Books on the topic 'Cryogenic tank'
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E, Lake R., Wilkerson C, and George C. Marshall Space Flight Center., eds. Unlined reusable filament wound composite cryogenic tank testing. National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.
Find full textE, Lake R., Wilkerson C, and George C. Marshall Space Flight Center., eds. Unlined reusable filament wound composite cryogenic tank testing. National Aeronautics and Space Administration, Marshall Space Flight Center, 1999.
Find full textUnited States. National Aeronautics and Space Administration., ed. Tank pressure control in low gravity by jet mixing. National Aeronautics and Space Administration, 1993.
Find full text1963-, Stephens Craig A., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Predicted thermal response of a cryogenic fuel tank exposed to simulated aerodynamic heating profiles with different cryogens and fill levels. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Find full textE, Anton C., and Langley Research Center, eds. Low cost, SPF aluminum cryogenic tank structure for ALS. National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Numerical modeling of a cryogenic fluid within a fuel tank. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
Find full textJ, Hanna Gregory, and Hugh L. Dryden Flight Research Center., eds. Thermal modeling and analysis of a cryogenic tank design exposed to extreme heating profiles. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1991.
Find full textJ, Hanna Gregory, and Hugh L. Dryden Flight Research Center., eds. Thermal modeling and analysis of a cryogenic tank design exposed to extreme heating profiles. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1991.
Find full textCarl, Bouvier, and United States. National Aeronautics and Space Administration., eds. X-33/RLV: Reusable cryogenic tank VHM using fiber optic distributed sensing technology. National Aeronautics and Space Administration, 1998.
Find full textCarl, Bouvier, and United States. National Aeronautics and Space Administration., eds. X-33/RLV: Reusable cryogenic tank VHM using fiber optic distributed sensing technology. National Aeronautics and Space Administration, 1998.
Find full textCarl, Bouvier, and United States. National Aeronautics and Space Administration., eds. X-33/RLV: Reusable cryogenic tank VHM using fiber optic distributed sensing technology. National Aeronautics and Space Administration, 1998.
Find full textKo, William L. Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heating. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
Find full textKo, William L. Thermocryogenic buckling and stress analyses of a partially filled cryogenic tank subjected to cylindrical strip heating. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
Find full textS, Greenberg H., Johnson S. E, and United States. National Aeronautics and Space Administration., eds. Reusable LH2 tank technology demonstration through ground test. National Aeronautics and Space Administration, 1995.
Find full textFacility, Dryden Flight Research, ed. Thermal-fluid analysis of the fill and drain operations of a cryogenic fuel tank. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1993.
Find full textFacility, Dryden Flight Research, ed. Thermal-fluid analysis of the fill and drain operations of a cryogenic fuel tank. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1993.
Find full textRivers, H. Kevin. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textCenter, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textCenter, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textCenter, Langley Research, ed. Cyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textFacility, Dryden Flight Research, ed. Thermal-fluid analysis of the fill and drain operations of a cryogenic fuel tank. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1993.
Find full textFacility, Dryden Flight Research, ed. Thermal-fluid analysis of the fill and drain operations of a cryogenic fuel tank. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1993.
Find full textChato, David J. Ground testing for the no-vent fill of cryogenic tanks: Results of tests for a 71 cubic foot tank. National Aeronautics and Space Administration, 1993.
Find full textR, Jan, and Langley Research Center, eds. A fundamental study of laser beam welding aluminum-lithium alloy 2195 for cryogenic tank applications. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textP, Stanton W., and George C. Marshall Space Flight Center., eds. A new aging treatment for improving cryogenic toughness of the main structural alloy of the super lightweight tank. National Aeronautics and Space Administration, Marshall Space Flight Center, 1996.
Find full textJ, Russ Edwin, Wachter Joseph P, and United States. National Aeronautics and Space Administration., eds. Cryogenic on-orbit liquid depot storage, acquisition, and transfer satellite (COLD-SAT): Feasibility study final report. National Aeronautics and Space Administration, 1990.
