Simulation Research of Vaporization and Pressure Variation in a Cryogenic Propellant Tank at the Launch Site
Author:
Publisher
Springer Science and Business Media LLC
Subject
Applied Mathematics,General Physics and Astronomy,General Engineering,Modelling and Simulation
Link
http://link.springer.com/content/pdf/10.1007/s12217-013-9340-2.pdf
Reference11 articles.
1. Barsi, S., Kassemi, M.: Numerical and experimental comparisons of the self-pressurization behavior of an LH2 tank in normal gravity. Cryogenics 48(3–4), 122–129 (2008). doi: 10.1016/j.cryogenics.2008.01.003
2. Barsi, S., Panzarella, C.H., Kassemi, M.: An active vapor approach to modeling pressurization in cryogenic storage tanks. In: 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. Joint Propulsion Conferences. American Institute of Aeronautics and Astronautics (2007)
3. Estey, P.N., Lewis, D.H. Jr., Connor, M.: Prediction of a propellant tank pressure history using state space methods. J. Spacecr. Rocket. 20(1), 49–54 (1983)
4. Kittel, P., Plachta, D.W.: Propellant preservation for mars missions. In: Advances in Cryogenic Engineering, vol. 45. Springer (2000)
5. Knuth, E.: Non stationary phase changes involving a condensed phase and a saturated vapor. Phys. Fluids 1(2), 84–86 (1959)
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