Investigation of fundamental modeling and thermal performance issues for a metallic thermal protection system design

40th AIAA Aerospace Sciences Meeting and Exhibit

Volumn , Issue , 2002, Pages

  Blosser, Max L ^a  

^a NASA LANGLEY RESEARCH CENTER   (United States)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84894328745     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (15)

1. Blosser, M. L., "Advanced Metallic Thermal Protection Systems for Reusable Launch Vehicles", Ph. D. Dissertation, UVA, May 2000.
2. Dorsey, John T.; Poteet, Carl; and Chen, Roger: "Metallic Thermal Protection System Technology Development: Concepts, Requirements and Assessment Overview, " 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 14-17, 2002.
3. Poteet, Carl; Abu-Khajeel, Hasan,; and Hsu, Su-Yuen: "Preliminary Thermal-Mechanical Sizing of Metallic TPS: Process Development and Sensitivity Studies, " 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 14-17, 2002.
4. Daryabeigi, K.: "Design of High Temperature Multi-layer Insulation for Reusable Launch Vehicles, " PhD Dissertation, University of Virginia, May 2000.
5. Blosser, M.L.; Chen, R.R.; Schmidt, I.H.; Dorsey, J.T.; Poteet, C.C.; and Bird, R.K.: "Advanced Metallic Thermal Protection System Development, " 40th AIAA Aerospace Sciences Meeting and Exhibit, Reno, NV, January 14-17, 2002.
6. Sawyer, J. W., Hodge, J., & Moore, B., 1998, Aero/Thermal Test of Metallic TPS for X-33 Reusable Launch Vehicle, 3rd European Workshop on Thermal Protection Systems, ESTEC, The Netherlands.
7. Whetstone, W.D.: "EISI-EAL Engineering Analysis Language Reference Manual, System Level 335, " Engineering Information Services, Inc., San Jose, CA, Oct. 1998
8. Marlowe, M.B.; Moore, R.A.; and Whetstone, W.D.: "SPAR Thermal Analysis Processors Reference Manual, System Level 16, " NASA CR-159162, 1979.
9. Kreith, F.; and Black, W.Z.: Basic Heat Transfer, Harper & Row, Publishers, New York, 1980.
10. Gorton, M.P.; Shideler, J.L.; and Webb, G.L.: "Static and Aerothermal Tests of a Superalloy Honeycomb Prepackaged Thermal Protection System, " NASA TP 3257, March, 1993.
11. Phadke, M.S.: Quality Engineering using Robust Design, Prentice Hall, Englewood Cliffs, NJ, 1989.
12. Ross, P.J.: Taguchi Techniques for Quality Engineering: Loss Function, Orthogonal Experiments, Parameter and Tolerance Design, Second edition, McGraw-Hill, New York, 1996.
13. Norris, P.M.: "Application of Experimental Design Methods to Assess the Effect of Uncertain Boundary Conditions in Inverse Heat Transfer Problems, " International Journal of Heat and Mass Transfer, Vol. 41, No. 2, pp.313-322, 1998.
14. Kakac, S.; Shah, R.K.; and Aung, W.: Handbook of Single-Phase Convective Heat Transfer, John Wiley & Sons, New York, 1987.
15. Ko, W.L.; Quinn, R.D.; and Gong, L.: "Finite-Element Reentry Heat Transfer Analysis of Space Shuttle Orbiter, " NASA TP 2657, Dec., 1986.