【英文标准名称】:Connectorswithassessedquality,foruseind.c.,low-frequencyanalogueandindigitalhigh-speeddataapplications-Part3:Rectangularconnectors-Section101:Detailspecificationforarangeofshieldedconnectorswithtrapezoidalshapedshellsand
【原文标准名称】:有质量评定的直流低频模拟及数字高速数据应用系统用连接器第3部分:矩形连接器第101节:在1.27mm×2.54mm中心线上不可拆卸矩形接触件及梯形外壳的屏蔽系列连接器详细规范
【标准号】:IEC61076-3-101-1997
【标准状态】:现行
【国别】:国际
【发布日期】:1997-08
【实施或试行日期】:
【发布单位】:国际电工委员会(IX-IEC)
【起草单位】:IEC/SC48B
【标准类型】:()
【标准水平】:()
【中文主题词】:插接件连接;矩形连接器;尺寸;试验;电气工程;屏蔽的;电插头;规范;详细规范;直流电压;音频系统
【英文主题词】:Assessedreliability;Audiosystems;Backpanels;Connectoredjoints;Detailspecification;Dimensions;Directvoltage;Direct-currentsystem;Electricplugs;Electricalengineering;Electronicequipmentandcomponents;Lowfrequencies;Printedcircuits;Rectangularconnectors;Shielded;Shieldedcables;Specification;Testing
【摘要】:Connectorswithassessedquality,foruseind.c,low-frequencyanalogueandindigitalhigh-speeddataapplications-Part3:Rectangularconnectors-Section101:Detailspecificationforarangeofshieldedconnectorswithtrapezoidalshapedshellsandnon-removablerectangularcontactsona1,27mmx2,54mmcentre-lineGeneraldataTechnicaldataDimensionalinformation.Characteristics.TestscheduleQualityassessmentprocedures.
【中国标准分类号】:L23
【国际标准分类号】:31_220_10
【页数】:125P.;A4
【正文语种】:英语


MIL-HDBK-2066, DEPARTMENT OF DEFENSE HANDBOOK: CATAPULTING AND ARRESTING GEAR FORCING FUNCTIONS FOR AIRCRAFT STRUCTURAL DESIGN (07 MAR 1999) [SUPERSEDING MIL-STD-2066]., This document summarizes loads, accelerations, velocities, and other parameters statistically analyzed and extracted from test data representative of the various shipboard and shore based launching and recovery equipment employed by the U.S. Navy. In determining the volume of information to be presented, every effort has been made to condense the data and yet present it, as much as possible, in a form that requires the least amount of additional calculations by the user. The data shown herein may be used to derive time histories of loads and accelerations for the design conditions of MIL-A-8863 "Airplane Strength and Rigidity, Ground Loads for Navy Procured Airplanes” and MIL-A-8866 "Airplane Strength and Rigidity, Reliability Requirements, Repeated Loads9 and Fatigue.” Source: