Simulation of the aerothermal environment experienced by space vehicles during atmospheric reentry can be performed by arc-jet facilities, which generate high enthalpy hypersonic flows for long time. Such is the case of Small Planetary Entry Simulator (SPES) at the Department of Aerospace Engineering of University of Naples (DIAS), described in the paper. To support arc-jet tests within SPES it is important to dispose of a simple tool which evaluates all aerothermodynamic flow properties by using the few experimental measurements available and a chemical model of the high enthalpy flow. In the paper we present the model implemented and used for arc-jet tests performed for AVIO company, to evaluated performances of its thermal protection material for the European space vehicle named IXV.

Fast Diagnostics for high enthalpy hypersonic flows / Esposito, Antonio; Caso, Vincenzo. - STAMPA. - (2011), pp. 0-0. (Intervento presentato al convegno 3rd CEAS Air&Space Conference, 21th AIDAA Congress tenutosi a Venezia nel 24 – 28 Ottobre 2011).

Fast Diagnostics for high enthalpy hypersonic flows

ESPOSITO, ANTONIO;CASO, VINCENZO
2011

Abstract

Simulation of the aerothermal environment experienced by space vehicles during atmospheric reentry can be performed by arc-jet facilities, which generate high enthalpy hypersonic flows for long time. Such is the case of Small Planetary Entry Simulator (SPES) at the Department of Aerospace Engineering of University of Naples (DIAS), described in the paper. To support arc-jet tests within SPES it is important to dispose of a simple tool which evaluates all aerothermodynamic flow properties by using the few experimental measurements available and a chemical model of the high enthalpy flow. In the paper we present the model implemented and used for arc-jet tests performed for AVIO company, to evaluated performances of its thermal protection material for the European space vehicle named IXV.
2011
Fast Diagnostics for high enthalpy hypersonic flows / Esposito, Antonio; Caso, Vincenzo. - STAMPA. - (2011), pp. 0-0. (Intervento presentato al convegno 3rd CEAS Air&Space Conference, 21th AIDAA Congress tenutosi a Venezia nel 24 – 28 Ottobre 2011).
File in questo prodotto:
Non ci sono file associati a questo prodotto.

I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.

Utilizza questo identificativo per citare o creare un link a questo documento: https://hdl.handle.net/11588/567776
Citazioni
  • ???jsp.display-item.citation.pmc??? ND
  • Scopus ND
  • ???jsp.display-item.citation.isi??? ND
social impact