1 |
Robert J. Stochl, Philip A. Masters, Richard L. Dewitt, and Joseph E. Maloy, "Gaseous hydrogen pressurant requirements for the discharge of liquid hydrogen from a 3.96 meter (13 ft) diameter spherical tank", NASA TN D-5387, Aug. 1969
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2 |
Robert J. Stochl, Philip A. Masters, Richard L. Dewitt, and Joseph E. Maloy, "Gaseous hydrogen requirements for the discharge of liquid hydrogen from a 1.52 meter (5 ft) diameter spherical tank", NASA TN D-5336, Aug. 1969
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3 |
Robert J. Stochl, Philip A. Masters, Richard L. Dewitt, and Joseph E. Maloy, "Gaseous helium requirements for the discharge of liquid hydrogen from a 3.96 meter (13 ft) diameter spherical tank", NASA TN D-7019, Dec. 1970
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4 |
Robert J. Stochl, Philip A. Masters, Richard L. Dewitt, and Joseph E. Maloy, "Gaseous helium requirements for the discharge of liquid hydrogen from a 1.52 meter (5 ft) diameter spherical tank", NASA TN D-5621, Jan. 1970
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5 |
William H. Roudebush, "An analysis of the problem of tank pressurizatin during outflow", NASA TN D-2585, Jan. 1965
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6 |
Richard L. Dewitt, Robert J. Stochl, William R. Johnson, "Experimental evaluation of pressurant gas injectors during the pressurized discharge of liquid hydrogen", NASA TN D-3458, 1966
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7 |
Elloit Ring, "Rocket Propellant and Pressurization Systems", Prentice-Hall, Inc., 1964
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8 |
M. Epstein and R. E. Anderson, "An equation for the prediction of cryogenic pressurant requirements for axisymmetric propellant tanks", Advances in cryogenic engineering, Vol. 13, pp. 207-214, 1968
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9 |
Neil T. Van Dresar, "Prediction of pressurant mass requirements for axisymmetric liquid hydrogen tanks", Journal of propulsion and power, Vol. 13, No. 6, pp. 796-799, 1997
DOI
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