{"id":221,"date":"2018-03-23T10:01:01","date_gmt":"2018-03-23T09:01:01","guid":{"rendered":"http:\/\/templategdr.dii.unipd.it\/?page_id=221"},"modified":"2026-03-20T14:22:34","modified_gmt":"2026-03-20T13:22:34","slug":"facilities","status":"publish","type":"page","link":"https:\/\/research.dii.unipd.it\/flightds\/facilities\/","title":{"rendered":"Facilities"},"content":{"rendered":"<h3 style=\"font-weight: 400\"><strong>Space Automation<\/strong><\/h3>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"wp-image-315 size-medium alignleft\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2022\/12\/robotic_facility-300x211.jpg\" alt=\"\" width=\"300\" height=\"211\" srcset=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2022\/12\/robotic_facility-300x211.jpg 300w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2022\/12\/robotic_facility-768x540.jpg 768w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2022\/12\/robotic_facility.jpg 870w\" sizes=\"auto, (max-width: 300px) 100vw, 300px\" \/><\/p>\n<p>The group has developed several technologies and facilities with the purpose to improve the robotics automation in space.<\/p>\n<p>The space robotics is studied in two different ways that have produce two different environments:<\/p>\n<ul>\n<li style=\"list-style-type: none\">\n<ul>\n<li><strong>Numerical simulator<\/strong>. In the last years, the group has collaborate with ESA in order to develop a virtual environment to tests Guidance Navigation and Control algorithms for space robotics.<\/li>\n<li><strong>Experimental validation<\/strong>. The numerical simulations are tested with real hardware (which is representative of that used in satellites) through experimental campaign.<\/li>\n<\/ul>\n<\/li>\n<\/ul>\n<hr \/>\n<h3 style=\"text-align: right\"><img loading=\"lazy\" decoding=\"async\" class=\"wp-image-705 size-medium alignright\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/cannone-225x300.jpg\" alt=\"\" width=\"225\" height=\"300\" srcset=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/cannone-225x300.jpg 225w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/cannone-768x1024.jpg 768w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/cannone-1024x1365.jpg 1024w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/cannone-810x1080.jpg 810w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/cannone.jpg 1136w\" sizes=\"auto, (max-width: 225px) 100vw, 225px\" \/><\/h3>\n<h3 style=\"font-weight: 400\"><strong>CISAS Hypervelocity Impacts facility<\/strong><\/h3>\n<p style=\"text-align: left\">The CISAS hypervelocity impacts facility is based on a two-stage light gas gun (LGG), which can achieve a high daily firing rate with low operating costs. The gun is capable of accelerating projectiles up to 100 mg at a maximum speed of 5.5 km\/s; up to 10 experiments per day can be achieved due to a specific setup which employs reusable components. The projectile velocity is measured by two laser optical barriers placed just before the impact chamber; a high-velocity camera is placed on one side of the impact chamber and is employed to record impact videos. In addition, dedicated sensors can be added to instrument the target depending on the experimental setup (e.g., accelerometers, acoustic sensors, ballistic pendulum).<br \/>\nImpact test campaigns include the assessment of collision-induced vibrations and damages on space systems, the verification of shields, the analysis of materials response to hypervelocity impacts, and the investigation of fragmentation phenomena.<\/p>\n<p><a href=\"https:\/\/cisas.unipd.it\/\">CISAS &#8220;G. Colombo&#8221; Centre of Studies and Activities for Space website<\/a><\/p>\n<p>&nbsp;<\/p>\n<hr \/>\n<h3 style=\"font-weight: 400\"><strong>CISAS laboratories for the qualification of space components<\/strong><\/h3>\n<p style=\"font-weight: 400\">The laboratories dedicated to the qualification of space components have been continuously updated to meet the needs dictated by participation in national and international space programs mainly in AIV activities and on qualification tests for sensors and instrumentation. The laboratories house clean rooms (from class 10000 to class 100), climatic chambers for thermal vacuum tests with temperature control in the range of 80-420 K and a control volume of about 1000 liters, and electrodynamic shakers capable of performing mechanical tests with sine, random and shock excitation.