Find full textJ, Russ Edwin, Wachter Joseph P, and United States. National Aeronautics and Space Administration., eds. Cryogenic on-orbit liquid depot storage, acquisition, and transfer satellite (COLD-SAT): Feasibility study final report. National Aeronautics and Space Administration, 1990.
Find full textDresar, Neil T. Van. Pressurization and expulsion of cryogenic liquids: Generic requirements for a low-gravity experiment. National Aeronautics and Space Administration, 1991.
Find full textCenter, Langley Research, ed. Bonding and sealing evaluations for cryogenic tanks. National Aeronautics and Space Administration, Langley Research Center, 1997.
Find full textChato, David J. Review and test of chilldown methods for space-based cryogenic tanks. National Aeronautics and Space Administration, 1991.
Find full textDresar, Neil T. Van. Thermodynamic models for bounding pressurant mass requirements of cryogenic tanks. National Aeronautics and Space Administration, 1993.
Find full textF, Johnson Theodore, and United States. National Aeronautics and Space Administration., eds. Thermal structures technology development for reusable launch vehicle cryogenic propellant tanks. National Aeronautics and Space Administration, 1998.
Find full textF, Johnson Theodore, and United States. National Aeronautics and Space Administration., eds. Thermal structures technology development for reusable launch vehicle cryogenic propellant tanks. National Aeronautics and Space Administration, 1998.
Find full textGeorge C. Marshall Space Flight Center., ed. Evaluation of microcracking in two carbon-fiber/epoxy-matrix composite cryogenic tanks. National Aeronautics and Space Administration, Marshall Space Flight Center, 2001.
Find full textUnited States. National Aeronautics and Space Administration., ed. Preliminary thermal design of the COLD-SAT Spacecraft. National Aeronautics and Space Administration, 1991.
Find full textTimothy, Martin, Hodgson Ed, and United States. National Aeronautics and Space Administration., eds. Extended mobility unit subcritical liquid oxygen storage and supply system (EMU SLOSSS): Conceptual design study report. Martin Marietta, Civil Space and Communications Company, 1992.
Find full textLin, Chin-Shun. Numerical investigation of the thermal stratification in cryogenic tanks subjected to wall heat flux. National Aeronautics and Space Administration, 1990.
Find full textChato, David J. Ground testing on the nonvented fill method of orbital propellant transfer: Results of initial test series. National Aeronautics and Space Administration, 1991.
Find full textUnited States. National Aeronautics and Space Administration., ed. Test plan, task 5, subtask 5.2, early on-orbit TPS debris impact tests. Rockwell Aerospace, Space Systems Division, 1994.
Find full textA, Talay Theodore, Austin R. Eugene, and United States. National Aeronautics and Space Administration., eds. Reusable Launch Vehicle Technology Program. American International Astronautical Federation, 1996.
Find full textJ, Birt M., and Langley Research Center, eds. Characterization of Al-Cu-Li alloy 2090 near net shape extrusion. National Aeronautics and Space Administration, Langley Research Center, 1998.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Unlined Reuseable Filament Wound Composite Cryogenic Tank Testing. Independently Published, 2018.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Unlined Reuseable Filament Wound Composite Cryogenic Tank Testing. Independently Published, 2018.
Find full textHybrid thermal control testing of a cryogenic propellant tank. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Find full textNumerical modeling of a cryogenic fluid within a fuel tank. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Debonding Stress Concentrations in a Pressurized Lobed Sandwich-Walled Generic Cryogenic Tank. Independently Published, 2018.
Find full textTesting of densified liquid hydrogen stratification in a scale model propellant tank. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textCyclic cryogenic thermal-mechanical testing of an X-33/RLV liquid oxygen tank concept. National Aeronautics and Space Administration, Langley Research Center, 1999.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Cyclic Cryogenic Thermal-Mechanical Testing of an X-33/Rlv Liquid Oxygen Tank Concept. Independently Published, 2018.
Find full textNational Aeronautics and Space Administration (NASA) Staff. Pressure-Volume-Temperature (Pvt) Gauging of an Isothermal Cryogenic Propellant Tank Pressurized with Gaseous Helium. Independently Published, 2019.
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