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Simulation of the behavior of a payload fairing during separation
KTH, School of Engineering Sciences (SCI), Mechanics.
2013 (English)Independent thesis Advanced level (degree of Master (Two Years)), 20 credits / 30 HE creditsStudent thesisAlternative title
Simulering av beteendet hos en nyttolastk├ąpa under separation (Swedish)
Abstract [en]

The present paper describes the development of a finite element based tool at the launcher directorate of theFrench Space Agency (CNES) in order to support the ground study and testing of fairing separation systems.The main topic is the finite element modeling process and its validation. The considered finite element methodsand resolution algorithms are presented, with a focus on shell element formulations in the used finite elementpackages. The model results are compared with those obtained for a separation system with a pre-existing modeland a ground test. The developed model shows good agreement with the reference results and enables the CNESto fulfill its technical support role.

Place, publisher, year, edition, pages
2013. , p. 17
National Category
Engineering and Technology
Identifiers
URN: urn:nbn:se:kth:diva-202622OAI: oai:DiVA.org:kth-202622DiVA, id: diva2:1078063
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Available from: 2017-03-02 Created: 2017-03-02 Last updated: 2017-03-02Bibliographically approved

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  • apa
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Output format
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