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一种机载导弹舱体内隔热层快速成型技术

肖军 程功 赵融 魏仲委

航空兵器Issue(3):83-87,5.
航空兵器Issue(3):83-87,5.DOI:10.19297/j.cnki.41-1228/tj.2018.03.015

一种机载导弹舱体内隔热层快速成型技术

Rapid Forming Technology of Heat Insulation Coating on Inner-Wall for Airborne Missiles

肖军 1程功 1赵融 1魏仲委1

作者信息

  • 1. 中国空空导弹研究院,河南洛阳 471009
  • 折叠

摘要

Abstract

Thermal protective measures must be applied to safeguard regular work for precision com-ponents,assemblys,and apparatus of an airborne missile from overheat during supersonic and hypersonic speed flight.In this paper,a rapid forming technology for heat insulation coatig on inner-wall of airborne missile's cabins is discussed.The forming technology is suited for airborne missile projects engineering development,with small number,multi-batchs,quick and flexible characteristics,as well as large scale production.

关键词

机载导弹/隔热/成型技术/热防护

Key words

airborne missile/heat insulation/forming technology/thermal protection

分类

军事科技

引用本文复制引用

肖军,程功,赵融,魏仲委..一种机载导弹舱体内隔热层快速成型技术[J].航空兵器,2018,(3):83-87,5.

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