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[\/et_pb_text][\/et_pb_column][\/et_pb_row][\/et_pb_section][et_pb_section fb_built=”1″ _builder_version=”4.25.0″ _module_preset=”default” custom_margin=”-8px|||||” custom_padding=”0px||0px|||” global_colors_info=”{}”][et_pb_row _builder_version=”4.25.0″ _module_preset=”default” custom_padding=”0px|||||” global_colors_info=”{}”][et_pb_column type=”4_4″ _builder_version=”4.25.0″ _module_preset=”default” global_colors_info=”{}”][et_pb_text _builder_version=”4.27.4″ _module_preset=”default” text_font=”Rajdhani||||||||” text_font_size=”20px” header_3_font=”Rajdhani|||on|||||” header_3_text_align=”center” header_3_text_color=”#014877″ header_3_font_size=”23px” custom_padding=”40px|||||” global_colors_info=”{}”]<\/p>\n
<\/blockquote>\nproject objective<\/strong><\/h3>\n
The primary goal of the <\/span>LCS4 (Low-Cost Separation System for Small Satellites) project<\/strong> is to <\/span>design, develop, and qualify an affordable European alternative<\/strong> to existing small satellite separation systems. This new separation system is optimized for <\/span>LightSat missions (lightweight satellites)<\/strong> and provides a <\/span>cost-effective solution<\/strong> that is <\/span>fully compatible <\/strong>with the <\/span>PSC MLB (Planetary Systems Corp Motorized Lightband<\/span><\/strong>) system<\/strong>.<\/span><\/p>\n
\n
\n<\/div>\n<\/strong><\/h3>\n
key components of the lcs4 system<\/strong><\/strong><\/h3>\n
1. Structural Subsystem<\/strong><\/h4>\n
\n
- Circular Rings<\/strong> \u2013 The system consists of two circular rings<\/strong>, with one attached to the satellite<\/strong> and the other to the launch vehicle<\/strong>.<\/li>\n
- Separation<\/strong> occurs at the interface between these two rings<\/strong>, ensuring structural integrity<\/strong> and minimizing vibrations during launch.<\/li>\n<\/ul>\n
2. Separation Subsystem<\/strong><\/h4>\n
\n
- Locking Mechanism<\/strong> \u2013 Securely holds the satellite during pre-launch operations and flight<\/strong> and releases it upon command<\/strong>.<\/li>\n
- Designed to provide controlled separation velocity<\/strong> while minimizing unwanted torques<\/strong>, which could affect the satellite\u2019s post-separation orientation.<\/li>\n<\/ul>\n
3. Electrical Subsystem<\/strong> (mission-specific)<\/h4>\n
\n
- Electrical Interfaces<\/strong> \u2013 Includes connectors and microswitches<\/strong> that enable separation detection<\/strong> according to the specific mission requirements.<\/li>\n
- Capable of integrating redundant systems<\/strong> to ensure high reliability<\/strong> in the separation process.<\/li>\n<\/ul>\n
<\/ul>\n
\n
\n<\/div>\n<\/strong><\/span><\/h3>\n
advantages of the lcs4 system<\/strong><\/strong><\/h3>\n
\n
- Low Cost<\/strong> \u2013 A budget-friendly alternative to existing separation systems.<\/li>\n
- Modularity<\/strong> \u2013 Adaptable to different sizes and weight categories of small satellites.<\/li>\n
- Compatibility<\/strong> \u2013 Fully integrable with standard launch adapters<\/strong> and systems such as PSC MLB<\/strong>.<\/li>\n
- Reliability<\/strong> \u2013 Optimized design minimizes the risk of failure<\/strong> during separation.<\/li>\n<\/ul>\n
The LCS4 system introduces a new generation of cost-effective separation solutions<\/strong>, supporting the growth of the European small satellite market<\/strong> and enhancing efficiency and accessibility for space missions<\/strong>.<\/p>\n
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\n<\/div>\n<\/p>\n<\/div>\n<\/div>\n<\/div>\n<\/div>\n
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Low-Cost Separation System for Small Satellites project objective The primary goal of the LCS4 (Low-Cost Separation System for Small Satellites) project is to design, develop, and qualify an affordable European alternative to existing small satellite separation systems. This new separation system is optimized for LightSat missions (lightweight satellites) and provides a cost-effective solution that is […]<\/p>\n","protected":false},"author":7,"featured_media":0,"parent":1416,"menu_order":0,"comment_status":"closed","ping_status":"closed","template":"","meta":{"_et_pb_use_builder":"on","_et_pb_old_content":"","_et_gb_content_width":"","footnotes":""},"class_list":["post-256825","page","type-page","status-publish","hentry"],"_links":{"self":[{"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/pages\/256825","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/pages"}],"about":[{"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/types\/page"}],"author":[{"embeddable":true,"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/users\/7"}],"replies":[{"embeddable":true,"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/comments?post=256825"}],"version-history":[{"count":4,"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/pages\/256825\/revisions"}],"predecessor-version":[{"id":257829,"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/pages\/256825\/revisions\/257829"}],"up":[{"embeddable":true,"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/pages\/1416"}],"wp:attachment":[{"href":"https:\/\/www.sabaerospace.cz\/en\/wp-json\/wp\/v2\/media?parent=256825"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}