摘要
本文介绍应用于卫星的碳/环氧波纹壳代号8509研制情况。研制的产品经试验表明,所采用的材料和制造技术是先进的,主要力学性能超出2914波纹壳的性能。
The development of carbon/epoxy corrugated cylinder (codeNo 8509) for satellite application are presented. Tests show that the materi-als and techniques adopted are advanced and the mechanical properties of8509 are superior to that of 2914.
出处
《宇航材料工艺》
CAS
CSCD
北大核心
1993年第3期29-33,共5页
Aerospace Materials & Technology