<\/p>\n<hr \/>\n<p style=\"font-weight: 400;text-align: left\"><strong>CISAS Horizontal TV chamber: <\/strong>this\u00a0<span lang=\"EN-US\">chamber is used for experiments in High vacuum conditions. <\/span><\/p>\n<table>\n<tbody>\n<tr>\n<td width=\"30%\">\n<div><span lang=\"IT\">Internal Volume<\/span><\/div>\n<\/td>\n<td>\n<p style=\"font-weight: 400\">Max:\u00a0 Diameter 900 mm \u2013 Length 900 mm<\/p>\n<p style=\"font-weight: 400\">(Without internal baseplate)<\/p>\n<p style=\"font-weight: 400\">Nominal:\u00a0 Height\u00a0 570 mm \u2013 Length 900 mm (With internal baseplate)<\/p>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Thermal control (Cooling)<\/span><\/div>\n<\/td>\n<td>\n<p style=\"font-weight: 400\">Controlled Nitrogen flow in a dedicated cryostat<\/p>\n<p><span style=\"font-weight: 400\">(Achieved Cryostat temperature around -190\u00b0C)<\/span><\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Thermal control (Heating)<\/span><\/div>\n<\/td>\n<td>\n<p style=\"font-weight: 400\">3 PID-controlled thermal resistance circuits ( Max Current 15 A)<\/p>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Available temperature sensors (pt 100) <\/span><\/div>\n<\/td>\n<td>\n<div><span lang=\"IT\">30<\/span><\/div>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Achievable Internal Absolute Pressure <\/span><\/div>\n<\/td>\n<td>\n<div><span lang=\"IT\">\u00a0&lt; 5 10<sup>-5<\/sup> mbar<\/span><\/div>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"EN-US\">Available interfaces on external flanges <\/span><\/div>\n<\/td>\n<td>\n<div><span lang=\"EN-US\">BNC, DB9, DB25, USB ..configurable using different flanges \u00a0<\/span><\/div>\n<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p>&nbsp;<\/p>\n<table>\n<tbody>\n<tr>\n<td width=\"50%\"><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-653 aligncenter\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-2-300x151.jpg\" alt=\"\" width=\"380\" height=\"191\" srcset=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-2-300x151.jpg 300w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-2.jpg 432w\" sizes=\"auto, (max-width: 380px) 100vw, 380px\" \/><\/p>\n<div style=\"text-align: center\"><span lang=\"EN-US\">CISAS Horizontal TV chamber- Detail of interfaces on lateral flanges.<\/span><\/div>\n<div style=\"text-align: center\"><span lang=\"EN-US\">(configurable using different flanges) <\/span><\/div>\n<\/td>\n<td width=\"50%\"><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-652 alignleft\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-1.png\" alt=\"\" width=\"243\" height=\"191\" \/><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-651 alignleft\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-1.jpg\" alt=\"\" width=\"172\" height=\"191\" \/><\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n<p style=\"font-weight: 400;text-align: center\">CISAS Horizontal TV chamber (left) and view of the internal cryostat with the thermally controlled baseplate.<\/p>\n<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p>&nbsp;<\/p>\n<hr \/>\n<p style=\"font-weight: 400;text-align: left\"><strong>CISAS vertical TV chamber:<\/strong>\u00a0CISAS vertical\u00a0 TV chamber is used for experiments in Vacuum conditions when a bigger internal volume is needed (for example for testing Lunar drilling payloads).<\/p>\n<table>\n<tbody>\n<tr>\n<td>\n<table>\n<tbody>\n<tr>\n<td>\n<div><span lang=\"IT\">Internal Volume<\/span><\/div>\n<\/td>\n<td>\n<p style=\"font-weight: 400\">Nominal:\u00a0 Diameter 1000 mm \u2013 \u00a0Height 3800 mm<\/p>\n<p style=\"font-weight: 400\">(Without internal baseplate)<\/p>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Thermal control (Cooling)<\/span><\/div>\n<\/td>\n<td>\n<p style=\"font-weight: 400\">Controlled Nitrogen flow in a dedicated cryostat<\/p>\n<p style=\"font-weight: 400\"><span style=\"font-weight: 400\">(Achieved Cryostat temperature around -190\u00b0C)<\/span><\/p>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Thermal control (Heating)<\/span><\/div>\n<\/td>\n<td>\n<p style=\"font-weight: 400\">PID-controlled thermal resistance circuits ( Max Current 15 A)<\/p>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Available temperature sensors (pt 100) <\/span><\/div>\n<\/td>\n<td>\n<div><span