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Thermal Analysis of the X-38 Aft Fin During Re-EntryThis document contains the details of the thermal analysis of the X-38 aft fin during re-entry. This analysis was performed in order to calculate temperature response of the aft fin components. This would be provided as input to a structural analysis and would also define the operating environment for the electromechanical actuator (EMA). The calculated structural temperature response would verify the performance of the thermal protection system (TPS). The geometric representation of the aft fin was derived from an I-DEAS finite element model that was used for structural analysis. The thermal mass network model was derived from the geometric representation.
Document ID
20000025393
Acquisition Source
Johnson Space Center
Document Type
Conference Paper
Authors
Hong, Andrew E.
(NASA Johnson Space Center Houston, TX United States)
Date Acquired
August 19, 2013
Publication Date
November 1, 1999
Publication Information
Publication: Ninth Thermal and Fluids Analysis Workshop Proceedings
Subject Category
Aerodynamics
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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