新型航天器刚性太阳电池翼基板的平面度品质控制  

Quality Control of Planeness in New Spacecraft Solar Wing Substrate

作　　者：沃西源[1] 涂彬[1] 殷永霞[1] 谭放[1] 

机构地区：[1]北京空间机电研究所,北京100076

出　　处：《高科技纤维与应用》2009年第1期26-29,33,共5页Hi-Tech Fiber and Application

摘　　要：简介了新型航天器太阳电池翼基板的结构进行,分析了刚性基板制造过程中影响其平面度的主要因素,根据这些影响因素提出了相应的工艺措施,使刚性基板的平面度得到有效控制,为新型航天器成功的经受了多次的飞行试验考验奠定了基础。The paper introduces the structure of the new spacecraft solar sunstrate briefly, and analyzes the major factors which influenced the planeness in the manufacturing process of sunstrate. Some technological processes were found to control the planeness of the rigidity sunstrate bases on the influencing factors. This has become one of the cornerstones of several successes in space flight tests.

关 键 词：太阳电池翼 刚性基板 平面度 品质控制 

分 类 号：V442[航空宇航科学与技术—飞行器设计]