{"id":18,"date":"2021-10-21T18:42:54","date_gmt":"2021-10-21T18:42:54","guid":{"rendered":"https:\/\/www.isi.edu\/centers-serc\/?page_id=18"},"modified":"2024-08-09T16:23:58","modified_gmt":"2024-08-09T16:23:58","slug":"nanosatellites","status":"publish","type":"page","link":"https:\/\/www.isi.edu\/centers-serc\/research\/nanosatellites\/","title":{"rendered":"Nanosatellites"},"content":{"rendered":"\n\n\t<a onclick=\"topFunction()\" id=\"toTop\" aria-label=\"Go to top\">\n<\/a>\n\t<p>\u200bSERC explores various new concepts in small and nanosatellite build and design. \u00a0Advanced payload integration and deployment from nanosatellites in LEO, digital design tool to autocode generation of onboard software, use of nanosats as parasitic ride-alongs with larger spacecraft, and advanced rendezvous and proximity operations techniques are some of the areas of research.<\/p>\n\t<header>\n<h2>Nanosat Projects (in order of build and\/or launch)<\/h2>\n<ul>\n<li><a href=\"#caerus\">CAERUS (Launched in 2010)<\/a><\/li>\n<li><a href=\"#aeneas\">AENEAS<\/a><\/li>\n<li><a href=\"#endor\">ENDOR Design Study<\/a><\/li>\n<li><a href=\"#dodona\">DODONA<\/a><\/li>\n<li><a href=\"#ozmosis\">OZMOSIS Design Study<\/a><\/li>\n<li><a href=\"#magneto\">MAGNETO<\/a><\/li>\n<li><a href=\"#nanoots\">NanoOTS Cubesat Design Study (in conjunction with Parabilis Inc.)<\/a><\/li>\n<li><a href=\"https:\/\/www.isi.edu\/centers-serc\/research\/nanosatellites\/maveric\/\">MAVERIC<\/a><\/li>\n<\/ul>\n<\/header>\n<header>\n<h2>Small Satellite projects (in order of build and\/or launch):<\/h2>\n<ul>\n<li><a href=\"#alcyone\">ALCYONE<\/a><\/li>\n<\/ul>\n<\/header>\n<article>\n    <section><h2>CAERUS (Launched in 2010)<\/h2><p>USC&#8217;s first satellite was a 1U Cubesat that became part of a 3U integrated onto the Northrop Grumman Mayflower Mission, launched in 2010. Caerus was the primary communication subsystem that supported the 3U and featured a new quad monopole deployable antenna designed and developed by the SERC team.<\/p><\/section>\n    <section><img decoding=\"async\" loading=\"lazy\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/10\/caerus-1.png\" alt=\"Deployed satellite on lab bench\"\/><\/section>\n<\/article>\n<article>\n    <section><img decoding=\"async\" loading=\"lazy\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/10\/aeneas-1.png\" alt=\"Render of deployed satellite around Earth with Sun in the background\"\/><\/section>\n    <section><h2>AENEAS<\/h2><p>USC&#8217;s second nanosatellite flight,\u00a0Aeneas, modified\u00a0a 3U (30x10x10cm) National Reconnaissance Office (NRO)-specified Colony I Cubesat bus to address a research thrust of the Department of Homeland Security (DHS). \u00a0Aeneas was launched in June\u00a02012 and is still operational today. Aeneas primary payload demonstrated tracking cargo containers over the open ocean with a 1-watt WiFi-like transceiver. This was in support of a\u00a0DHS effort for open ocean cargo tracking, designed by the primary payload provider iControl Inc. SERC advancements on the Cubeat included\u00a0a custom-built deployable 0.5m mesh antenna, and an increase of\u00a0the attitude control and power generation capabilities of the Colony I bus over the original specifications.<a href=\"https:\/\/www.isi.edu\/centers-serc\/research\/nanosatellites\/aeneas\/\">Visit AENEAS Page<\/a><\/p><\/section>\n<\/article>\n<article>\n    <section><h2>ENDOR Design Study<\/h2>\n<p>This project was a full CDR design of a Cubesat with a deployable 20cm inflatable sphere.  The goal was to understand the interaction between a 2-body problem in LEO, and the extent of influence that a sphere that is larger than the original Cubesat body would have on its attitude control, stability, thermal and RF shading, and life on orbit.  This project was in conjunction with students from Huntington Beach High School, Santa Monica College and Dept of Astronautical Engineering at USC.<\/p>\n<\/section>\n    <section><img decoding=\"async\" loading=\"lazy\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/10\/endor-1.png\" alt=\"Render of satellite on orbit around Earth\"\/><\/section>\n<\/article>\n<article>\n    <section><img decoding=\"async\" loading=\"lazy\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/10\/dodona-1.png\" alt=\"Group of four researchers wearing gloves and lab coats holding a microsatellite\"\/><\/section>\n    <section><h2>DODONA<\/h2><p>USC&#8217;s third nanosatellite project,\u00a0Dodona is a sister satellite to Aeneas.