| 摘要 |
FIELD: astronautics.SUBSTANCE: invention relates to heat insulation of spacecraft. Spacecraft thermal blanket consists of alternating layers formed non-flat polymer film with single or double-sided sputtering of metal, for example aluminium, and polymer network on which can be applied hot-melt adhesive. Polymers used as for making films and for making net include polyester, polyimide, aramid, arimid.EFFECT: low heat conductivity and total weight of heat insulation.1 cl, 6 dwg, 2 tbl |
