Application of numerical multizone approach to the study of satellite thruster plumes

Journal of Spacecraft and Rockets

Volumn 35, Issue 4, 1998, Pages 502-508

  Giordano, D ^a,d   Ivanov, M ^b,d,e   Kashkovsky, A ^b,e   Markelov, G ^b,e   Tumino, G ^a   Koppenwallner, G ^c,f  

^a EUROPEAN SPACE AGENCY   (Netherlands)

^b KHRISTIANOVICH INSTITUTE OF THEORETICAL AND APPLIED MECHANICS   (Russian Federation)

^c Hyperschall Technologic Göttingen   (Germany)

^d AIAA   (United States)

^e AIAA ^*  (Russian Federation)

^f Compl Aerodynamics Laboratory ^*

Author keywords

[No Author keywords available]

Indexed keywords

COMPUTER SIMULATION; FLIGHT DYNAMICS; FLOW PATTERNS; MONTE CARLO METHODS; NAVIER STOKES EQUATIONS; OPTIMIZATION; ORBITS; SATELLITES; THERMAL PLUMES;

NUMERICAL MULTIZONE METHOD; SATELLITE THRUSTER PLUMES;

ROCKET ENGINES;

EID: 0032115697     PISSN: 00224650     EISSN: 15336794     Source Type: Journal    
DOI: 10.2514/2.3359     Document Type: Article

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