{"id":242727,"date":"2016-09-07T14:38:08","date_gmt":"2016-09-07T18:38:08","guid":{"rendered":"http:\/\/amsat-uk.org\/?p=30639"},"modified":"2016-09-07T14:38:08","modified_gmt":"2016-09-07T18:38:08","slug":"5-ghz-to-10-ghz-lunar-transponder-mission","status":"publish","type":"post","link":"https:\/\/spaceweekly.com\/?p=242727","title":{"rendered":"5 GHz to 10 GHz Lunar Transponder Mission"},"content":{"rendered":"<p><a href=\"https:\/\/ukamsat.files.wordpress.com\/2016\/09\/view-of-earth-from-the-moon-adobestock_77398324.jpeg\"><img loading=\"lazy\" decoding=\"async\" class=\"alignright size-medium wp-image-30627\" src=\"https:\/\/ukamsat.files.wordpress.com\/2016\/09\/view-of-earth-from-the-moon-adobestock_77398324.jpeg?w=300&#038;h=292\" alt=\"View of Earth from the Moon AdobeStock_77398324\" width=\"300\" height=\"292\" \/><\/a>AMSAT-NA plan a satellite carrying transponders for 5 GHz to 10 GHz that is expected to launch into a Lunar orbit in September 2018.<\/p>\n<p><strong>Heimdallr<\/strong> is a\u00a03 axis stabilized 6U CubeSat with a mass of approximately 8 kg. It will have a Cold Gas Thruster for inertia dump and a star tracker for navigation. Deployable, gimbled solar panels will produce up to 100 watts of DC power, electric propulsion will be used to achieve lunar orbit.<\/p>\n<p>There will be a combination of omni and directional patch antennas on one side of spacecraft.<\/p>\n<p>The first part of mission is to provide Telemetry, Tracking, and Command (TT&amp;C) to obtain lunar orbit. The second part is to perform the data downlink experiment while the final part is to provide a two way regenerative repeater and analog repeater in lunar orbit for lifetime of satellite.<\/p>\n<p>Proposing these downlinks:<br \/>\n\u2022 Omni transponder: 10.451 GHz +\/- 0.5 MHz<br \/>\n\u2022 Directional transponder: 10.4575 GHz. +\/- 3.5 MHz<br \/>\n\u2022 Analog transponder: 10.4665 GHz. +\/- 2.0 MHz<\/p>\n<p>For the first part of the mission (TT&amp;C) using 300 bps BPSK 1\/2 rate viterbi Ranging 1.5 Mbps BPSK DSSS. For the\u00a0 second part of mission 4.5 Mbps QPSK \u00bd rate DVB-S2. For the final part of mission 25 kbps BPSK 1\/5 rate DVB-S2.<\/p>\n<p>Proposing these Uplinks<br \/>\n\u2022 Omni transponder: 5.651 GHz +\/- 0.5 MHz<br \/>\n\u2022 Directional transponder: 5.6575 GHz. +\/- 3.5 MHz<br \/>\n\u2022 Analog transponder: 5.665 GHz. +\/- 2 MHz<\/p>\n<p>A link budget is available at<br \/>\n<a href=\"https:\/\/drive.google.com\/folderview?id=0B3u-mSOWBMISYnZyZGJpeThKeU0&amp;usp=sharing\" >https:\/\/drive.google.com\/folderview?id=0B3u-mSOWBMISYnZyZGJpeThKeU0&amp;usp=sharing<\/a><\/p>\n<p>It is anticipated that a 1 or 2 metre dish will be required using the AMSAT designed ground station equipment.<\/p>\n<p>Source IARU Satellite Frequency Coordination Status pages <a href=\"http:\/\/www.amsat.org.uk\/iaru\/\" >http:\/\/www.amsat.org.uk\/iaru\/<\/a><\/p>\n<p>&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" alt=\"\" border=\"0\" src=\"https:\/\/pixel.wp.com\/b.gif?host=amsat-uk.org&#038;blog=41081109&#038;%23038;post=30639&#038;%23038;subd=ukamsat&#038;%23038;ref=&#038;%23038;feed=1\" width=\"1\" height=\"1\" \/><\/p>\n","protected":false},"excerpt":{"rendered":"<p>AMSAT-NA plan a satellite carrying transponders for 5 GHz to 10 GHz that is expected to launch into a Lunar orbit in September 2018. Heimdallr is a&nbsp;3 axis stabilized 6U CubeSat with a mass of approximately 8 kg. It will &hellip; <a href=\"https:\/\/amsat-uk.org\/2016\/09\/07\/5-ghz-to-10-ghz-lunar-transponder-mission\/\">Continue reading <span>&rarr;<\/span><\/a><img loading=\"lazy\" decoding=\"async\" alt=\"\" border=\"0\" src=\"https:\/\/pixel.wp.com\/b.gif?host=amsat-uk.org&amp;blog=41081109&amp;post=30639&amp;subd=ukamsat&amp;ref=&amp;feed=1\" width=\"1\" height=\"1\"><\/p>\n","protected":false},"author":51,"featured_media":615444,"comment_status":"closed","ping_status":"open","sticky":false,"template":"","format":"standard","meta":{"footnotes":""},"categories":[15],"tags":[],"class_list":["post-242727","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-AMSAT"],"_links":{"self":[{"href":"https:\/\/spaceweekly.com\/index.php?rest_route=\/wp\/v2\/posts\/242727","targetHints":{"allow":["GET"]}}],"collection":[{"href":"https:\/\/spaceweekly.com\/index.php?rest_route=\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/spaceweekly.com\/index.php?rest_route=\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/spaceweekly.com\/index.php?rest_route=\/wp\/v2\/users\/51"}],"replies":[{"embeddable":true,"href":"https:\/\/spaceweekly.com\/index.php?rest_route=%2Fwp%2Fv2%2Fcomments&post=242727"}],"version-history":[{"count":4,"href":"https:\/\/spaceweekly.com\/index.php?rest_route=\/wp\/v2\/posts\/242727\/revisions"}],"predecessor-version":[{"id":242852,"href":"https:\/\/spaceweekly.com\/index.php?rest_route=\/wp\/v2\/posts\/242727\/revisions\/242852"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/spaceweekly.com\/index.php?rest_route=\/wp\/v2\/media\/615444"}],"wp:attachment":[{"href":"https:\/\/spaceweekly.com\/index.php?rest_route=%2Fwp%2Fv2%2Fmedia&parent=242727"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/spaceweekly.com\/index.php?rest_route=%2Fwp%2Fv2%2Fcategories&post=242727"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/spaceweekly.com\/index.php?rest_route=%2Fwp%2Fv2%2Ftags&post=242727"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}