QJ 1816-1989 固体火箭发动机位移测量方法
作者:标准资料网 时间:2024-05-05 01:08:01 浏览:9652
来源:标准资料网
基本信息
标准名称: | 固体火箭发动机位移测量方法 |
中标分类: |
航空、航天 >>
航天器及其附件 >>
航天器动力系统 |
替代情况: | 被GJB 2365-1995代替 |
发布日期: | 1989-12-12 |
实施日期: | 1990-06-12 |
首发日期: | |
作废日期: | |
出版日期: | |
页数: | 10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
Product Code:SAE AMS5663
Title:Nickel Alloy, Corrosion and Heat-Resistant, Bars, Forgings, and Rings, 52.5Ni - 19Cr - 3.0Mo - 5.1Cb (Nb) - 0.90Ti - 0.50Al - 19Fe, Consumable Electrode Or Vacuum Induction Melted, 1775 °F (968 °C) Solution and Precipitation Heat Treated
Issuing Committee:Ams F Corrosion Heat Resistant Alloys Committee
Scope: This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.These products have been used typically for parts requiring high resistance to creep and stress-rupture up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), but usage is not limited to such applications.
Rationale: This specification covers a corrosion and heat resistant nickel alloy in the form of bars, forgings, flash welded rings, and stock for forging or flash welded rings.These products have been used typically for parts requiring high resistance to creep and stress-rupture up to 1300 degrees F (704 degrees C) and oxidation resistance up to 1800 degrees F (982 degrees C), but usage is not limited to such applications.【英文标准名称】:StandardTestMethodsforBackingFabricCharacteristicsofPileYarnFloorCoverings
【原文标准名称】:背衬织物的标准试验方法
【标准号】:ASTMD2646-1996
【标准状态】:作废
【国别】:美国
【发布日期】:1996
【实施或试行日期】:
【发布单位】:美国材料与试验协会(ASTM)
【起草单位】:ASTM
【标准类型】:()
【标准水平】:()
【中文主题词】:放大;布;机织物;纺织材料;纺织试验;试验
【英文主题词】:cloth;textiles;testing;amplification;textiletesting;wovenfabrics
【摘要】:
【中国标准分类号】:W04
【国际标准分类号】:59_080_30
【页数】:4P;A4
【正文语种】:英语