1) Conical shell of missile
导弹锥壳
2) missile nose
导弹头锥
1.
The paper briefly presents the monomers for polyarylacetylene and their synthesis, resins and the polymerization and discusses the application prospect to the solid rocket motor, missile nose and spacecraft.
本文概要介绍了聚芳基乙炔所用单体、合成及树脂聚合机理,讨论了在固体火箭发动机喷管、导弹头锥以及航天飞行器等材料中的应用前景。
4) missile engine case
导弹发动机壳体
5) conical shell
锥壳
1.
Through the analysis of material layout and lofting process for conical shell,the relevant equations were derived.
通过分析锥壳放样排料的过程,推导出锥壳放样排料的有关公式。
2.
Natural frequencies and damping ratios of a conical shell with honeycomb construction are identified by modal experiment.
通过模态试验对蜂窝结构锥壳结构的纵向固有频率和阻尼比进行了识别,并与数值仿真结果进行了对比。
3.
This paper is concerned with the free vibration analysis of conical shell on the two-parameter elastic foundation.
本文研究双参数弹性地基上锥壳的自由振动问题，并计及地基惯性作用。
补充资料：MX导弹(见“和平卫士”导弹)
MX导弹(见“和平卫士”导弹)
MX missile
MX daodanMx导弹(Mx mis、ix。)见“和平卫士”导弹。
说明：补充资料仅用于学习参考，请勿用于其它任何用途。
参考词条