Insulated reentry heat shield

摘要: The present invention discloses an insulated reentry heat shield for minimizing transfer to a spacecraft structure or the like during atmospheric reentry. ( 10 ) comprises outer resistant layer 12 including ablative first material backed by inner insulating 14 second material. and layers 12, are bonded one another middle 16 disposed therebetween. is formed disposing at least of phenolic loaded third between heating all three simultaneously remove volatiles from layer. In embodiment, carbon-carbon, carbon foam, scrim cloth. also method use in constructing shield. includes steps preparing comprised attaching attached cloth felt layer, layer(s) material,