Aerothermodynamic aspects of entry probe heat shield design

Astrophysics and Space Science

Volumn 260, Issue 1-2, 1998, Pages 45-62

  Marraffa, L ^a   Smith, A ^b  

^a EUROPEAN SPACE AGENCY   (Netherlands)

^b Fluid Gravity Engineering   (United Kingdom)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 0038900089     PISSN: 0004640X     EISSN: None     Source Type: Journal    
DOI: 10.1023/a:1001874903881     Document Type: Article

References (10)

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3. 2 past an Infinite Cylinder according to State- to State Vibrational Kinetics and to the Harmonic-Oscillator Model, 30th AIAA Thermophysics Conference, June 19-22, 1995, San Diego (CA)
4. Gogel T. H. Messerschmid E.W. MCM Users Manual. Institut Fur Raumfahrtsysteme University of Stuttgart 1994
5. Goulard R., Catalytic Recombination Rates in Hypersonic Stagnation Heat Transfer, Jet Propulsion Journal, vol. 28, n. 11, pp. 737-745, Nov. 1958
6. Marraffa L., Giordano D., Huot J. P., Smith A. (1992), Hypersonic Aerothermodynamic Aspects of ESA Scientific Exploration Probes, Proceedings of the IUTAM Symposium, Marseilles, September 1992
7. Marriott, P.M. (1996), Comparison of the DSMC Maximum Entropy approach and the SSH approach for single cell relaxation vibrationally relaxing Flow. AIAA 96-0603. 34th AIAA Aerospace Sciences Meeting and Exhibit, January 15-18, 1996, Reno, NV
8. Roberts T. P., Daley S., Smith A.J. (1996), TINA Version 3, Theory and User Manual, FGE TN 89/96, December 1996
9. Smith A. J., Gogel T., Vandevelde P.(1996), Plasma Radiation Database-PARADE Final Report ESTEC Contract 11148/94/NL/FG. FGE TR28/96 April 1996.
10. Smith A., Heat Transfer for Perfect Gas and Chemical Reacting, in AGARD/VKI Special Course-Capsule Aerothermodynamics, AGARD Report 808, March 1995