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BS 2782 Method 631A-1993 塑料的试验方法.第6部分:尺寸性能.试验方法631A:挠性薄片重量厚度与屈服点的测定

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【英文标准名称】:Methodsoftestingplastics.Dimensionalproperties.Determinationofgravimetricthicknessandyieldofflexiblesheet
【原文标准名称】:塑料的试验方法.第6部分:尺寸性能.试验方法631A:挠性薄片重量厚度与屈服点的测定
【标准号】:BS2782Method631A-1993
【标准状态】:作废
【国别】:英国
【发布日期】:1993-03-15
【实施或试行日期】:
【发布单位】:英国标准学会(BSI)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:辊子;厚度测量;柔性材料;膜(物态);凸形的;重量测量;塑料;高聚物;试样;试验条件;薄板材
【英文主题词】:polymers;films(statesofmatter);testingconditions;thicknessmeasurement;embossed;rolls;plastics;testspecimens;flexiblematerials;sheetmaterials;weightmeasurement
【摘要】:
【中国标准分类号】:G31
【国际标准分类号】:
【页数】:6P;A4
【正文语种】:英语


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【英文标准名称】:Pulsesinbags;Sampling
【原文标准名称】:袋装豆类.取样
【标准号】:ISO951-1979
【标准状态】:作废
【国别】:国际
【发布日期】:1979-09
【实施或试行日期】:
【发布单位】:国际标准化组织(ISO)
【起草单位】:ISO/TC34
【标准类型】:()
【标准水平】:()
【中文主题词】:抽样表;抽样方法;质量管理;豆类;豆科作物;加标签;采样设备;装货;抽样;农产品
【英文主题词】:sampling;qualitycontrol;baggeddelivery;leguminousgrains;pulses(crops);samplingtables;labelling(process);agriculturalproducts;labelling;samplingequipment;samplingmethods
【摘要】:
【中国标准分类号】:B20
【国际标准分类号】:0520;5706
【页数】:6P;A4
【正文语种】:英语


MIL-HDBK-336-3, MILITARY HANDBOOK SURVIVABILITY, AIRCRAFT, NONNUCLEAR, GENERAL CRITERIA (VOLUME 3) (4 FEB 1983)., 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. The objective of Volume 3 is to provide a ready reference containing design information on military aircraft engine and propulsion system survivability. It contains data on design-techniques to reduce visual, infrared, radar, and aural detectability; and projectile and high-energy laser vulnerability of military aircraft engines and engine installations. The design techniques discussed ranged from combat- and test- proven systems, through development, laboratory, and breadboard equipment, to undeveloped concepts. Turbine engines are stressed, but piston engines are also presented. 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.