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Computational modeling of nonlinear propellant sloshing for spacecraft AOCS applications

Crossref DOI link: https://doi.org/10.1007/s12567-018-0216-6

Published Online: 2018-08-01

Published Print: 2018-09

Update policy: https://doi.org/10.1007/springer_crossmark_policy

Authors

Hahn, Manuel https://orcid.org/0000-0001-6207-2382
Adami, Stefan

Förstner, Roger
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Text and Data Mining valid from 2018-08-01
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Article History

Received: 8 October 2017

Revised: 22 July 2018

Accepted: 24 July 2018

First Online: 1 August 2018