{"id":2313,"date":"2019-03-19T13:38:47","date_gmt":"2019-03-19T13:38:47","guid":{"rendered":"https:\/\/www.open-engineering.com\/?page_id=2313"},"modified":"2024-04-08T11:51:05","modified_gmt":"2024-04-08T11:51:05","slug":"small-scale-satellites","status":"publish","type":"page","link":"https:\/\/www.open-engineering.com\/index.php\/small-scale-satellites\/","title":{"rendered":"Small satellites"},"content":{"rendered":"\t\t<div data-elementor-type=\"wp-post\" data-elementor-id=\"2313\" class=\"elementor elementor-2313\">\n\t\t\t\t\t\t<section class=\"elementor-section elementor-top-section elementor-element elementor-element-87a2473 elementor-section-boxed elementor-section-height-default elementor-section-height-default\" data-id=\"87a2473\" data-element_type=\"section\" data-e-type=\"section\">\n\t\t\t\t\t\t<div class=\"elementor-container elementor-column-gap-default\">\n\t\t\t\t\t<div class=\"elementor-column elementor-col-100 elementor-top-column elementor-element elementor-element-877976f\" data-id=\"877976f\" data-element_type=\"column\" data-e-type=\"column\">\n\t\t\t<div class=\"elementor-widget-wrap elementor-element-populated\">\n\t\t\t\t\t\t<div class=\"elementor-element elementor-element-7331e4e elementor-widget__width-inherit elementor-widget elementor-widget-heading\" data-id=\"7331e4e\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t\t<h1 class=\"elementor-heading-title elementor-size-default\">Small scale satellites - Digital twin<\/h1>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-6f947e1 elementor-widget__width-inherit elementor-widget elementor-widget-text-editor\" data-id=\"6f947e1\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t\t\t\t\t\t<p>The global market for smaller scale satellites in space is expected to reach $491.3m by 2027, growing over 15 percent per year says Allied Market Research.<br \/><span style=\"font-size: 17px;\"><br \/><\/span><\/p><p><span style=\"font-size: 17px;\">A CubeSat is a cubical-shaped small satellite measuring 10x10x10 cm3- approximately the dimension of the popular Rubik&#8217;s cube weighs around 1 kg. A CubeSat can be used as a single unit (1 U) or in clusters of several units or U\u2019s (1U, 2U, 3U, 6U, and 12U, among others). <br \/><\/span><\/p><p><span style=\"font-size: 17px;\">The growing number of missions covered with microsatellites increases the need for numerical simulations.<\/span><\/p><p><span style=\"font-size: 17px;\">\u00a0<\/span><\/p>\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-3c0bba5 elementor-widget__width-inherit elementor-widget elementor-widget-image\" data-id=\"3c0bba5\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"image.default\">\n\t\t\t\t\t\t\t\t\t\t\t\t<figure class=\"wp-caption\">\n\t\t\t\t\t\t\t\t\t\t\t<a href=\"http:\/\/www.cubesatkit.com\/\" target=\"_blank\">\n\t\t\t\t\t\t\t<img fetchpriority=\"high\" decoding=\"async\" width=\"276\" height=\"300\" src=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-IGS-model-276x300.png\" class=\"attachment-medium size-medium wp-image-2807\" alt=\"\" srcset=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-IGS-model-276x300.png 276w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-IGS-model.png 291w\" sizes=\"(max-width: 276px) 100vw, 276px\" \/>\t\t\t\t\t\t\t\t<\/a>\n\t\t\t\t\t\t\t\t\t\t\t<figcaption class=\"widget-image-caption wp-caption-text\">1U platform (from CubeSat Kit)<\/figcaption>\n\t\t\t\t\t\t\t\t\t\t<\/figure>\n\t\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-9362f9c elementor-widget__width-inherit elementor-widget elementor-widget-heading\" data-id=\"9362f9c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t\t<h2 class=\"elementor-heading-title elementor-size-default\">Create a 3D model suitable for FEA<\/h2>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-288527b elementor-widget__width-inherit elementor-position-top elementor-widget elementor-widget-image-box\" data-id=\"288527b\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"image-box.default\">\n\t\t\t\t\t<div