STP544: Predicting Spacecraft Multilayer Insulation Performance from Heat Transfer Measurements

    Stimpson, LD
    Member of the Technical Staff, Jet Propulsion Laboratory, California Institute of Technology, Pasadena, Calif.

    Hagemeyer, WA
    senior project engineer, Hugles Aircraft Company, El Segundo, Calif.

    Pages: 10    Published: Jan 1974


    One of the most commonly utilized insulation systems for National Aeronautics and Space Administration spacecraft is multilayer insulation (MLI). The problem of predicting performance of MLI blankets containing discontinuities is described. Design data and test techniques are required which allow correlation of heat leaks through discontinuities with measurable parameters. Some of these design data are obtained using the Jet Propulsion Laboratory's calorimetric testing program.

    New materials and testing approaches will be required for more extreme environments of future spacecraft. Both higher and lower environmental temperatures are anticipated. Insulation performance must meet these demands, at the same time avoiding excessive weight.


    thermal insulation, spacecraft, performance, predictions, tests, discontinuities, calorimeters, high temperature tests, cryogenics, heat transmission

    Paper ID: STP34773S

    Committee/Subcommittee: C16.30

    DOI: 10.1520/STP34773S

    CrossRef ASTM International is a member of CrossRef.