{"id":41306,"date":"2008-09-19T23:41:08","date_gmt":"2008-09-19T15:41:08","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/ils-proton-m-launches-with-canadas-nimiq-4\/"},"modified":"2008-09-19T23:41:08","modified_gmt":"2008-09-19T15:41:08","slug":"ils-proton-m-launches-with-canadas-nimiq-4","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/ils-proton-m-launches-with-canadas-nimiq-4\/","title":{"rendered":"ILS\u2019 Proton-M launches with Canada\u2019s Nimiq 4"},"content":{"rendered":"<p>International Launch Services (ILS) have launched their Proton M launch vehicle from Pad 39 (Area 200) at Baikonur Cosmodrome, Kazakhstan, carrying the Nimiq 4 satellite for Canada. Lift-off was recorded at 5:48 pm EDT.\n<\/p>\n<p>  NASASpaceflight.com is covering the launch as a live event, with background, live updates, images and a free launch video all available on the links below (read more).<br \/>\n<em><img fetchpriority=\"high\" decoding=\"async\" src=\"http:\/\/forum.nasaspaceflight.com\/forums\/get-attachment.asp?action=view&amp;attachmentid=9981\" border=\"0\" alt=\"\" hspace=\"5\" vspace=\"5\" width=\"600\" height=\"129\" align=\"left\"><\/em><\/p>\n<\/p>\n<p><em>**Proton-M\/Nimiq 4\u00c2&nbsp;\u2013 Live Update Pages**<\/em><\/p>\n<p><em>**Click here for the Proton-M\/Nimiq 4 launch video** <\/em><em>\u2013 available NOW\u2026<br \/>\n<\/em><em>(Video section is FREE, but you need to sign up as a member of the forum to enter the video section of the site. We only use your e-mail to send you your password. It will not be used for spam etc.)<\/em><\/p>\n<p><em>Proton-M\/Nimiq 4 Overview:<\/em><\/p>\n<p>The first three stages of the Proton will use a standard ascent trajectory to place the Breeze-M fourth stage and the Nimiq 4 satellite into a suborbital trajectory from which the Breeze M Upper Stage will then place itself and the spacecraft into a low Earth circular parking orbit.<\/p>\n<p>Once Nimiq 4 is in the parking orbit, it will be injected into a geosynchronous transfer orbit following four additional burns of the Breeze M.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" src=\"http:\/\/forum.nasaspaceflight.com\/index.php?action=dlattach;topic=4037.0;attach=96168;image\" border=\"0\" alt=\"\" hspace=\"5\" vspace=\"5\" width=\"147\" height=\"238\" align=\"left\">The Proton booster is 4.1 m (13.5 ft) in diameter along its second and third stages, with a first stage diameter of 7.3 m (24.0 ft). Overall height of the three stages of the Proton booster is 42.3 m (138.8 ft).<\/p>\n<p>The first stage consists of a central tank containing the oxidizer surrounded by six outboard fuel tanks. Each fuel tank also carries one of the six RD-275 engines that provide first stage power. Total first stage sea-level thrust is approximately 9.6 MN (2,158,000 lbf) with a vacuum-rated level thrust of 10.5 MN (2,360,000 lbf).<\/p>\n<p>The second stage is powered by three RD-0210 engines plus one RD-0211 engine and develops a vacuum thrust of 2.3 MN (517,000 lbf).<\/p>\n<p>The third stage is powered by one RD-0213 engine, this stage develops thrust of 583 kN (131,000 lbf), and a four-nozzle vernier engine that produces thrust of 31 kN (7,000 lbf).<\/p>\n<p>The Breeze M is powered by one pump fed gimbaled main engine that develops thrust of 19.6 kN (4,400 lbf). The Breeze-M is composed of a central core and a jettisonable additional propellant tank. Inert mass of the stage at lift-off is approximately 2,370 kg (5,225 lb).<\/p>\n<p>The quantity of propellant carried is dependent on specific mission requirements and is varied to maximize mission performance. The Breeze M is controlled by a closed loop, triple-redundant guidance system.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" src=\"http:\/\/forum.nasaspaceflight.com\/index.php?action=dlattach;topic=4037.0;attach=96169;image\" border=\"0\" alt=\"\" hspace=\"5\" vspace=\"5\" width=\"190\" height=\"180\" align=\"left\">Nimiq 4 has two payloads for Canadian broadcast services. The main payload will provide specialty television and foreign language programming.<\/p>\n<p>The second payload has six beams covering Canada for such advanced services as high-definition television. Nimiq satellites are dedicated to the provision of direct-to-home services for Bell TV.<\/p>\n<p>Nimiq 4 is a commercial communications satellite built by EADS Astrium. The main payload has 32 Ku-band channels providing specialty television and foreign language programming. The satellite will be located at 82 degrees West longitude.<\/p>\n<p>Nimiq 4 is based on the Eurostar-3000S version of the highly successful Eurostar communications satellite. It will have a launch mass of 4.8 tonnes, a solar array span of 39 meters once deployed in orbit, and spacecraft power of 12 kW at end of life.<\/p>\n<p>The double-floor E3000 model is equipped with an all-chemical propulsion system and Lithium-Ion batteries. The satellite, operating in geostationary orbit, will provide commercial services for a minimum of 15 years.<\/p>\n<p><em>Re-live the launch updates on the live event pages, linked above.<\/em><\/p>\n","protected":false},"excerpt":{"rendered":"<p>International Launch Services (ILS) have launched their Proton M launch vehicle from Pad 39 (Area 200) at Baikonur Cosmodrome, Kazakhstan, carrying the Nimiq 4 satellite for Canada. Lift-off was recorded at 5:48 pm EDT. NASASpaceflight.com is covering the launch as a live event, with background, live updates, images and a free launch video all available [&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":[],"class_list":["post-41306","post","type-post","status-publish","format-standard","hentry","category-news"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/41306"}],"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=41306"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/41306\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=41306"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=41306"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=41306"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}