class=\"elementor-image-box-wrapper\"><figure class=\"elementor-image-box-img\"><img decoding=\"async\" width=\"328\" height=\"316\" src=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-solid-model.png\" class=\"attachment-full size-full wp-image-2810\" alt=\"\" srcset=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-solid-model.png 328w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-solid-model-300x289.png 300w\" sizes=\"(max-width: 328px) 100vw, 328px\" \/><\/figure><div class=\"elementor-image-box-content\"><h3 class=\"elementor-image-box-title\">Fom IGS to 3D solid<\/h3><p class=\"elementor-image-box-description\">Very often, the provided CAD model is not adapted to CAE because it is made of a collection of surface (and not 3D solids) and contains details that are not relevant for the type of insights one wants to gain from the numerical mock-up.\nOur simulation workflow makes it easy to remove unnecessary details and constructing 3D solids.<\/p><\/div><\/div>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-fc07253 elementor-widget__width-inherit elementor-widget elementor-widget-image\" data-id=\"fc07253\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"image.default\">\n\t\t\t\t\t\t\t\t\t\t\t\t<figure class=\"wp-caption\">\n\t\t\t\t\t\t\t\t\t\t<img decoding=\"async\" width=\"768\" height=\"277\" src=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Volumic_Mesh-768x277.png\" class=\"attachment-medium_large size-medium_large wp-image-2865\" alt=\"\" srcset=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Volumic_Mesh-768x277.png 768w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Volumic_Mesh-300x108.png 300w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Volumic_Mesh-1024x369.png 1024w\" sizes=\"(max-width: 768px) 100vw, 768px\" \/>\t\t\t\t\t\t\t\t\t\t\t<figcaption class=\"widget-image-caption wp-caption-text\">A typical FEM model used for simulations<\/figcaption>\n\t\t\t\t\t\t\t\t\t\t<\/figure>\n\t\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-d1c42c4 elementor-widget__width-inherit elementor-widget elementor-widget-heading\" data-id=\"d1c42c4\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"heading.default\">\n\t\t\t\t\t<h2 class=\"elementor-heading-title elementor-size-default\">Multiphysics simulations<\/h2>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-36caf65 elementor-position-right elementor-widget__width-inherit elementor-vertical-align-top elementor-widget elementor-widget-image-box\" data-id=\"36caf65\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"image-box.default\">\n\t\t\t\t\t<div class=\"elementor-image-box-wrapper\"><figure class=\"elementor-image-box-img\"><a href=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal.png\" tabindex=\"-1\"><img loading=\"lazy\" decoding=\"async\" width=\"1123\" height=\"1115\" src=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal.png\" class=\"attachment-full size-full wp-image-2866\" alt=\"\" srcset=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal.png 1123w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal-150x150.png 150w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal-300x298.png 300w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal-768x763.png 768w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal-1024x1017.png 1024w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal-192x192.png 192w\" sizes=\"(max-width: 1123px) 100vw, 1123px\" \/><\/a><\/figure><div class=\"elementor-image-box-content\"><h3 class=\"elementor-image-box-title\"><a href=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/coques_modal.png\">Structural design<\/a><\/h3><p class=\"elementor-image-box-description\">During the launch, a satellite is submitted to static and dynamic loading. Using the OOFELIE::Multiphysics solver permits to consider: modal analysis, and random vibration (PSD) analysis.<br>The picture on the right shows one mode of vibration for e.g.