The aim of this paper is to present a re-entry stability analysis for the uncontrolled, non-winged, blunted cone space vehicle SARA (Atmospheric Re-entry Satellite) by taking into account a ballistic trajectory. The SARA project is a cooperation between Brazilian Space Agency (AEB) and Institute of Aeronautics and Space (IAE) to develop and construct a recoverable space vehicle to perform microgravity experiments. The Brazilian suborbital rocket VS-40 provides the insertion of the SARA capsule into microgravity environment reaching altitudes above 190 km. The analyzes presented in this work focuses on two configurations for SARA being the first, a blunted cone without aps (aero-breaking) and, the second, a blunted cone with aps. The work shows in details the re-entry stability analysis and co-simulation methodology including Newton's impact method modeling (NIM) and Computational Fluid Dynamics (CFD) software.
Atmospheric re-entry stability analysis of the space vehicle SARA / De Oliveira, Élcio J.; Souza, Carlos H. M.; Korzenowski, Heidi; Gasbarri, Paolo; Vilas Bôas, Danton J. F.. - STAMPA. - 9:(2017), pp. 6077-6084. (Intervento presentato al convegno 68th International Astronautical Congress: Unlocking Imagination, Fostering Innovation and Strengthening Security, IAC 2017 tenutosi a Adelaide; Australia).
Atmospheric re-entry stability analysis of the space vehicle SARA
Gasbarri, Paolo;
2017
Abstract
The aim of this paper is to present a re-entry stability analysis for the uncontrolled, non-winged, blunted cone space vehicle SARA (Atmospheric Re-entry Satellite) by taking into account a ballistic trajectory. The SARA project is a cooperation between Brazilian Space Agency (AEB) and Institute of Aeronautics and Space (IAE) to develop and construct a recoverable space vehicle to perform microgravity experiments. The Brazilian suborbital rocket VS-40 provides the insertion of the SARA capsule into microgravity environment reaching altitudes above 190 km. The analyzes presented in this work focuses on two configurations for SARA being the first, a blunted cone without aps (aero-breaking) and, the second, a blunted cone with aps. The work shows in details the re-entry stability analysis and co-simulation methodology including Newton's impact method modeling (NIM) and Computational Fluid Dynamics (CFD) software.File | Dimensione | Formato | |
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De Oliveira_Atmospheric-re-entry_2017.pdf
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