Computational Modeling of Cryogenic Propellant Resupply
Author:
Affiliation:
1. University of Memphis
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2006-984
Reference10 articles.
1. 1Griffin, J.W. "Background and Programmatic Approach for the Development of Orbital Fluid Resupply Tankers,"AIAA-86-1601,Jun.1986.
2. 2Jones,O.S.,Meserole,J.S.,Hedges,D.E.,andSchmidt,G.R."ConceptualDesignoftheSubscaleOrbitalFluid Transfer Experiment(SOFTE),"AIAA-90-2378,Jul.1990.
3. On-orbit cryogenic fluid transfer
4. 4Chato, D.J., and Sanabria, R. "Review and Test of Chilldown Methods for Space-Based Cryogenic Tanks," AIAA-91-1843,Jun.1991.
5. 5Aydellot, J.C., and Rudland, R.S. "Technology Requirements to be Addressed by the NASA Lewis Research Center Cryogenic Fluid ManagementFacility Program," AIAA-85-1229,Jul.1985.
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