HB 3796-1986 铆钉窝锪钻 用于１２０°沉头铆钉
作者:标准资料网 时间:2024-05-09 13:10:19 浏览:8081
来源:标准资料网
基本信息
| 标准名称： | 铆钉窝锪钻 用于１２０°沉头铆钉 |
| 中标分类： |
航空、航天 >>
航空器与航天器制造用设备 >>
工具 |
| 发布日期： | 1986-07-14 |
| 实施日期： | 1986-10-01 |
| 首发日期： | 1900-01-01 |
| 作废日期： | 1900-01-01 |
| 出版日期： | 1900-01-01 |
| 页数： | 2页 |
适用范围
没有内容
前言
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目录
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引用标准
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所属分类： 航空 航天 航空器与航天器制造用设备 工具
基本信息
| 标准名称： | 水利部机关各单位名称代码 |
| 中标分类： |
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| 发布日期： | 1997-08-22 |
| 实施日期： | 1996-10-01 |
| 首发日期： | |
| 作废日期： | |
| 出版日期： | |
| 页数： | 2页 |
适用范围
没有内容
前言
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目录
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引用标准
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所属分类：
MIL-HDBK-336-1, MILITARY HANDBOOK SURVIVABILITY, AIRCRAFT, NONNUCLEAR, GENERAL CRITERIA (VOLUME 1) (25 OCT 1982)., This is the first volume in a four-volume design handbook for nonnuclear survivability of military aircraft. Each volume is structured to be used in conjunction with the other three volumes, as needed, in the design process. This volume contains general information pertaining to vulnerability and survivability analysis techniques, weapon terminal effects, computer program descriptions, and basic subsystem design concepts. Volume 1 is arranged in a manner that allows the user to easily identify the specific information of interest. APPLICATION: The data contained in this design handbook have been arranged to support the development of both fixed and rotary wing military aircraft. Each has unique mission and performance characteristics that require specialized attention and design solutions. The subystem design categories have been established with these considerations in mind. For example, the power train and rotor blade subsystems deal primarily with military helicopter applications, while the launch/recovery systems deal with those subsystem elements for both fixed and rotary wing aircraft landing gear systems and for those systems related to the assisted takeoff (launching) and deceleration (recovery) methods most used by the Air Force and Navy fixed-wing aircraft.
