Title of article
Transient thermal analysis of Vega launcher structures
Author/Authors
F. Gori، نويسنده , , M. De Stefanis، نويسنده , , W.M. Worek، نويسنده , , W.J. Minkowycz، نويسنده ,
Issue Information
روزنامه با شماره پیاپی سال 2008
Pages
8
From page
2159
To page
2166
Abstract
A transient thermal analysis is carried out to verify the base cover thermal protection system of Vega 2nd stage Solid Rocket Motor (SRM) and the flange coupling of the inter-stage 2/3. The analysis is performed with a finite element code. The work has developed suitable numerical Fortran subroutines to assign radiation and convection boundary conditions. The thermal behaviour of the structures is presented.
Keywords
Thermal protection , Finite element analysis , Solid Rocket Motor , Radiation and convection
Journal title
Applied Thermal Engineering
Serial Year
2008
Journal title
Applied Thermal Engineering
Record number
1041737
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