Heat transfer simulation and surface catalycity prediction at the martian atmosphere entry conditions

9th International Space Planes and Hypersonic Systems and Technologies Conference

Volumn , Issue , 1999, Pages

  Kolesnikov, Anatoly ^a   Yakushin, Mikhail ^a   Pershin, Ivan ^a   Vasil'evskii, Sergey ^a  

^a INSTITUTE FOR PROBLEMS IN MECHANICS   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

ATMOSPHERIC TEMPERATURE; CARBON DIOXIDE; COATINGS; ENTHALPY; FLIGHT DYNAMICS; HEAT FLUX; PROBES; QUARTZ; SPACECRAFT;

CATALYTIC EFFICIENCIES; HEAT TRANSFER SIMULATION; LOCAL HEAT TRANSFER SIMULATIONS; MAXIMUM TEMPERATURE; RECOMBINATION REACTIONS; STAGNATION POINT HEAT FLUXES; STAGNATION PRESSURES; SURFACE TEMPERATURES;

HEAT TRANSFER;

EID: 84982318111     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: None     Document Type: Conference Paper

References (23)

1. Rubio Garcia V., Marraffa L., Scoon G., Roumeas R., Mars mini-probes. Elements of Aerothermodynamics and Entry Trajectories. Proc. of the Third European Symposium on Aerothermodynamics for Space Vehicles, ESTEC, Noordwijk, The Netherlands, 24-26 November 1998 (ESA SP-426, January 1999), p. 155-162.
2. Kolesnikov A., Conditions of Simulation of Stagnation Point Heat Transfer from a High-Enthalpy Flow. Fluid Dynamics (tr. from Russian), V. 28, N. 1, 1993, p. 131-137. '.
3. Kolesnikov A, 'The Aerothèrmodynamiċ Simulation in Sub-and Supersonic High-Enthalpy Jets: Experiment and Theory. Proc. of the Second European Symposium on Aerothermodynamics for Space Vehicles, ESTEC, Noordwijk, The Netherlands, 21-25 November 1994 (ESA SP-367, February 1995), p. 583-590.
4. Bykova N., Vasilevskii S., Gordeev A., Kolesnikov A., Pershin I., Yakushin M. Determination of the Effective Probabilities of Catalytic Reactions on the Surfaces of Heat Shield Materials in Dissociated Carbon Dioxide Flows. Fluid Dynamics (tr. from Russian), V. 32, N. 6, 1997, p. 876-886.
5. Kolesnikov A., Pershin I., Vasilevskii S., and Yakushin M., Study of Quartz-Surface Càtalycity in Dissociated Carbon Dioxide Flows, AIAA Paper 98-2847, 1998.
6. Kolesnikov A:, Yakushin M., Vasilevskii S., Pershin I., Gordeev A., Catalysis Effects on Quartz Surface in High-Enthalpy Oxygen & Carbon Dioxide Flows, Proc. of the Third European Symposium on Aerothermodynamics for Space Vehicles, ESTEC, Noordwijk, The Netherlands, 24-26 November 1998 (ESA SP-426, 1999), p. 537-544.
7. Chen Y. K., Henline W. D., Stewart D. A., Candler G. V., Navier-Stokes Solutions with Surface Catalysis for Martian Atmospheric Entry. Journal of Spacecraft and Rockets, V. 30,; N 1, 1993, p. 32-42.
8. Gupta R. N., Leė R. N., Scott C. D., Aerothermal Study of Mars Pathfinder-Aeroshell. Journal of Spacecraft and Rockets, V. 33, N. 1, 1996, p. 61-69.
9. Kay R. D., Netterfíeld M. P., Thermochemical Non-Equilibrium Computations of a Mars Entry Vehicles. AIAA Paper 93-2841, 1993.
10. Gromov V. G., Afonina N. E., Thermochemical Nonequilibrium Computations for a Mars Probe, Proc. of the Third European Symposium on Aerothermodynamics for Space Vehicles, ESTEC, Noordwijk, The Netherlands, 24-26: November 1998 (ESA SP-426, 1999), p. 179-186.
11. Gordeev A. N., Kolesnikov A. F., Yakushin M. I., An Induction Plasmatron Application to 'Buran's' Heat Protection. Tiles Ground Tests, SÁMPE Journal, V, 28, N. 3, 1992, p.: 29-33.
12. Bykova N., Vasilevskii S., Gordeev A., Kolesnikov A., Pershin I., Yakushin M, An Induction Plasmatron. Application for Simulation of Entry into Martian Atmosphere. Proc. of the Third International Symposium on Environmental Testing for Space Programmes, ESTËC, Noordwijk, The Netherlands, 24-27 June 1997 (SP-408, August 1997), p. 195-200.
13. Kolesnikov Â., ShchelinV., Numerical Analysis of Simulation Accuracy for Hypersonic Heat Transfer in Subsonic Jets of Dissociated Nitrogen, Fluid Dynamics (tr. from Russian), V. 25, N. 2, 1990, p. 278-288.
14. Kolesnikov A., The Concept of The Local Thermo-Chemical Simulation for Re-Entry Problem: Validation & Applications, presented at the 9th Thermal & Fluids Analysis Workshop, August 31-September 4, 1998, NASA Lewis Research: Center and Ohio Aerospacę Institute, Cleveland, Ohio.
15. Kolesnikov, A., Marraffa L., An Analysis of Stagnation Point Thermochemical Simulation by Plasmatron for Mars Probe, AIAA 99-3564, 1999.
16. Vasilevskii S. A., Kolesnikov A. F., and Yakushin M. I., Determination of the Effective Probabilities of the Heterogeneous' Recombination of Atoms When Heat Flow is Influenced by Gas-Phase Reactions, High Temperature, Plenum, (tr. from Russian), V. 29, N. 3, 1991, p. 411-419.
17. Vasilevskii S. A., Kolesnikov A. F., Yakushin M. I., Mathematical Models for Plasma and Gas Flows in Induction Plasmatrons, In: Molecular Physics and Hypersonic Flows, ed. by M. Capitelli, NATO ASI Series, V. 482, 1996, Kluwer, p. 495-504.
18. Kolesnikov A. F., Vasilevskii S. A., Some problems of Numerical Simulation of Discharge. Electrodynamics in Induction Plasmatron, Proc. of 15th IMACS World Congress, Berlin, August 1997. V. 3, Computational Physics, Chemistry and Biology. Ed. by A. Sydov, p. 175-180.
19. Kolesnikov A. F., Vasilevskii S. A., Results and Problems of Inductively Coupled Plasma Flows Modeling, IPM RAS, Preprint N. 610, Moscow, 1998, 28 p. '.
20. Patankar S. V., Spalding D. B., Heat and Mass Transfer in Boundary Layers. Intertext Books, London, 1970.
21. Fay J. A. and Riddell F. R., Theory of Stagnation Point Heat Transfer in. Dissociated Air, J. Aeronaut. Sci., V. 25, N. 2, 1958, p. 73-85.
22. Petrov V. A., Reznik V. Yu., Total Normal Emissivity of Quartz Glass of 'QR' Type at High Temperatures, Teplofizika Vysokih Temperatur, V. 10, N. 4, 1972, p. 778.
23. Park C, Candler G. V., Howe J. T., Jaffe Ŕ. T., Cjhiemical-Kinetic Problems of Future NASA Missions, AIAA91-0464, 1991.