{"id":12568,"date":"2020-03-27T01:58:47","date_gmt":"2020-03-26T17:58:47","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/atlas-5-launch-timeline-for-the-aehf-6-mission\/"},"modified":"2020-03-27T01:58:47","modified_gmt":"2020-03-26T17:58:47","slug":"atlas-5-launch-timeline-for-the-aehf-6-mission","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/atlas-5-launch-timeline-for-the-aehf-6-mission\/","title":{"rendered":"Atlas 5 launch timeline for the AEHF 6 mission"},"content":{"rendered":"<p>A United Launch Atlas 5 rocket is set to launch the U.S. Air Force\u2019s sixth and final Advanced Extremely High Frequency communications satellite from Cape Canaveral. This timeline shows the major mission events planned over a nearly six-hour flight to an optimized geostationary transfer orbit.<\/p>\n<p>The 197-foot-tall (60-meter) rocket, propelled by an RD-180 main engine and five solid rocket boosters, is set for liftoff during a two-hour launch window Thursday, March 26, that opens at 2:57 p.m. EDT (1857 GMT).<\/p>\n<p>The AEHF 5 mission will be the 83rd flight of an Atlas 5 rocket, and the second Atlas 5 launch of 2020.<\/p>\n<p>Built by Lockheed Martin, the AEHF 6 satellite joins five previous satellites in the AEHF constellation launched by Atlas 5 rockets in 2010, 2012, 2013, 2018 and 2019. The first four AEHF satellites in orbit allowed the Air Force\u2019s new generation of secure, nuclear-hardened voice, video and data relay spacecraft to span the globe, and the addition of two more AEHF geostationary relay satellite will grow the network\u2019s capacity and resiliency.<\/p>\n<p>The Atlas 5 launch sequence will last 5 hours, 40 minutes, from liftoff until deployment of the AEHF 6 spacecraft. On this mission, ULA added extra hardware and maneuvering fuel to the Centaur upper stage, enabling the launcher to deliver the AEHF 6 satellite closer to its final orbit more than 22,000 miles (nearly 36,000 kilometers) above the equator.<\/p>\n<p>The GSO kit was added to the Atlas 5 rocket on the fifth AEHF launch last August, after the first four AEHF missions did not employ the additional capability.<\/p>\n<p>The extra performance provided by the GSO kit will allow the Centaur upper stage to coast an additional two hours before its third firing. Spacecraft separation is scheduled for T+plus 5 hours, 40 minutes.<\/p>\n<p>Thanks to the mission profile change, the AEHF 6 satellite will separate in an orbit with a perigee, or low point, several thousand miles higher than would be possible without the GSO kit. That means AEHF 6 \u2014 like AEHF 5 last year \u2014 will need to consume less of its own finite propellant supply to circularize its orbit, leading to a longer operating lifetime for the mission.<\/p>\n<p>According to an Atlas 5 user\u2019s guide published by ULA, the GSO kit includes additional battery power, a full load of hydrazine to control the upper stage\u2019s orientation in space, and additional shielding over sensitive components, including the Centaur\u2019 hydrogen and oxygen tanks.<\/p>\n<p>An overview of the Atlas 5\/AEHF 6 launch sequence and a ground track map illustrating the rocket\u2019s path after liftoff are are posted below.<\/p>\n<p><iframe loading=\"lazy\" src=\"https:\/\/www.youtube.com\/embed\/tPfJq3aBJ6Y\" width=\"678\" height=\"381\" frameborder=\"0\" allowfullscreen=\"allowfullscreen\"><span data-mce-type=\"bookmark\" style=\"display: inline-block; width: 0px; overflow: hidden; line-height: 0;\" class=\"mce_SELRES_start\">\ufeff<\/span><\/iframe><\/p>\n<figure id=\"attachment_44244\" aria-describedby=\"caption-attachment-44244\" style=\"width: 1200px\" class=\"wp-caption alignnone\"><img fetchpriority=\"high\" decoding=\"async\" class=\"size-full wp-image-44244\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_map.jpg\" alt=\"\" width=\"1200\" height=\"747\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_map.jpg 1200w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_map-300x187.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_map-768x478.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_map-678x422.jpg 678w\" sizes=\"(max-width: 1200px) 100vw, 1200px\"><figcaption id=\"caption-attachment-44244\" class=\"wp-caption-text\">Credit: United Launch Alliance<\/figcaption><\/figure>\n<p><strong>T+0:00:01.1: Liftoff<\/strong><\/p>\n<figure id=\"attachment_31649\" aria-describedby=\"caption-attachment-31649\" style=\"width: 678px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-31649\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_1.jpg\" alt=\"\" width=\"678\" height=\"378\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_1.jpg 678w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_1-300x167.jpg 300w\" sizes=\"(max-width: 678px) 100vw, 678px\"><figcaption id=\"caption-attachment-31649\" class=\"wp-caption-text\">After igniting its RD-180 main engine at T-minus 2.7 seconds, the Atlas 5 rocket fires its five solid rocket boosters and rises away from Complex 41 at Cape Canaveral Air Force Station, Florida, with approximately 2.6 million pounds of thrust.<\/figcaption><\/figure>\n<p><strong>T+0:00:34.4: Mach 1<\/strong><\/p>\n<figure id=\"attachment_31650\" aria-describedby=\"caption-attachment-31650\" style=\"width: 678px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-31650\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_2.jpg\" alt=\"\" width=\"678\" height=\"378\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_2.jpg 678w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_2-300x167.jpg 300w\" sizes=\"auto, (max-width: 678px) 100vw, 678px\"><figcaption id=\"caption-attachment-31650\" class=\"wp-caption-text\">The Atlas 5 rocket exceeds the speed of sound, flying east from Cape Canaveral Air Force Station.