Cryogenic Tank Modeling for the Saturn AS-203 Experiment

Author:

Grayson Gary,Lopez Alfredo,Chandler Frank,Hastings Leon,Tucker Stephen

Publisher

American Institute of Aeronautics and Astronautics

Reference11 articles.

1. 2Mikelis,N.E.,Miller,J.K.,andTaylor,K.V."SloshinginPartiallyFilledLiquidTanksanditsEffectonShip Motions: Numerical Simulationsand Experimental Verification," Royal InstitutionofNaval Architects, Spring Meetings, Paper No. 7,London, 1984.

2. 3Sicilian,J.M.andTegart,J.R."ComparisonofFLOW-3DCalculationswithVeryLargeAmplitudeSlosh Data," ASME Pressure Vesselsand Piping Conference, Vol.176,pp.23-30,1989.

3. 5Grayson,G.,andDiStefano,E."PropellantAcquisitionforSingle-StageRocketTechnology,"29th AIAA/SAE/ASME/ASEE Joint PropulsionConference, Paper 93-2283, Monterey, CA, June 1993.

4. Coupled thermodynamic-fluid-dynamic solution for a liquid-hydrogen tank

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