{"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-HDBK-1791 - Designing for Internal Aerial Delivery in Fixed Wing Aircraft (S\/S by MIL-STD-1791) - \u898f\u683c\u30de\u30b9\u30bf\u30fc","type":"rich","width":600,"height":338,"html":"<blockquote class=\"wp-embedded-content\" data-secret=\"ZSfOqFBE32\"><a href=\"https:\/\/kikakumaster.com\/ja\/mil-spec\/mil-hdbk-1791\/\">MIL-HDBK-1791 &#8211; Designing for Internal Aerial Delivery in Fixed Wing Aircraft (S\/S by MIL-STD-1791)<\/a><\/blockquote><iframe sandbox=\"allow-scripts\" security=\"restricted\" src=\"https:\/\/kikakumaster.com\/ja\/mil-spec\/mil-hdbk-1791\/embed\/#?secret=ZSfOqFBE32\" width=\"600\" height=\"338\" title=\"&#8220;MIL-HDBK-1791 &#8211; Designing for Internal Aerial Delivery in Fixed Wing Aircraft (S\/S by MIL-STD-1791)&#8221; &#8212; \u898f\u683c\u30de\u30b9\u30bf\u30fc\" data-secret=\"ZSfOqFBE32\" 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":"Designing for Internal Aerial Delivery in Fixed Wing Aircraft (S\/S by MIL-STD-1791) - This standard covers general design and performance requirements of military equipment for internal air transport in military prime mission cargo aircraft and long range international segment of the Civil Reserve Air Fleet (CRAF)."}