MIL-PRF-55182H (AMENDMENT 2)
时间:2024-04-28 17:04:46 来源: 标准资料网 作者:标准资料网 阅读:9400
MIL-PRF-55182H (AMENDMENT 2),PERFORMANCE SPECIFICATION, RESISTORS, FIXED, FILM, NONESTABLISHED RELIABILITY, ESTABLISHED RELIABILITY, AND SPACE LEVEL, GENERAL SPECIFICATION FOR (22 MAR 2007)., This specification covers the general requirements for nonestablished reliability (non-ER), established reliability (ER), and space level that are hermetically or nonhermetically sealed fixed film resistors that have a high degree of stability with respect to time under severe environmental conditions. ER resistors have failure rates (FR) that are established at 60 percent confidence ranging from 0.001 percent per 1,000 hours to 1.0 percent per 1,000 hours.
Product Code:SAE AMSS22141
Title:Steel, Investment Castings Alloy and Carbon (Cancelled Jan 2003)
Issuing Committee:Ams E Carbon And Low Alloy Steels Committee
Scope:This specification covers alloy and carbon steel castings made by the investment precision casting process. (See 6.1).
基本信息
标准名称: | 固体火箭发动机燃烧室壳体内压试验方法 |
英文名称: | Internal-pressure test method for the chamber case of solid rocket motor |
中标分类: |
航空、航天 >>
航天器及其附件 >>
航天器动力系统 |
ICS分类: |
航空器和航天器工程 >>
航空航天发动机和推进系统
|
替代情况: | QJ 1392-1988%QJ 2039-1991 |
发布日期: | 2005-12-12 |
实施日期: | 2006-05-01 |
首发日期: | |
作废日期: | |
出版日期: | |
页数: | 17页 |
适用范围
没有内容
前言
没有内容
目录
没有内容
引用标准
没有内容
所属分类: 航空 航天 航天器及其附件 航天器动力系统 航空器和航天器工程 航空航天发动机和推进系统