{"id":37957,"date":"2019-07-30T23:24:19","date_gmt":"2019-07-30T15:24:19","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/soyuz-2-1a-launches-meridian-8-out-of-plesetsk\/"},"modified":"2019-07-30T23:24:19","modified_gmt":"2019-07-30T15:24:19","slug":"soyuz-2-1a-launches-meridian-8-out-of-plesetsk","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/soyuz-2-1a-launches-meridian-8-out-of-plesetsk\/","title":{"rendered":"Soyuz 2-1a launches Meridian 8 out of Plesetsk"},"content":{"rendered":"<p>Russia\u2019s Soyuz rocket carried a Meridian communications satellite to orbit Tuesday morning. The rocket\u2019s Fregat upper stage deployed its payload into an elliptical orbit about 140 minutes after liftoff from the Plesetsk Cosmodrome, which took place at 08:56 Moscow Time (05:56 UTC).\n<\/p>\n<p>Meridian forms part of the Russian Government\u2019s fleet of communications satellites, operating in elliptical Molniya orbits that enable near-continuous coverage of high northern latitudes. Meridian compliments the geostationary Raduga and Globus communications satellites.<\/p>\n<p>Meridian No.18L is the eighth satellite to be launched for the Meridian system. It is the first of a new batch of four satellites ordered in 2016 to replenish the constellation after a next-generation replacement was delayed.<\/p>\n<p>Following the same design as the earlier Meridian satellites, it is based around a pressurized, three-axis-stabilized bus developed by ISS Reshetnev, likely related to the Uragan-M series of navigation satellites. Each Meridian is designed to operate for at least seven years.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" aria-describedby=\"caption-attachment-62465\" class=\"wp-image-62465 size-large\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-03-41-522-535x350.jpg\" alt=\"\" width=\"535\" height=\"350\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-03-41-522-535x350.jpg 535w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-03-41-522-350x229.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-03-41-522-768x503.jpg 768w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-03-41-522.jpg 793w\" sizes=\"(max-width: 535px) 100vw, 535px\"><\/p>\n<p id=\"caption-attachment-62465\" class=\"wp-caption-text\">One of only a handful of renderings of a Meridian satellite \u2013 via NPO PM<\/p>\n<p>The first Meridian satellite, No.11L, was successfully deployed in December 2006, however by the time of the next satellite\u2019s launch in May 2009 it had ceased to function. The second satellite was placed into too low an orbit after the upper stage of its carrier rocket malfunctioned, although some operation may still have been possible.<\/p>\n<p>Further launches occurred in November 2010, May and December 2011, November 2012 and October 2014. The December 2011 launch failed to reach orbit after an engine problem and apparent explosion affecting the third stage of the Soyuz rocket that had been performing that mission.<\/p>\n<p>The other three satellites ordered in the same block as Meridian No.18L are expected to launch over the next few years. At least one further Meridian launch is scheduled to take place in 2019.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>Soyuz 2-1a Launch Updates<\/li>\n<li>Russian Forum Section<\/li>\n<li>L2 Russian Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>The Molniya orbit that Meridian uses is a particular regime of highly elliptical orbit with a perigee \u2013 or low point \u2013 relatively close to the Earth and the apogee \u2013 its highest point \u2013 far above so that the spacecraft takes just under 12 hours to complete a revolution. This period \u2013 about half a sidereal day (the time taken for the Earth to rotate on its axis, relative to the stars) \u2013 means a satellite can reach apogee twice a day, over the same points on the surface.<\/p>\n<p>NASA mission updates<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>Spaceflight news subscription<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>NASA mission patches<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>Because the orbit is highly elliptical from the ground a satellite would appear to spend most of its time close to apogee, making it easier to track with an antenna. Orbital inclination of about 63.4 degrees places the apogee over the polar regions, but also cancels out perturbations and freezes the apogee and perigee of the orbit relative to the Earth\u2019s surface.<\/p>\n<p>The majority of communications satellites operate in geostationary orbit over the equator, where they remain in fixed positions relative to the surface. At high latitudes, these satellites are so close to the horizon that signals can easily become obstructed or be disrupted by atmospheric or thermal effects. Close to the poles, geostationary satellites may be below the horizon altogether. Satellites in Molniya orbit appear higher in the sky at these latitudes, allowing reliable communications links to be established.