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Electromagnetic Launch Vehicle Fairing and Acoustic Blanket Model of Received Power Using FEKO

Author
Trout, Dawn H.
Published
March 27, 2011.
Physical Description
1 electronic document
Additional Creators
Wahid, Parveen F. and Stanley, James E.
Online Version

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Unclassified, Unlimited, Publicly available.
Free-to-read Unrestricted online access
Summary
Evaluating the impact of radio frequency transmission in vehicle fairings is important to sensitive spacecraft. This paper employees the Multilevel Fast Multipole Method (MLFMM) feature of a commercial electromagnetic tool to model the fairing electromagnetic environment in the presence of an internal transmitter. This work is an extension of the perfect electric conductor model that was used to represent the bare aluminum internal fairing cavity. This fairing model includes typical acoustic blanketing commonly used in vehicle fairings. Representative material models within FEKO were successfully used to simulate the test case.
Other Subject(s)
Collection
NASA Technical Reports Server (NTRS) Collection.
Note
Document ID: 20110000495.
KSC-2011-051R.
KSC-2010-276.
Applied Computational Electromagnetics Society; 27-31 Mar. 2011; Williamsburg, VA; United States.
Terms of Use and Reproduction
Copyright, Distribution as joint owner in the copyright.
View MARC record | catkey: 15993062