| Document Date: 2014-08-25 15:47:33
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City Madrid / San Antonio / Bremen / / Company Flow Science Inc. / / Country Germany / Spain / / / Facility tower ZARM / Southwest Research Institute / / IndustryTerm simulation tools / satellite applications / mechanical energy / in-house software / closed loop simulation tool / house tool / µg applications / internal equipment / software tools / controller algorithm / in-house tools / hot gas thruster models / cold gas / numerical tools / hot gas thrust pulse / linear systems / anti sloshing devices / satellite tanks / steady state solution / visualization tool / / OperatingSystem Windows NT / / Organization Southwest Research Institute / National Aeronautics and Space Administration / / Person Ai / / / Position Angular Rates Controller / controller / active flight controller / / Product Bremen / / ProgrammingLanguage VISUAL BASIC / MATLAB / / ProvinceOrState Texas / / Technology controller algorithm / condensation / simulation / SHARED MEMORY / / URL www.flow3d.com / /
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Space Propulsion 2012 conference 7th-10th May 2012 Bordeaux Modelling of fluid motion in spacecraft propellant tanks - Sloshing N. Fries* ⊗ , P. Behruzi*, T. Arndt*, M. Winter*, G. Netter*, U. Renner* *Astrium Space Tr