{"id":88,"date":"2021-10-22T17:04:08","date_gmt":"2021-10-22T17:04:08","guid":{"rendered":"https:\/\/www.isi.edu\/centers-serc\/?page_id=88"},"modified":"2021-11-29T17:09:45","modified_gmt":"2021-11-29T17:09:45","slug":"generation-1","status":"publish","type":"page","link":"https:\/\/www.isi.edu\/centers-serc\/research\/lunar-lander-prototype\/generation-1\/","title":{"rendered":"Generation 1"},"content":{"rendered":"\n\n\t<p>Generation-1 of LEAPFROG will use a larger thrust engine to provide a &gt;1.25 thrust-to-weight ratio. Design optimization to reduce the mass of the structure, attitude control system, and electronics will enable a longer flight time and allow new payloads and sensors to be added. The platform will also have improved hover capability and self-correction for attitude and velocity drift.<\/p>\n\t\t\t\t<img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/11\/leapfrog1-0.jpg\" alt=\"leapfrog1-0\" itemprop=\"image\" height=\"350\" width=\"1200\" title=\"leapfrog1-0\" onerror=\"this.style.display='none'\"  \/>\n\n","protected":false},"excerpt":{"rendered":"<p>Generation-1 of LEAPFROG will use a larger thrust engine to provide a &gt;1.25 thrust-to-weight ratio. Design optimization to reduce the mass of the structure, attitude control system, and electronics will enable a longer flight time and allow new payloads and sensors to be added. The platform will also have improved hover capability and self-correction for&hellip;<\/p>\n","protected":false},"author":421,"featured_media":0,"parent":84,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"news_source":"","news_author":"","external_news_link":"","footnotes":""},"class_list":["post-88","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.2 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Generation 1 - Space Engineering Research Center<\/title>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/www.isi.edu\/centers-serc\/research\/lunar-lander-prototype\/generation-1\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Generation 1 - Space Engineering Research Center\" \/>\n<meta property=\"og:description\" content=\"Generation-1 of LEAPFROG will use a larger thrust engine to provide a &gt;1.25 thrust-to-weight ratio. 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