\u00a0 Its a full 3U satellite whose primary mission is to test out new payload technologies.<a href=\"https:\/\/www.isi.edu\/centers-serc\/research\/nanosatellites\/dodona\/\">Visit DODONA Page<\/a><\/p><\/section>\n<\/article>\n<article>\n    <section><h2>OZMOSIS Design Study<\/h2>\n<p>A 3U cubesat design study in concert with USC&#8217;s Space Science Center to build and fly a unique optical telescope for Earth based sensor imaging.  The science mission was two fold, the first was to support climate change measurements based on ozone depletion measurements in the solar occultation mode; the second was related to ionosphere measurements of space weather.  The payload instrument to fly in the 3U was a simple, compact (10x10x10 cm) instrument based on an off-axis telescope to provide good (optical) vertical resolution in the FOV with low stray light.  Equipped with two spectral channels (UV and visible light) as a prototype instrument for very low cost adjunct climate change spacecraft (Figure 1).<\/p>\n<\/section>\n    <section><img decoding=\"async\" loading=\"lazy\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/10\/ozmosis-1.png\" alt=\"OZMOSIS Design Study render\"\/><\/section>\n<\/article>\n<article>\n    <section><img decoding=\"async\" loading=\"lazy\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/12\/magneto.jpg\" alt=\"Magneto deployed CAD\"\/><\/section>\n    <section><h2>MAGNETO<\/h2><p>USC&#8217;s first all student class project to design, build, test, integrate and launch a Cubesat in a single academic year!<a href=\"https:\/\/www.isi.edu\/centers-serc\/research\/nanosatellites\/magneto\/\">Visit MAGNETO Page<\/a><\/p><\/section>\n<\/article>\n<article>\n    <section><h2>NanoOTS Cubesat Design Study (in conjunction with Parabilis Inc.)<\/h2><p>SERC supported Parabilis Space Inc.&#8217;s Phase 1 effort to design a Nano Orbital Transfer System using their novel propulsion system. The SERC team did several trade studies on placement of arrays for power and integration of a propulsion system inside a 3U cubesat for optimal location and center of mass propulsive efficiency.<a href=\"https:\/\/parabilis-space.com\/programs-and-applications\/#nanosat-maneuvering-and-orbital-transfer-system-ots\">Visit Parabilis Page<\/a><\/p><\/section>\n    <section><img decoding=\"async\" loading=\"lazy\" src=\"https:\/\/www.isi.edu\/centers-serc\/wp-content\/uploads\/sites\/12\/2021\/10\/nanoots.png\" alt=\"Render of deployed microsatellite\"\/><\/section>\n<\/article><section>\n    <h2>Small Satellite Projects<\/h2>\n<\/section>\n\t<h2>ALCYONE<\/h2>\n<p>This was a 250kg small satellite design done in conjuction with Northrop Grumman, to host a hyperspectral imager for a NOAA mission. SERC team members completed a PDR level design of the bus structure and systems, and built a full scale mass mockup using honeycomb sandwich panels.<\/p>\n\n","protected":false},"excerpt":{"rendered":"<p>\u200bSERC explores various new concepts in small and nanosatellite build and design. \u00a0Advanced payload integration and deployment from nanosatellites in LEO, digital design tool to autocode generation of onboard software, use of nanosats as parasitic ride-alongs with larger spacecraft, and advanced rendezvous and proximity operations techniques are some of the areas of research. Nanosat Projects&hellip;<\/p>\n","protected":false},"author":421,"featured_media":0,"parent":592,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"news_source":"","news_author":"","external_news_link":"","footnotes":""},"class_list":["post-18","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.6 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Nanosatellites - 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\/nanosatellites\/\" \/>\n<meta property=\"og:locale\" content=\"en_US\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Nanosatellites - Space Engineering Research Center\" \/>\n<meta property=\"og:description\" content=\"\u200bSERC explores various new concepts in small and nanosatellite build and design. \u00a0Advanced payload integration and deployment from nanosatellites in LEO, digital design tool to autocode generation of onboard software, use of nanosats as parasitic ride-alongs with larger spacecraft, and advanced rendezvous and proximity operations techniques are some of the areas of research. 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