<\/p><\/div><\/div>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-8e80190 elementor-position-left elementor-widget__width-inherit elementor-vertical-align-top elementor-widget elementor-widget-image-box\" data-id=\"8e80190\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"image-box.default\">\n\t\t\t\t\t<div class=\"elementor-image-box-wrapper\"><figure class=\"elementor-image-box-img\"><a href=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-temperature.png\" tabindex=\"-1\"><img loading=\"lazy\" decoding=\"async\" width=\"427\" height=\"254\" src=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-temperature.png\" class=\"attachment-full size-full wp-image-2815\" alt=\"\" srcset=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-temperature.png 427w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-temperature-300x178.png 300w\" sizes=\"(max-width: 427px) 100vw, 427px\" \/><\/a><\/figure><div class=\"elementor-image-box-content\"><h3 class=\"elementor-image-box-title\"><a href=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/03\/Cubesat-temperature.png\">Thermal design<\/a><\/h3><p class=\"elementor-image-box-description\">The OOFELIE::Multiphysics solver permits also to assess of the impact of thermal loads during operation in Earth orbit. Assessing the impact of thermal stresses on the mechanical response can be done within the same solution.<br>The picture on the left shows the temperature distribution a given time for e.g.<\/p><\/div><\/div>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-6cfb10c elementor-position-right elementor-widget__width-inherit elementor-vertical-align-top elementor-widget elementor-widget-image-box\" data-id=\"6cfb10c\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"image-box.default\">\n\t\t\t\t\t<div class=\"elementor-image-box-wrapper\"><figure class=\"elementor-image-box-img\"><a href=\"https:\/\/www.open-engineering.com\/index.php\/products\/the-oofeliemultiphysics-suite\/the-oofeliemultiphysics-solver\/features-available\/\" tabindex=\"-1\"><img loading=\"lazy\" decoding=\"async\" width=\"640\" height=\"421\" src=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2018\/06\/geometry-1044090_640.jpg\" class=\"attachment-full size-full wp-image-455\" alt=\"\" srcset=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2018\/06\/geometry-1044090_640.jpg 640w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2018\/06\/geometry-1044090_640-300x197.jpg 300w\" sizes=\"(max-width: 640px) 100vw, 640px\" \/><\/a><\/figure><div class=\"elementor-image-box-content\"><h3 class=\"elementor-image-box-title\"><a href=\"https:\/\/www.open-engineering.com\/index.php\/products\/the-oofeliemultiphysics-suite\/the-oofeliemultiphysics-solver\/features-available\/\">An holistic Approach<\/a><\/h3><p class=\"elementor-image-box-description\">The OOFELIE::Multiphysics solver can give you access to even more insights, global or local, on your design with additionnal simulations capabilities in the field of electromagnetics, flexible mechanisms, sensors ... <\/p><\/div><\/div>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-57092704 elementor-button-success elementor-align-center elementor-widget__width-inherit elementor-widget elementor-widget-button\" data-id=\"57092704\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"button.default\">\n\t\t\t\t\t\t\t\t\t\t<a class=\"elementor-button elementor-button-link elementor-size-md\" href=\"https:\/\/www.open-engineering.com\/index.php\/inquiry4product\/\" target=\"_blank\">\n\t\t\t\t\t\t<span class=\"elementor-button-content-wrapper\">\n\t\t\t\t\t\t<span class=\"elementor-button-icon\">\n\t\t\t\t<svg aria-hidden=\"true\" class=\"e-font-icon-svg e-far-envelope\" viewBox=\"0 0 512 512\" xmlns=\"http:\/\/www.w3.org\/2000\/svg\"><path d=\"M464 64H48C21.49 64 0 85.49 0 112v288c0 26.51 21.49 48 48 48h416c26.51 0 48-21.49 48-48V112c0-26.51-21.49-48-48-48zm0 48v40.805c-22.422 18.259-58.168 46.651-134.587 106.49-16.841 13.247-50.201 45.072-73.413 44.701-23.208.375-56.579-31.459-73.413-44.701C106.18 199.465 70.425 171.067 48 152.805V112h416zM48 400V214.398c22.914 18.251 55.409 43.862 104.938 82.646 21.857 17.205 60.134 55.186 