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Self automorphic characteristic convex condition cover null for space ship

机译:宇宙飞船的自同构特征凸条件覆盖为空

摘要

PURPOSE: To provide a cover for spacecraft unit, in which sunlight is not converted on a spacecraft, which has self-holding property in a convex shape, which is thin and light, whose manufacture and fitting area easy and which is transparent to a radio frequency. ;CONSTITUTION: A cover 10 has a convex dome 12 having a first plurality of ribs 1 and a second plurality of parallel ribs 16. The ribs self-hold the dome in a convex shape. Drawstrings 32 fitted at the mooring points 34 of a unit are inserted at the peripheral part and the cover is fitted to the unit. A cover material is made into a layup body containing a conduction layer and a thermal control layer and the conduction layer is a semiconductor like germanium.;COPYRIGHT: (C)1994,JPO
机译:目的:提供用于航天器单元的盖,该罩在其中太阳光不会在航天器上转换,该罩具有呈凸形的自保持特性,该罩既薄又轻,其制造和装配区域容易,并且对无线电透明频率。组成:盖子10具有凸形圆顶12,该凸圆顶12具有多个第一肋1和多个第二平行肋16。这些肋将圆顶自动保持为凸形。装配在单元的系泊点34处的拉绳32被插入到外围部分,并且盖被装配至该单元。将覆盖材料制成包含导电层和热控制层的叠层体,并且该导电层是诸如锗的半导体。; COPYRIGHT:(C)1994,JPO

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