lang=\"IT\">20<\/span><\/div>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"IT\">Achievable Internal Absolute Pressure <\/span><\/div>\n<\/td>\n<td>\n<div><span lang=\"IT\">\u00a0&lt; 5 10<sup>-3<\/sup> mbar<\/span><\/div>\n<\/td>\n<\/tr>\n<tr>\n<td>\n<div><span lang=\"EN-US\">Available interfaces on external flanges <\/span><\/div>\n<\/td>\n<td>\n<div><span lang=\"EN-US\">BNC, DB9, DB25, USB ..configurable using different flanges \u00a0<\/span><\/div>\n<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<\/td>\n<td width=\"30%\">&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-654 aligncenter\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-4-239x300.jpg\" alt=\"\" width=\"200\" height=\"251\" srcset=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-4-239x300.jpg 239w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-4.jpg 252w\" sizes=\"auto, (max-width: 200px) 100vw, 200px\" \/><\/p>\n<div><span lang=\"EN-US\">CISAS Vertical \u00a0TV \u00a0chamber<\/span><\/div>\n<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<hr \/>\n<table>\n<tbody>\n<tr>\n<td width=\"70%\">\n<h4 style=\"font-weight: 400;text-align: left\"><strong>Electrodynamic shaker<\/strong><\/h4>\n<p style=\"font-weight: 400;text-align: left\">The electrodynamic shaker has a maximum force up to 10 kN in the frequency range 5-5000 Hz and is use to perform \u00a0sine, random and SRS shock tests on space equipment for qualification and acceptance processes.<\/p>\n<h4 style=\"font-weight: 400;text-align: right\"><strong>Solar simulator<\/strong><\/h4>\n<p style=\"font-weight: 400;text-align: right\">The designed solar simulator can reproduce the intensity and spectral distribution of the Sun&#8217;s radiation up to 10 Solar constants and has been installed near a Thermal Vacuum Chamber provided with a viewport in order to be able to test the performance of any space equipment under a range of pressure and temperature conditions, including different intensities of sunlight and different angles of incidence.<\/p>\n<\/td>\n<td width=\"50%\"><img loading=\"lazy\" decoding=\"async\" class=\"wp-image-660 aligncenter\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-1-1.png\" alt=\"\" width=\"185\" height=\"216\" \/><\/p>\n<p style=\"text-align: center\">Electrodynamic shaker<\/p>\n<\/td>\n<\/tr>\n<\/tbody>\n<\/table>\n<p style=\"text-align: center\"><strong><img loading=\"lazy\" decoding=\"async\" class=\" wp-image-669 aligncenter\" src=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-2-1-300x149.png\" alt=\"\" width=\"531\" height=\"264\" srcset=\"https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-2-1-300x149.png 300w, https:\/\/research.dii.unipd.it\/flightds\/wp-content\/uploads\/sites\/19\/2023\/03\/Picture-2-1.png 403w\" sizes=\"auto, (max-width: 531px) 100vw, 531px\" \/><\/strong>Solar Simulator<\/p>\n<hr \/>\n<p>&nbsp;<\/p>\n<p>&nbsp;<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Space Automation The group has developed several technologies and facilities with the purpose to improve the robotics automation in space. The space robotics is studied in two different ways that have produce two different environments: Numerical simulator. In the last years, the group has collaborate with ESA in order to develop a virtual environment to&hellip; <br \/> <a class=\"read-more\" href=\"https:\/\/research.dii.unipd.it\/flightds\/facilities\/\">Leggi tutto<\/a><\/p>\n","protected":false},"author":1,"featured_media":0,"parent":0,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"footnotes":""},"folder":[],"class_list":["post-221","page","type-page","status-publish","hentry"],"yoast_head":"<!-- This site is optimized with the Yoast SEO plugin v27.4 - https:\/\/yoast.com\/product\/yoast-seo-wordpress\/ -->\n<title>Facilities - FLIGHTDS<\/title>\n<meta name=\"description\" content=\"The University of Padova, the DII and the CISAS centre provide the necessary facilities for the entire research and development phase\" \/>\n<meta name=\"robots\" content=\"index, follow, max-snippet:-1, max-image-preview:large, max-video-preview:-1\" \/>\n<link rel=\"canonical\" href=\"https:\/\/research.dii.unipd.it\/flightds\/facilities\/\" \/>\n<meta property=\"og:locale\" content=\"it_IT\" \/>\n<meta property=\"og:type\" content=\"article\" \/>\n<meta property=\"og:title\" content=\"Facilities - 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