DSMC modeling of chemically reacting two- and three-dimensional flows from Soyuz-TM rocket exhaust plumes

34th Thermophysics Conference

Volumn , Issue , 2000, Pages

  Gimelshein, S F ^a   Levin, D A ^a   Drakes, J A ^b   Karabadzhak, G F ^c   Plastinin, Yu ^c  

^a GEORGE WASHINGTON UNIVERSITY   (United States)

^b Arnold AFB ^*  (United States)

^c CENTRAL RESEARCH INSTITUTE OF MACHINE BUILDING   (Russian Federation)

Author keywords

[No Author keywords available]

Indexed keywords

ORBITS; REACTION RATES; ROCKETS;

COEFFICIENT OF VISCOSITY; DIRECT SIMULATION MONTE CARLO METHOD; MOLECULAR COLLISIONS; NEAR FIELD RADIATION; OVERLAY TECHNIQUES; SPACECRAFT THRUSTERS; THREE-DIMENSIONAL COMPUTATIONS; THREE-DIMENSIONAL FLOW;

MONTE CARLO METHODS;

EID: 85086615338     PISSN: None     EISSN: None     Source Type: Conference Proceeding    
DOI: 10.2514/6.2000-2433     Document Type: Conference Paper

References (14)

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2. Viereck, R. A., Murad, E., Knecht, D. J., Pike, C. P., Bernstein, L. S., Elgin, J. B., and Broad-foot, A. L., "The interaction of the atmosphere with the space shuttle thruster plume: The NH(A-X) 336-nm emission, " Journal of Geophysical Research, Vol. 101, No. A3, 1996, pp. 5371-5380.
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10. th Aerospace Sciences Meeting &; Exhibit, Reno, NV., January, 2000.
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14. th AIAA Aerospace Sciences Meeting & Exhibit, Reno, NV, January 1998.