{"id":24381,"date":"2023-01-26T00:49:54","date_gmt":"2023-01-25T16:49:54","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/japan-begins-busy-year-with-classified-igs-radar-7-launch\/"},"modified":"2023-01-26T00:49:54","modified_gmt":"2023-01-25T16:49:54","slug":"japan-begins-busy-year-with-classified-igs-radar-7-launch","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/japan-begins-busy-year-with-classified-igs-radar-7-launch\/","title":{"rendered":"Japan begins busy year with classified IGS-Radar 7 launch"},"content":{"rendered":"<p>The Japan Aerospace Exploration Agency (JAXA) and Mitsubishi Industries have conducted the nation\u2019s first orbital flight of 2023. The mission saw an H-IIA rocket carry the classified IGS-7 radar reconnaissance satellite into a Sun-synchronous orbit.<\/p>\n<p>Liftoff occurred on Thursday, Jan. 26, 2023, at 01:49:20 UTC from Launch Area Y1 at the Tanegashima Space Center in southern Japan.&nbsp; The launch window lasted just 61 seconds, closing at 01:50:21 UTC.<\/p>\n<p>The mission is the first of several planned orbital launches for Japan in 2023; however, that flight rate hinges not just on payload availability but on the successful introduction of the H3 rocket, currently slated for no earlier than February 12, 2023.<\/p>\n<\/p>\n<p><b>IGS-Radar 7<\/b><\/p>\n<p>The payload for this classified H-IIA mission was the IGS (Intelligence Gathering Satellite) 7 spacecraft for the Japanese government\u2019s Cabinet Satellite Information Center.<\/p>\n<p>Reports indicate a ground resolution of less than one meter for the Synthetic Aperture Radar (SAR) series of the overall IGS program, which also includes a series of optical satellites.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" aria-describedby=\"caption-attachment-56726\" class=\"size-full wp-image-56726\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/2018-06-11-231614.jpg\" alt=\"\" width=\"1155\" height=\"833\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/2018-06-11-231614.jpg 1155w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/2018-06-11-231614-350x252.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/2018-06-11-231614-485x350.jpg 485w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2018\/06\/2018-06-11-231614-768x554.jpg 768w\" sizes=\"(max-width: 1155px) 100vw, 1155px\"><\/p>\n<p id=\"caption-attachment-56726\" class=\"wp-caption-text\">Render of a second-generation IGS radar satellite. (Credit: p-island.com &amp; S. Matsuura)<\/p>\n<p>The newer generations of the system launched since 2015 have been capable of resolutions down to 30 cm for the optical range and 50 cm for the SAR range.<\/p>\n<p>Space Technology<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>Space tourism guides<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>Rocket building kits<path d=\"M7.59009 18.59L9.00009 20L17.0001 12L9.00009 4L7.59009 5.41L14.1701 12\" style=\"animation: initial !important; background: initial !important; border: 0px !important; box-shadow: none !important; color: inherit !important; cursor: inherit !important; direction: inherit !important; display: inline !important; fill: currentcolor !important; filter: initial !important; float: none !important; margin: 0px !important; opacity: initial !important; outline: 0px !important; overflow: initial !important; padding: 0px !important; stroke: initial !important; transform: initial !important; vertical-align: initial !important; visibility: inherit !important;\"><\/path>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>The IGS program was created in response to the 1988 North Korean missile test over Japan.&nbsp; The network is tasked, in large part, with providing early warning of impending hostile missile launches.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>IGS-Radar 7 Updates<\/li>\n<li>Japanese Section<\/li>\n<li>L2 Master Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>Information from the satellites is also used as part of civil natural disaster monitoring and response.<\/p>\n<p>The exact orbital parameters were not known prior to launch; however, past IGS missions indicate a Sun-synchronous orbit with a perigee between 475 and 500 km and an apogee between 500 to 515 km with an inclination of approximately 97.4\u00b0.<\/p>\n<p><b>H-IIA\u2019s Retirement Year<\/b><\/p>\n<p>Taking IGS-Radar 7 to orbit \u2014 as it has for all the other IGS missions \u2014 was the H-IIA rocket.<\/p>\n<p>Operated by Mitsubishi Heavy Industries for JAXA, the H-IIA entered service on August 29, 2001. Four variants of the rocket have flown over the course of its career \u2014 though only one variant remains today.