<\/p>\n<p>Meridian satellites use orbits with apogees between 38,000 and 39,000 kilometres (23,600 to 24,200 miles, 20,500 to 21,100 nautical miles) and perigees between 1,480 and 2,220 kilometres (920 to 1,370 miles, 800 to 1,190 nautical miles). Tuesday\u2019s launch will have injected Meridian No.18L close to its operational orbit: the satellite will maneuver into its final position under its own power at a later date before it enters service.<\/p>\n<p>The Molniya orbit is named after the Molniya series of satellites developed by the Soviet Union, its name coming from the Russian word for Lightning. Launched between 1964 and 2005, three generations of Molniya satellites were used for multiple forms of communications including telephony, television and military applications. Meridian is the successor to the military aspect of the Molniya constellation.<\/p>\n<p>Molniya also gave its name to the Molniya rocket, a four-stage vehicle derived from Sergei Korolev\u2019s R-7 missile which was used to launch these satellites, as well as early interplanetary probes and US-K missile early warning satellites. An ancestor of the Soyuz rocket that was used for Tuesday\u2019s launch, Molniya continued to fly in its upgraded Molniya-M form until its retirement in 2010.<\/p>\n<p>The Meridian No.18L satellite launched aboard a Soyuz-2-1a rocket with a Fregat-M upper stage. The three-stage Soyuz-2-1a booster is one of three types of Soyuz-2 vehicle, which represent the latest version of Russia\u2019s legendary Soyuz rocket.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-62466\" class=\"size-full wp-image-62466\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-06-41-341.jpg\" alt=\"\" width=\"1080\" height=\"588\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-06-41-341.jpg 1080w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-06-41-341-350x191.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-06-41-341-630x343.jpg 630w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-06-41-341-768x418.jpg 768w\" sizes=\"(max-width: 1080px) 100vw, 1080px\"><\/p>\n<p id=\"caption-attachment-62466\" class=\"wp-caption-text\">Soyuz 2-1a on a previous launch \u2013 via Roscosmos<\/p>\n<p>First flown in November 1966 Soyuz was an improved version of the Voskhod rocket \u2013 itself a three-stage version of Molniya that had been used in the Voskhod human spaceflight program and in support of unmanned reconnaissance missions. Soyuz, Molniya and Voskhod all trace their heritage back to Korolev\u2019s R-7, which in 1957 became the first intercontinental ballistic missile (ICBM) to fly in and \u2013 later that year \u2013 launched the first satellite, Sputnik.<\/p>\n<p>Upgrades on the Soyuz-2-1a over the previous-generation Soyuz-U included modernized first and second stage engines as well as a new digital flight control system. Its stablemate, Soyuz-2-1b, incorporates a more powerful third stage engine to accommodate heavier payloads, while the smaller Soyuz-2-1v is a heavily modified two-stage version optimized for lighter payloads.<\/p>\n<p>Tuesday\u2019s launch saw Soyuz lift off from Pad 4 at Site 43 of the Plesetsk Cosmodrome in northern Russia. Russia\u2019s main military launch site, Plesetsk\u2019s four Soyuz launch pads were originally built to support testing and operational deployment of R-7A missiles, undergoing conversion for satellite launches after the missile\u2019s retirement.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-62467\" class=\"size-full wp-image-62467\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-08-29-282.jpg\" alt=\"\" width=\"914\" height=\"598\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-08-29-282.jpg 914w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-08-29-282-350x229.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-08-29-282-535x350.jpg 535w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-08-29-282-768x502.jpg 768w\" sizes=\"(max-width: 914px) 100vw, 914px\"><\/p>\n<p id=\"caption-attachment-62467\" class=\"wp-caption-text\">A Soyuz 2-1 rocket is prepared for its mission at the Plesetsk Cosmodrome \u2013 via Russian military<\/p>\n<p>Site 43\/4 is the only one of the four pads currently in service: the nearby Site 43\/3 was last used in 2002 but is in the final stages of renovation, while Site 41\/1 has been demolished and Site 16\/2 was earmarked for a future upgrade and return to operation. Soyuz can also launch from the Baikonur Cosmodrome in Kazakhstan, the Vostochny Cosmodrome in Russia\u2019s far East, and the Centre Spatial Guyanais in Kourou, French Guiana.<\/p>\n<p>All three stages of the Soyuz vehicle burned RG-1 propellant oxidized by liquid oxygen. About sixteen seconds before liftoff the four RD-107A engines of the first stage \u2013 and the single RD-108A engine powering the second stage \u2013 would have ignited. Over the final seconds of the countdown, these engines built up to full thrust. At the zero-second mark, the launch pad\u2019s swing arms came open and Soyuz climbed away from Plesetsk under the power of the first two stages burning together.