<\/figcaption><\/figure>\n<p><strong>T+0:00:46.2: Max-Q<\/strong><\/p>\n<figure id=\"attachment_31651\" aria-describedby=\"caption-attachment-31651\" style=\"width: 678px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-31651\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_3.jpg\" alt=\"\" width=\"678\" height=\"315\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_3.jpg 678w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_3-300x139.jpg 300w\" sizes=\"auto, (max-width: 678px) 100vw, 678px\"><figcaption id=\"caption-attachment-31651\" class=\"wp-caption-text\">The Atlas 5 rocket passes through the region of maximum dynamic pressure during ascent through the lower atmosphere.<\/figcaption><\/figure>\n<p><strong>T+0:01:46.7: Jettison SRBs<\/strong><\/p>\n<figure id=\"attachment_31652\" aria-describedby=\"caption-attachment-31652\" style=\"width: 678px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-31652\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_4.jpg\" alt=\"\" width=\"678\" height=\"379\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_4.jpg 678w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/04\/a5_timeline_4-300x168.jpg 300w\" sizes=\"auto, (max-width: 678px) 100vw, 678px\"><figcaption id=\"caption-attachment-31652\" class=\"wp-caption-text\">Having burned out of propellant approximately 15 seconds earlier, the five spent Aerojet Rocketdyne-built solid rocket boosters are jettisoned once dynamic pressure conditions are satisfied. The first pair of boosters will jettison, followed a second-and-a-half later by the remaining three.<\/figcaption><\/figure>\n<p><strong>T+0:03:24.9: Payload Fairing Jettison<\/strong><\/p>\n<figure id=\"attachment_34917\" aria-describedby=\"caption-attachment-34917\" style=\"width: 800px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-34917\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_plfjettison.jpg\" alt=\"\" width=\"800\" height=\"451\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_plfjettison.jpg 800w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_plfjettison-300x169.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_plfjettison-768x433.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_plfjettison-678x381.jpg 678w\" sizes=\"auto, (max-width: 800px) 100vw, 800px\"><figcaption id=\"caption-attachment-34917\" class=\"wp-caption-text\">The Atlas 5 rocket\u2019s payload fairing, made in Switzerland by RUAG Space, is jettisoned in a clamshell-like fashion once external heating levels drop below predetermined limits after climbing through the dense lower atmosphere. The Forward Load Reactor deck that connected the payload fairing\u2019s structure to the Centaur upper stage is released five seconds after the shroud\u2019s jettison.<\/figcaption><\/figure>\n<p><strong>T+0:04:26.3: Main Engine Cutoff<\/strong><\/p>\n<figure id=\"attachment_34918\" aria-describedby=\"caption-attachment-34918\" style=\"width: 880px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-34918\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_beco.jpg\" alt=\"\" width=\"880\" height=\"491\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_beco.jpg 880w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_beco-300x167.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_beco-768x429.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_beco-678x378.jpg 678w\" sizes=\"auto, (max-width: 880px) 100vw, 880px\"><figcaption id=\"caption-attachment-34918\" class=\"wp-caption-text\">The RD-180 main engine completes its firing after consuming its kerosene and liquid oxygen fuel supply in the Atlas first stage.<\/figcaption><\/figure>\n<p><strong>T+0:04:32.3: Stage Separation<\/strong><\/p>\n<figure id=\"attachment_34919\" aria-describedby=\"caption-attachment-34919\" style=\"width: 877px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-34919\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_staging.jpg\" alt=\"\" width=\"877\" height=\"495\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_staging.jpg 877w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_staging-300x169.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_staging-768x433.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_staging-678x383.jpg 678w\" sizes=\"auto, (max-width: 877px) 100vw, 877px\"><figcaption id=\"caption-attachment-34919\" class=\"wp-caption-text\">The Common Core Booster first stage of the Atlas 5 rocket separates from the Centaur upper stage. Over the next few seconds, the Centaur engine liquid hydrogen and liquid oxygen systems are readied for ignition.<\/figcaption><\/figure>\n<p><strong>T+0:04:42.3: Centaur Ignition 1<\/strong><\/p>\n<figure id=\"attachment_34920\" aria-describedby=\"caption-attachment-34920\" style=\"width: 881px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-34920\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes1.jpg\" alt=\"\" width=\"881\" height=\"495\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes1.jpg 881w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes1-300x169.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes1-768x432.