<\/p>\n<p>The H-IIA flew this mission in the H2A 202 configuration, with the first number denoting the number of stages (2), the second representing the number of liquid-fueled boosters (0), and the third representing the number of SRB-A solid rocket boosters (2).<\/p>\n<p>Just before liftoff, the H-IIA commanded the single LE-7A liquid engine on the hydrogen-oxygen first stage to ignite and build up to full thrust.&nbsp; After a brief series of health checks, commands were sent to simultaneously ignite the two SRB-A solid rocket boosters, release the rocket, and disconnect the T0 umbilicals \u2014 committing the vehicle to flight.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-82904\" class=\"size-full wp-image-82904\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-scaled.jpg\" alt=\"\" width=\"2560\" height=\"1707\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-scaled.jpg 2560w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-350x233.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-525x350.jpg 525w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-768x512.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-1920x1280.jpg 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-1170x780.jpg 1170w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-585x390.jpg 585w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/12\/FCl7ZQ1VEAEH6Qm-263x175.jpg 263w\" sizes=\"(max-width: 2560px) 100vw, 2560px\"><\/p>\n<p id=\"caption-attachment-82904\" class=\"wp-caption-text\">Launch of H-IIA F44. (Credit: MHI Launch Services)<\/p>\n<p>The twin SRB-As burned hydroxyl-terminated polybutadiene for 120 seconds before burning out and separating, leaving the first stage\u2019s approximately 1,098 kN of thrust (247,000 lbf or 112 tonnes-force) to continue pushing the stack toward orbit.<\/p>\n<p>After a 390-second burn, the first stage shut down and handed off to the rocket\u2019s hydrogen-oxygen second stage, which used its single LE-5B engine to finish the climb to orbit.<\/p>\n<p>The LE-5B engine produces approximately 137 kN of thrust (31,000 lbf or 14 tonnes-force).<\/p>\n<p>After the IGS-Radar 7 mission, only four H-IIA missions remain as the rocket is set to retire on its 50th mission.<\/p>\n<p>That retirement flight is currently planned for this year.<\/p>\n<p><b>H3 Development<\/b><\/p>\n<p>The H3 rocket is set to succeed the H-IIA, introducing numerous improvements and performance boosts while lowering the overall cost of the system.<\/p>\n<p>The H3 is currently tracking toward a debut launch no earlier than Feb. 12, 2023, in a window that opens at 01:37:55 UTC and closes at 01:44:15 UTC.<\/p>\n<p>The rocket is currently stacked in the vertical integration facility at the launch site after undertaking a static fire campaign on the launch pad in November 2022.&nbsp;<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-80106\" class=\"size-full wp-image-80106\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1.jpg\" alt=\"\" width=\"1299\" height=\"866\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1.jpg 1299w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1-350x233.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1-525x350.jpg 525w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1-768x512.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1-1170x780.jpg 1170w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1-585x390.jpg 585w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2021\/09\/h3_topics_20210322-1-1-263x175.jpg 263w\" sizes=\"(max-width: 1299px) 100vw, 1299px\"><\/p>\n<p id=\"caption-attachment-80106\" class=\"wp-caption-text\">The H3 rocket mounted on LC-Y Pad 2 ahead of its wet-dress rehearsal in early 2022. (Credit: JAXA)<\/p>\n<p>After initial installation, the second of the two SRB-3 boosters was reattached in late December after inspections on the H3 liquid core stage were needed.<\/p>\n<p>The first mission will carry the ALOS-3 (Advanced Land Observing Satellite 3) into a Sun-synchronous orbit.&nbsp; The rocket will fly in its H3-22S configuration.<\/p>\n<p>The final three digits of each H3 mission denote the rocket configuration.&nbsp; The first number indicates the number of first-stage LE-9 engines (2 or 3), the second digit signifies the number of SRB-3 boosters, and the final digit is either \u201cS,\u201d \u201cL,\u201d or \u201cW\u201d for the payload fairing.<\/p>\n<p>The \u201cS\u201d is for a short fairing at 10.4 m long, and \u201cL\u201d is for the long fairing at 16.4 m. Both the short and long fairings are 5.2 m in diameter.<\/p>\n<p>The \u201cW\u201d designation is for a wider 5.4 m diameter fairing that is the same length as the long variant.