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Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
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Guarded electrical cylindrical calorimeter measuring multilayer insulation thermal conductivity, discussing construction, test and error
Gas pressure differential across multilayer insulation blanket during rapid evacuation predicted, using one dimensional flow theory
Technique produces high resolution cross-sectional radiographs with close interplane spacing for inspecting multilayer boards to be used in providing circuitry routing and module structural support.
Users manual for FORTRAN 4 computer program for analysis of multilayered fiber composites
Thermal analysis of space hold performance of multilayer insulation on upper half of unshrouded liquid hydrogen tank within sun oriented vehicle
Multilayer porous refractory metal ionizer design with thick, porous, large-grain substrates and thin, porous micron-grain substrates
Composite multilayer insulation system of double goldized, Nylar radiation shields
Heat flux and optical property measurement for multilayer insulation
Space-hold thermal analysis of oblate spheroid tank mounted multilayer insulation configurations by computer including programs
Thermal cycling tests of ground and space liquid hydrogen storage tank heat shielding with multilayer, purged substrate, thermal insulation blankets
Multilayer insulation panels for cryogenic liquid containers
Self evacuating multilayer insulation system of aluminized Mylar and polyurethane foam for liquid hydrogen tanks
Transient thermal performance of multilayer insulation systems with liquid hydrogen tank during simulated Saturn 5 ascent pressure decay
Thermal analysis of electrical cylindrical calorimeter used for multilayer insulation thermal conductivity tests - Vol. 1
Empirical analysis of thermophysical properties of multilayer insulation composite materials for cryogenic storage equipment - Vol. 2
Outgassing of multilayer insulation materials for use in cryogenic fuel tanks
Lateral heat transfer measurements in cryogenic multilayer insulation, considering effective thermal conductivity
A summary is presented of the work performed by Marshall Space Flight Center (MSFC) and industry toward the development of flight-type multilayer insulation(MLI) systems. The MSFC MLI program is divided into three large categories: (1) the generation and compilation of MLI composite test data; (2) the analysis, design, and testing of heat flow through MLI applied to ducting, seams, electrical feedthroughs, structural supports, and the tank sidewall; and (3) the development, modification, and utilization of new testing procedures, tanks, and the test facilities. Numerous data have been generated, analyzed, and documented on different MLI composites.