SAE AMS4078 Aluminum Alloy Sheet and Plate, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, 7075: (-T73 Sheet, -T7351 Plate), Solution H
时间:2024-05-09 11:15:11 来源: 标准资料网 作者：标准资料网 阅读：9113
Product Code:SAE AMS4078
Title:Aluminum Alloy Sheet and Plate, 5.6Zn - 2.5Mg - 1.6Cu - 0.23Cr, 7075: (-T73 Sheet, -T7351 Plate), Solution Heat Treated and Overaged
Issuing Committee:Ams D Nonferrous Alloys Committee
Scope:This specification covers an aluminum alloy in the form of sheet and plate.
- 上一篇：SAE AMS2303 Steel Cleanliness, Aircraft Quality, Martensitic Corrosion-Resistant Steels, Magnetic Particle Inspection Pr
- 下一篇：SAE AMS4115 Aluminum Alloy, Rolled or Cold-Finished, Bars, Rods, Wire, and Flash Welded Rings, Annealed, 1.0Mg - 0.60Si
【英文标准名称】:ElectromagneticcompatibilityandRadiospectrumMatters(ERM)-ShortRangeDevices-RoadTransportandTrafficTelematics(RTTT)-ShortRangeRadarequipmentoperatinginthe77GHzto81GHzband-Part1:Technicalrequirementsandmethodsofmeasure
【原文标准名称】:电磁兼容性和射频频谱情况(ERM).短程设备.公路运输和交通远程通讯(RTTT).在77GHz至81GHz波段运行的短程雷达设备.第1部分:测量的技术要求和方法(英文版本EN302264-1V1.1.1(2009-06)的核准本作为德国标准)
【标准号】:DINEN302264-1-2009
【标准状态】:现行
【国别】:德国
【发布日期】:2009-10
【实施或试行日期】:
【发布单位】:德国标准化学会(DE-DIN)
【起草单位】:
【标准类型】:()
【标准水平】:()
【中文主题词】:电气工程;电磁兼容性;电磁兼容性(EMC);抗干扰度;干扰辐射;测量;测量技术;雷达设备;无线电装置;无线电系统;无线电报;道路运输;规范(验收);电讯;电信;远程信息管理;交通管制;运输工程
【英文主题词】:Electricalengineering;Electromagneticcompatibility;EMC;Interferencerejections;Interferingemissions;Measurement;Measuringtechniques;Radarequipment;Radioplants;Radiosystems;Radiotelegraphy;Roadtransport;Specification(approval);Telecommunication;Telecommunications;Telematics;Trafficcontrol;Transportengineering
【摘要】:
【中国标准分类号】:L06
【国际标准分类号】:33_060_20
【页数】:2P.;A4
【正文语种】:德语
MIL-DTL-27422D, DETAIL SPECIFICATION FOR THE TANK, FUEL, CRASH-RESISTANT, BALLISTIC-TOLERANT, AIRCRAFT (30 JAN 2007) [SUPERSEDING MIL-T-27422B(1)]., This specification covers the requirements and verification testing forcrash-resistant, ballistic-tolerant fuel cell for use in rotorcraft and tilt rotorcraft. Exactdesign criteria such as fuel cell dimensions, total weight, and interface requirements willbe dependent upon the intended aircraft specified in the contract or purchase order.