<\/p>\n<p>For its first mission, the H3-22S will fly with a two-engine first stage, two SRB-3 boosters, and a short fairing.<\/p>\n<p>Only three total propulsion configurations for the H3 are possible: H3-30, H3-22, and H3-24.<\/p>\n<p>The first stage will carry 225 tonnes of propellant and oxidizer, while the second stage will carry 23 tonnes of propellant and oxidizer.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-91422\" class=\"size-full wp-image-91422\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2023\/01\/H3-launch-jun-2020-15-NSF.png\" alt=\"\" width=\"4000\" height=\"2400\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2023\/01\/H3-launch-jun-2020-15-NSF.png 4000w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2023\/01\/H3-launch-jun-2020-15-NSF-350x210.png 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2023\/01\/H3-launch-jun-2020-15-NSF-583x350.png 583w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2023\/01\/H3-launch-jun-2020-15-NSF-768x461.png 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2023\/01\/H3-launch-jun-2020-15-NSF-1920x1152.png 1920w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2023\/01\/H3-launch-jun-2020-15-NSF-1170x702.png 1170w\" sizes=\"(max-width: 4000px) 100vw, 4000px\"><\/p>\n<p id=\"caption-attachment-91422\" class=\"wp-caption-text\">Rendering of the H3 rocket in flight, sporting 4 SRB-3 boosters in its H3-24L configuration. (Credit: Mack Crawford for NSF\/L2)<\/p>\n<p>The first stage\u2019s LE-9 engines burn hydrogen and oxygen, with the two-engine variant producing 2,942 kN of thrust (661,000 lbf or 300 tonnes force) whereas the three-engine variant will produce 4,413 kN of thrust (992,000 lbf or 450 tonnes force).<\/p>\n<p>The H3\u2019s upper stage\u2019s LE-5B-3 engine will produce 137 kN of thrust (31,000 lbf or 14 tonnes-force).<\/p>\n<p><b>HTV-X<\/b><\/p>\n<p>While the H3 rocket will be a versatile vehicle in terms of the payloads it will launch, a main customer is JAXA\u2019s upcoming HTV-X cargo resupply craft for the International Space Station.&nbsp;<\/p>\n<p>HTV-X is a follow-on and upgraded version of the H-II transfer vehicle which flew from 2009 to 2020.<\/p>\n<p>HTV-X will sport a 16 metric ton launch mass (comparable to HTV), with a payload-to-ISS capacity of 4.07 t in the pressurized volume and 1.75 t in the unpressurized section.<\/p>\n<p>The pressurized section of HTV-X measures 78 cubic meters \u2014 far exceeding HTV\u2019s pressurized volume of 14 cubic meters.<\/p>\n<p>The craft will be capable of remaining docked to the ISS for up to six months, double the length of its predecessor.&nbsp; HTV-X will also be able to remain in orbit after leaving the ISS for up to 18 months to serve as a free-flying space station and technology demonstration platform.<\/p>\n<p>HTV-X\u2019s first launch, assuming the first year of operational service of the H3 rocket is successful, is currently planned for no earlier than January 2024.<\/p>\n<p><em>(Lead image: An H-IIA rocket prepares for flight ahead of a previous mission. Credit: JAXA)<\/em><\/p>\n","protected":false},"excerpt":{"rendered":"<p>The Japan Aerospace Exploration Agency (JAXA) and Mitsubishi Industries have conducted the nation\u2019s first orbital flight of 2023. The mission saw an H-IIA rocket carry the classified IGS-7 radar reconnaissance satellite into a Sun-synchronous orbit. Liftoff occurred on Thursday, Jan. 26, 2023, at 01:49:20 UTC from Launch Area Y1 at the Tanegashima Space Center in [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":0,"comment_status":"","ping_status":"","sticky":false,"template":"","format":"standard","meta":{"_acf_changed":false,"inline_featured_image":false,"footnotes":"","_links_to":"","_links_to_target":""},"categories":[2],"tags":[8087,876,377,3876],"class_list":["post-24381","post","type-post","status-publish","format-standard","hentry","category-news","tag-h-iia","tag-h3","tag-japan","tag-tanegashima"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/24381"}],"collection":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts"}],"about":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/types\/post"}],"author":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/users\/1"}],"replies":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/comments?post=24381"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/24381\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=24381"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=24381"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=24381"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}