{"version":"1.0","provider_name":"\u898f\u683c\u30de\u30b9\u30bf\u30fc","provider_url":"https:\/\/kikakumaster.com\/ja\/","author_name":"KikakuAdmin000","author_url":"https:\/\/kikakumaster.com\/ja\/author\/kikakuadmin000\/","title":"MIL-STD-1542 - Electromagnetic Compatibility and Grounding Requirements for Space System Facilities - \u898f\u683c\u30de\u30b9\u30bf\u30fc","type":"rich","width":600,"height":338,"html":"<blockquote class=\"wp-embedded-content\" data-secret=\"cdmJwhrqVS\"><a href=\"https:\/\/kikakumaster.com\/ja\/mil-spec\/mil-std-1542\/\">MIL-STD-1542 &#8211; Electromagnetic Compatibility and Grounding Requirements for Space System Facilities<\/a><\/blockquote><iframe sandbox=\"allow-scripts\" security=\"restricted\" src=\"https:\/\/kikakumaster.com\/ja\/mil-spec\/mil-std-1542\/embed\/#?secret=cdmJwhrqVS\" width=\"600\" height=\"338\" title=\"&#8220;MIL-STD-1542 &#8211; Electromagnetic Compatibility and Grounding Requirements for Space System Facilities&#8221; &#8212; \u898f\u683c\u30de\u30b9\u30bf\u30fc\" data-secret=\"cdmJwhrqVS\" frameborder=\"0\" marginwidth=\"0\" marginheight=\"0\" scrolling=\"no\" class=\"wp-embedded-content\"><\/iframe><script type=\"text\/javascript\">\n\/* <![CDATA[ *\/\n\/*! This file is auto-generated *\/\n!function(d,l){\"use strict\";l.querySelector&&d.addEventListener&&\"undefined\"!=typeof URL&&(d.wp=d.wp||{},d.wp.receiveEmbedMessage||(d.wp.receiveEmbedMessage=function(e){var t=e.data;if((t||t.secret||t.message||t.value)&&!\/[^a-zA-Z0-9]\/.test(t.secret)){for(var s,r,n,a=l.querySelectorAll('iframe[data-secret=\"'+t.secret+'\"]'),o=l.querySelectorAll('blockquote[data-secret=\"'+t.secret+'\"]'),c=new RegExp(\"^https?:$\",\"i\"),i=0;i<o.length;i++)o[i].style.display=\"none\";for(i=0;i<a.length;i++)s=a[i],e.source===s.contentWindow&&(s.removeAttribute(\"style\"),\"height\"===t.message?(1e3<(r=parseInt(t.value,10))?r=1e3:~~r<200&&(r=200),s.height=r):\"link\"===t.message&&(r=new URL(s.getAttribute(\"src\")),n=new URL(t.value),c.test(n.protocol))&&n.host===r.host&&l.activeElement===s&&(d.top.location.href=t.value))}},d.addEventListener(\"message\",d.wp.receiveEmbedMessage,!1),l.addEventListener(\"DOMContentLoaded\",function(){for(var e,t,s=l.querySelectorAll(\"iframe.wp-embedded-content\"),r=0;r<s.length;r++)(t=(e=s[r]).getAttribute(\"data-secret\"))||(t=Math.random().toString(36).substring(2,12),e.src+=\"#?secret=\"+t,e.setAttribute(\"data-secret\",t)),e.contentWindow.postMessage({message:\"ready\",secret:t},\"*\")},!1)))}(window,document);\n\/\/# sourceURL=https:\/\/kikakumaster.com\/wp-includes\/js\/wp-embed.min.js\n\/* ]]> *\/\n<\/script>\n","description":"Electromagnetic Compatibility and Grounding Requirements for Space System Facilities - The purpose of this standard is to specify the design, performance, and verification requirements for electrical subsystems for space system facilities, including electromagnetic compatibility (EMC), electrical power, grounding, bonding, shielding, lightning protection, and TEMPEST security. These requirements are interrelated and interdependent, and therefore require an integrated approach in the design.."}