Foam Core Shielding for Spacecraft
NASA’s Jet Propulsion Laboratory, Pasadena, California
Saturday, December 01 2007
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A foam core shield (FCS) system is now being developed to supplant multilayer insulation (MLI) systems heretofore installed on spacecraft for thermal management and protection against meteoroid impacts. A typical FCS system consists of a core sandwiched between a face sheet and a back sheet. The core can consist of any of a variety of low-to- medium-density polymeric or inorganic foams chosen to satisfy application-specific requirements regarding heat transfer and temperature.
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