103.062 54.955 42.717.231 80.509-37.199 103.053-54.947 49.528-38.783 82.032-64.401 104.947-82.653V400H48z\"><\/path><\/svg>\t\t\t<\/span>\n\t\t\t\t\t\t\t\t\t<span class=\"elementor-button-text\">Request TRIAL<\/span>\n\t\t\t\t\t<\/span>\n\t\t\t\t\t<\/a>\n\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-2413f32 elementor-widget__width-inherit elementor-position-top elementor-widget elementor-widget-image-box\" data-id=\"2413f32\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"image-box.default\">\n\t\t\t\t\t<div class=\"elementor-image-box-wrapper\"><figure class=\"elementor-image-box-img\"><a href=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/05\/mesh5.png\" tabindex=\"-1\"><img loading=\"lazy\" decoding=\"async\" width=\"2468\" height=\"1167\" src=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/05\/mesh5.png\" class=\"attachment-full size-full wp-image-3810\" alt=\"\" srcset=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/05\/mesh5.png 2468w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/05\/mesh5-300x142.png 300w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/05\/mesh5-768x363.png 768w, https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/05\/mesh5-1024x484.png 1024w\" sizes=\"(max-width: 2468px) 100vw, 2468px\" \/><\/a><\/figure><div class=\"elementor-image-box-content\"><h3 class=\"elementor-image-box-title\"><a href=\"https:\/\/www.open-engineering.com\/wp-content\/uploads\/2019\/05\/mesh5.png\">Small satellite and its equipments<\/a><\/h3><p class=\"elementor-image-box-description\">Analyse the behaviour of your satellite with its payload and equipments<\/p><\/div><\/div>\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-5c77046 elementor-widget__width-inherit elementor-widget elementor-widget-text-editor\" data-id=\"5c77046\" data-element_type=\"widget\" data-e-type=\"widget\" data-widget_type=\"text-editor.default\">\n\t\t\t\t\t\t\t\t\t<p style=\"text-align: center;\">In the following video, the variation of the temperature distribution inside a Cubesat is presented. Temperature changes with respect to its position in orbit. Deep space, earth albedo, and heat generated by electrical equipment inside the microsatellite are taken into account.<\/p>\t\t\t\t\t\t\t\t<\/div>\n\t\t\t\t<div class=\"elementor-element elementor-element-aaf376a elementor-widget__width-inherit premium-video__glow-none elementor-widget elementor-widget-premium-addon-video-box\" data-id=\"aaf376a\" data-element_type=\"widget\" data-e-type=\"widget\" data-settings=\"{&quot;aspect_ratio&quot;:&quot;11&quot;,&quot;premium_video_box_video_type&quot;:&quot;youtube&quot;}\" data-widget_type=\"premium-addon-video-box.default\">\n\t\t\t\t<div class=\"elementor-widget-container\">\n\t\t\t\t\t\r\n\r\n\t\t\r\n\t\t\t\t\t<div id=\"premium-video-box-container-aaf376a\" class=\"premium-video-box-container\" data-overlay=\"true\" data-type=\"youtube\" data-thumbnail=\"\" data-hover=\"none\">\r\n\t\t\t\t<div  >\r\n\t\t\t\t\t\r\n\t\t\t\t\t<div class=\"premium-video-box-inner-wrap\" data-video-animation=\" animated-\" data-delay-animation=\"\">\r\n\t\t\t\t\t\t<div data-src=\"https:\/\/www.youtube.com\/embed\/mZ2mxRBlOl8?feature=oembed&amp;rel=0&amp;mute=1&amp;loop=1&amp;controls=1&amp;playsinline=0&amp;autoplay=1&amp;cc_load_policy=0\" class=\"premium-video-box-video-container\">\r\n\t\t\t\t\t\t\t\r\n\t\t\t\t\t\t\t\t\t\t\t\t\t<\/div>\r\n\t\t\t\t\t\t\t<div style=\"background-image:transparent\" class=\"premium-video-box-image-container none\"><\/div>\r\n\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t\t<\/div>\r\n\r\n\t\t\t\t<\/div>\r\n\t\t\t<\/div>\r\n\t\t\r\n\t\t\t\t\t\t<\/div>\n\t\t\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/div>\n\t\t\t\t\t<\/div>\n\t\t<\/section>\n\t\t\t\t<\/div>\n\t\t","protected":false},"excerpt":{"rendered":"<p>Small scale satellites &#8211; Digital twin The global market for smaller scale satellites in space is expected to reach $491.3m by 2027, growing over 15 percent per year says Allied 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