{"id":17186,"date":"2024-06-06T11:51:36","date_gmt":"2024-06-06T11:51:36","guid":{"rendered":"https:\/\/aerospacerepository.org\/?p=17186"},"modified":"2025-09-21T13:57:31","modified_gmt":"2025-09-21T13:57:31","slug":"design-and-implementation-of-electronic-sub-systems-for-the-staje-phase-1-payload","status":"publish","type":"post","link":"https:\/\/aerospacerepository.org\/index.php\/2024\/06\/06\/design-and-implementation-of-electronic-sub-systems-for-the-staje-phase-1-payload\/","title":{"rendered":"Design and Implementation of Electronic Sub-systems for the STAJe- Phase 1 Payload"},"content":{"rendered":"\n<p><strong>Sampada Vijay SHELAR, Allan PAULL<\/strong><\/p>\n\n\n\n<p><strong>DOI Number: 10.82241\/ceas-hisst-2024-261<\/strong><\/p>\n\n\n\n<p><strong>Conference number: HiSST-2024-261<\/strong><\/p>\n\n\n\n<p>STAJe- Phase 1 is a supersonic flight initiative which uses COTS hardware for the on-board electronic sub-systems and LORA technology is used for tracking of the flight module from an altitude of 20km to ground. The designing and manufacturing of customable printed circuit boards to fit into the mechanical sections of the payload is complete, tested and verified which is an excellent demonstration of interdisciplinary collaboration and rapid manufacturing for space applications. The on-ground testing of the electronic hardware for both, the payload and the telemetry stations, is completed and promising results are summarized. Finally, the conclusion provides a synopsis of different steps involved in the making of a flight vehicle for space applications.<\/p>\n\n\n\n<p><a href=\"https:\/\/aerospacerepository.org\/wp-content\/uploads\/2024\/06\/HiSST-2024-261.pdf\">Read the full paper here<\/a><\/p>\n\n\n\n<p><\/p>\n","protected":false},"excerpt":{"rendered":"<p><b>Sampada Vijay SHELAR, Allan PAULL<\/b><\/p>\n<p>DOI Number: https:\/\/doi.org\/10.82241\/ceas-hisst-2024-261<br \/>\nConference number: HiSST-2024-261<\/p>\n","protected":false},"author":2,"featured_media":0,"comment_status":"open","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[993,1407,1415],"tags":[1580,585,1803,1802],"class_list":["post-17186","post","type-post","status-publish","format-standard","hentry","category-events","category-11-hisst-2024","category-testing-evaluation","tag-electric-propulsion","tag-ground-testing","tag-lora","tag-payload-design","category-993","category-1407","category-1415","description-off"],"_links":{"self":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17186","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/users\/2"}],"replies":[{"embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/comments?post=17186"}],"version-history":[{"count":4,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17186\/revisions"}],"predecessor-version":[{"id":21237,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/posts\/17186\/revisions\/21237"}],"wp:attachment":[{"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/media?parent=17186"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/categories?post=17186"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/aerospacerepository.org\/index.php\/wp-json\/wp\/v2\/tags?post=17186"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}