS; DURABILITY; ESTIMATION; FINITE ELEMENT METHOD; HEATING; ITERATIVE METHODS; SPACE RESEARCH; STRUCTURAL ANALYSIS;

AEROTHERMAL HEATING; REUSABLE LAUNCH VEHICLES (RLV); STEFAN-BOLTZMANN CONSTANT; THERMAL PROTECTION SYSTEMS (TPS);

SPACECRAFT;

EID: 2342452525     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/1.9174     Document Type: Article

References (22)

1. Blosser, M. L., Chen, R. R., Schmidt, I. H., Dorsey, J. T., Poteet, C. C., Bird, R. K., and Wurster, K. E., "Development of Advanced Metallic Thermal-Protection-System Prototype Hardware," Journal of Spacecraft and Rockets, Vol.41, No. 2, 2004, pp. 183-194; also AIAA Paper 2002-0504. Jan. 2002.
2. Blosser, M. L., Chen, R. R., Schmidt, I. H., Dorsey, J. T., Poteet, C. C., Bird, R. K., and Wurster, K. E., "Development of Advanced Metallic Thermal-Protection-System Prototype Hardware," Journal of Spacecraft and Rockets, Vol.41, No. 2, 2004, pp. 183-194; also AIAA Paper 2002-0504. Jan. 2002.
3. Dorsey, J. T., Poteet, C. C., Wurster, K. E., and Chen, R. R., "Metallic Thermal Protection System Requirements, Environments, and Integrated Concepts," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 162-172; also AIAA Paper 2002-0502, Jan. 2002.
4. Dorsey, J. T., Poteet, C. C., Wurster, K. E., and Chen, R. R., "Metallic Thermal Protection System Requirements, Environments, and Integrated Concepts," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 162-172; also AIAA Paper 2002-0502, Jan. 2002.
5. Poteet, C. C., and Blosser, M. L., "Improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 221-231; also AIAA Paper 2002-0912, Jan. 2002.
6. Poteet, C. C., and Blosser, M. L., "Improving Metallic Thermal Protection System Hypervelocity Impact Resistance Through Numerical Simulations," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 221-231; also AIAA Paper 2002-0912, Jan. 2002.
7. Chen, R. R., and Blosser, M. L., "Metallic Thermal-Protection-System Panel Flutter Study," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 207-212; also AIAA Paper 2002-0501, Jan. 2002.
8. Chen, R. R., and Blosser, M. L., "Metallic Thermal-Protection-System Panel Flutter Study," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 207-212; also AIAA Paper 2002-0501, Jan. 2002.
9. Blosser, M. L., "Fundamental Modeling and Thermal Performance Issues for Metallic Thermal Protection System Concept," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 195-206; also AIAA Paper 2002-0503, Jan. 2002.
10. Blosser, M. L., "Fundamental Modeling and Thermal Performance Issues for Metallic Thermal Protection System Concept," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 195-206; also AIAA Paper 2002-0503, Jan. 2002.
11. Bird, R. K., Wallace, T. A., and Sankaran, S. N., "Development of Protective Coatings for High-Temperature Metallic Materials," Journal of Spacecraft and Rockets, Vol. 41, No. 2, 2004, pp. 213-220.
12. Blair, W., Meaney, J. E., and Rosenthal, H. A., "Re-Design of Titanium Multi-Wall Thermal Protection System Test Panels," NASA CR-172247, Jan. 1984.
13. Wang, J. T., and Johnson, T. F., "Cryogenic Tank Structure Sizing with Structural Optimization Method," AIAA Paper 2001-1599, April 2001.
14. Weiser, E. S., Johnson, T. F., St. Clair, T. L., Echigo, Y., Kaneshiro, H., and Grimsley, B. W., "Polyimide Foams for Aerospace Vehicles," High Performance Polymers, Vol. 12, Feb. 2000, pp. 1-12.
15. Blosser, M. L., "Advanced Metallic Thermal Protection Systems for Reusable Launch Vehicles," Ph.D. Dissertation, Graduate School of Engineering and Applied Science, Univ. of Virginia, Charlottesville, VA, May 2000.
16. Daryabeigi, K., "Analysis and Testing of High Temperature Fibrous Insulation for Reusable Launch Vehicles," AIAA Paper 99-1044, Jan. 1999.
17. Swann, R. T., and Pittman, C. M., "Analysis of Effective Thermal Conductivites of Honeycomb-Core and Corrugated-Core Sandwich Panels," NASA TN D-714, April 1961.
18. Poteet, C. C., "Groundhold and Reentry Purge Parameter Trade Study," Lockheed Martin Space Operations, Rept. LMES SDSR 99-01, Hampton, VA, Aug. 1999.
19. Gruszczynski, M. J., Thorp, V. L., Heim, W. J., and Swanson, N. J., "Design, Development, and Test of the Atlas Liquid Hydrogen Propellant Tank Foam Insulation System," AIAA Paper 91-1438, June 1991.
20. Klopp, W. D., "Inconel 617," Aerospace Structural Metals Handbook, 1994 ed., Vol. 5, CINDA/USAF CRDA Handbooks Operation, Purdue Univ., West Lafayette, IN, 1994, pp. 1-34.
21. Kattus, J. R., "Inconel 718," Aerospace Structural Metals Handbook, 1994 ed., Vol. 4, CINDA/USAF CRDA Handbooks Operation, Purdue Univ., West Lafayette, IN, 1994, pp. 1-58.
22. Hutt, A. J., and Parris, W. M., "TIMETAL-1100 Sheet Properties," Titanium '92 Science and Technology, TMS, San Diego, CA, 1993, pp. 2923-2930.