<\/p>\n<p>The first stage of Soyuz consisted of four boosters clustered around the second stage, with one engine per booster. These were designated Blok-B, V, G and D, while the second stage was designated Blok-A. Its RD-108A engine featured additional vernier chambers to assist in controlling the rocket\u2019s attitude but was otherwise identical to the first stage RD-107As.<\/p>\n<p>The five engines burned together for about 118 seconds when the first stage burned out and separated. As the boosters separate from the second stage, they vented residual oxygen from the nose to push themselves away from the vehicle, forming a pattern known as the Korolev Cross after the rocket\u2019s chief designer.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-62468\" class=\"size-full wp-image-62468\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-10-34-287.jpg\" alt=\"\" width=\"1075\" height=\"597\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-10-34-287.jpg 1075w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-10-34-287-350x194.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-10-34-287-630x350.jpg 630w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-10-34-287-768x427.jpg 768w\" sizes=\"(max-width: 1075px) 100vw, 1075px\"><\/p>\n<p id=\"caption-attachment-62468\" class=\"wp-caption-text\">Soyuz booster sep from a Soyuz 2-1 during an Arianespace launch<\/p>\n<p>After first stage separation, Soyuz\u2019s second stage continued to burn for another 170 seconds. At the end of its burn, the third stage ignited in the normal \u201cfire-in-the-hole\u201d sequence, lighting while the second stage was still firing to keep the propellant settled in its tank.<\/p>\n<p>Exhaust gases from third stage ignition escaped through a lattice structure at the top of the second stage, with separation occurring as soon as the third stage was up and burning. A second and a half later, the top part of the interstage structure separated from the base of the third stage.<\/p>\n<p>The third stage of Soyuz was powered by a single RD-0110 engine. It burned for about four minutes, placing Fregat and Meridian No.18L onto an initial suborbital trajectory. At shutdown Fregat separated and took over, igniting about a minute later for a very short burn to complete insertion into an initial parking orbit. About 36 minutes later Fregat restarted for a ten-minute burn to raise the orbit\u2019s apogee.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" aria-describedby=\"caption-attachment-62469\" class=\"size-full wp-image-62469\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-11-50-423.jpg\" alt=\"\" width=\"1141\" height=\"706\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-11-50-423.jpg 1141w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-11-50-423-350x217.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-11-50-423-566x350.jpg 566w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-11-50-423-180x110.jpg 180w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2019\/07\/NSF-2019-07-30-05-11-50-423-768x475.jpg 768w\" sizes=\"(max-width: 1141px) 100vw, 1141px\"><\/p>\n<p id=\"caption-attachment-62469\" class=\"wp-caption-text\">Fregat Upper Stage during an ESA mission<\/p>\n<p>After another coast phase, lasting over eighty minutes, a short third burn was made to raise the perigee. With all three burns complete, Meridian No.18L separated from Fregat to begin its mission. Half an hour later Fregat made a final burn to deorbit itself, minimizing debris left in orbit from Tuesday\u2019s mission.<\/p>\n<p>The Fregat-M stage used for Tuesday\u2019s launch was an upgraded version of the original Fregat, powered by an S5.98M engine that burned unsymmetrical dimethylhydrazine and dinitrogen tetroxide.<\/p>\n<p>Tuesday\u2019s launch was the twelfth for a Russian rocket in 2019, coming ten days after the successful launch of the crewed Soyuz MS-13 mission to the International Space Station aboard a Soyuz-FG rocket from Baikonur. Russia\u2019s next Soyuz launch is currently scheduled to take place tomorrow, with a Soyuz-2-1a vehicle carrying the Progress MS-12 cargo spacecraft, also bound for the space station.<\/p>\n","protected":false},"excerpt":{"rendered":"<p>Russia\u2019s Soyuz rocket carried a Meridian communications satellite to orbit Tuesday morning. The rocket\u2019s Fregat upper stage deployed its payload into an elliptical orbit about 140 minutes after liftoff from the Plesetsk Cosmodrome, which took place at 08:56 Moscow Time (05:56 UTC). Meridian forms part of the Russian Government\u2019s fleet of communications satellites, operating 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":[2318,1302],"class_list":["post-37957","post","type-post","status-publish","format-standard","hentry","category-news","tag-meridian","tag-soyuz"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/37957"}],"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=37957"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/37957\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=37957"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=37957"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=37957"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}