{"id":8642,"date":"2023-05-05T01:45:13","date_gmt":"2023-05-04T17:45:13","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/c3s-introduces-a-new-3u-satellite-platform-for-earth-observation-applications\/"},"modified":"2023-05-05T01:45:13","modified_gmt":"2023-05-04T17:45:13","slug":"c3s-introduces-a-new-3u-satellite-platform-for-earth-observation-applications","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/c3s-introduces-a-new-3u-satellite-platform-for-earth-observation-applications\/","title":{"rendered":"C3S Introduces a New 3U Satellite Platform for Earth Observation Applications"},"content":{"rendered":"<p style=\"text-align: center;\" itemprop=\"image\" itemscope=\"\" itemtype=\"https:\/\/schema.org\/ImageObject\"><img loading=\"lazy\" decoding=\"async\" src=\"https:\/\/cdn.satnow.com\/news\/platform_C_638187778871850367.png\" width=\"712\" height=\"377\" alt=\"C3S Introduces a New 3U Satellite Platform for Earth Observation Applications\" class=\"imageload removeImageattr\" data-original=\"https:\/\/cdn.satnow.com\/news\/platform_C_638187778871850367.png\" style=\"\"><meta itemprop=\"url\" content=\"https:\/\/cdn.satnow.com\/news\/platform_C_638187778871850367.png\"><meta itemprop=\"width\" content=\"712\"><meta itemprop=\"height\" content=\"377\"><\/p>\n<p>C3S, a company that develops and manufactures highly dependable 3\/6\/12\/16U platforms and subsystems like OBC, EPS, and communication modules to meet the requirements of IoT, Earth Observation, and space monitoring constellation missions has introduced a new 3U Satellite Platform.<\/p>\n<p>The 3U platform from C3S is a CubeSat platform with a 5-year design lifetime in LEO. It features an in-house developed structure and subsystems based on ECSS standards. The platform is constructed using a single-point failure-tolerant design.&nbsp;<\/p>\n<p>The platform has a mass of 3.3 Kg and measures 100 x 100 x 340.5 mm. It has an average power consumption of 4.5 W and a maximum incoming solar power of 50 W. This platform has a 58 Wh \/ 65 Wh battery capacity and power buses in the range of 3.3-12V. It uses a 32-bit ARM Cortex-M7 for the onboard computer and has a mass storage capacity of 16 MByte MRAM.<\/p>\n<p>The 3U platform can accommodate payloads of up to 4.7 kg with a volume of 1.25 &#8211; 1.4 U. The average power available for the payload is up to 20 W with a peak power of 35W. The platform supports CAN 2.0B and M-LVDS communication interfaces for the payload.<\/p>\n<p>The platform structure is optimized for high dissipation density and thermo-elasticity, both payload and platform-wise. Furthermore, a unique radiator design allows unequaled freedom in payload dissipation along with unprecedentedly high payload power availability.<\/p>\n<p>The 3U platform is SEE radiation tested, TID tested, and vibration tested. It is ideal for applications such as IoT, earth observation, and space weather monitoring.<\/p>\n<p><strong>Click here to learn about Satellite Buses and Platforms from various manufacturers listed on SATNow.<\/strong><\/p>\n","protected":false},"excerpt":{"rendered":"<p>C3S, a company that develops and manufactures highly dependable 3\/6\/12\/16U platforms and subsystems like OBC, EPS, and communication modules to meet the requirements of IoT, Earth Observation, and space monitoring constellation missions has introduced a new 3U Satellite Platform. The 3U platform from C3S is a CubeSat platform with a 5-year design lifetime in LEO. [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[26,51,20,24],"class_list":["post-8642","post","type-post","status-publish","format-standard","hentry","category-news","tag-ground","tag-iot","tag-satellite","tag-satellite-bus-platforms"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/8642"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=8642"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/8642\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=8642"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=8642"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=8642"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}