摘要
越南战争的经验表明,虽然直升机的战场损失率仅为1.2架/万架次,低于固定翼飞机,但是其驾驶员死亡绝对数却相当高。这引起了军方对直升机乘员生存保护,特别是适坠毁生存设计和要求研究的高度重视。最先是美国陆航于1967年编制出版了《飞机适坠毁生存设计指南》(下简称《指南》)。
Anti-crach standard of military helicopter had being reseached since 1960s by US Army Aviation and it also was improved constantly. The last MIL-STD-1290A(AV) was set in 1988. The background and major contents of the research are introduced here.
出处
《国际航空》
北大核心
1994年第1期34-35,共2页
International Aviation