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes1-678x381.jpg 678w\" sizes=\"auto, (max-width: 881px) 100vw, 881px\"><figcaption id=\"caption-attachment-34920\" class=\"wp-caption-text\">The Centaur RL10C-1 engine ignites for the first of three upper stage firings. This burn will inject the Centaur stage and the AEHF 6 satellite into an initial parking orbit.<\/figcaption><\/figure>\n<p><strong>T+0:11:46.9: Centaur Cutoff 1<\/strong><\/p>\n<figure id=\"attachment_34921\" aria-describedby=\"caption-attachment-34921\" style=\"width: 879px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-34921\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco1.jpg\" alt=\"\" width=\"879\" height=\"493\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco1.jpg 879w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco1-300x168.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco1-768x431.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco1-678x381.jpg 678w\" sizes=\"auto, (max-width: 879px) 100vw, 879px\"><figcaption id=\"caption-attachment-34921\" class=\"wp-caption-text\">The Centaur engine shuts down after arriving in a planned low-Earth parking orbit. The vehicle enters an 11-minute coast period before arriving at the required location in space for the second burn.<\/figcaption><\/figure>\n<p><strong>T+0:22:44.3:<\/strong><strong> Centaur Ignition 2<\/strong><\/p>\n<figure id=\"attachment_34922\" aria-describedby=\"caption-attachment-34922\" style=\"width: 880px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-34922\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes2.jpg\" alt=\"\" width=\"880\" height=\"494\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes2.jpg 880w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes2-300x168.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes2-768x431.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmes2-678x381.jpg 678w\" sizes=\"auto, (max-width: 880px) 100vw, 880px\"><figcaption id=\"caption-attachment-34922\" class=\"wp-caption-text\">Producing 22,900 pounds of thrust, the Centaur re-ignites to accelerate the AEHF 6 payload into a highly elliptical transfer orbit from the parking altitude achieved earlier in the launch sequence. This burn lasts more than six minutes.<\/figcaption><\/figure>\n<p><strong>T+0:28:52.7: Centaur Cutoff 2<\/strong><\/p>\n<figure id=\"attachment_34923\" aria-describedby=\"caption-attachment-34923\" style=\"width: 879px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-34923\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco2.jpg\" alt=\"\" width=\"879\" height=\"493\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco2.jpg 879w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco2-300x168.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco2-768x431.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2018\/10\/av073_centaurmeco2-678x381.jpg 678w\" sizes=\"auto, (max-width: 879px) 100vw, 879px\"><figcaption id=\"caption-attachment-34923\" class=\"wp-caption-text\">The second Centaur firing places the AEHF 6 satellite into an elliptical transfer orbit stretching more than 20,000 miles above Earth, beginning a five-hour coast period for the mission\u2019s final orbital adjustment maneuver. A secondary U.S. Air Force smallsat payload named TDO 2 will separate from the Centaur upper stage\u2019s aft bulkhead around 30 seconds after the RL10 engine shuts down. The&nbsp;TDO 2 mission support space domain awareness through optical calibration and satellite laser ranging.<\/figcaption><\/figure>\n<p><strong>T+5:36:39.1: Centaur Ignition 3<\/strong><\/p>\n<figure id=\"attachment_44245\" aria-describedby=\"caption-attachment-44245\" style=\"width: 900px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-44245\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_mes3_.jpg\" alt=\"\" width=\"900\" height=\"508\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_mes3_.jpg 900w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_mes3_-300x169.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_mes3_-768x433.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_mes3_-678x383.jpg 678w\" sizes=\"auto, (max-width: 900px) 100vw, 900px\"><figcaption id=\"caption-attachment-44245\" class=\"wp-caption-text\">After a five-hour coast, the Centaur\u2019s RL10 engine reignites for a roughly one-minute, 28-second firing to place the AEHF 6 satellite in the proper orbit for spacecraft separation.<\/figcaption><\/figure>\n<p><strong>T+5:38:07.8: Centaur Cutoff 3<\/strong><\/p>\n<figure id=\"attachment_44246\" aria-describedby=\"caption-attachment-44246\" style=\"width: 900px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-44246\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_meco3.jpg\" alt=\"\" width=\"900\" height=\"501\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_meco3.jpg 900w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_meco3-300x167.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_meco3-768x428.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf_meco3-678x377.jpg 678w\" sizes=\"auto, (max-width: 900px) 100vw, 900px\"><figcaption id=\"caption-attachment-44246\" class=\"wp-caption-text\">The powered phase of flight is concluded as the Centaur reaches the planned elliptical geostationary transfer orbit with an expected perigee, or low point, of 6,758 miles (10,876 kilometers), an apogee, or high point, of 21,933 miles (35,298 kilometers), and an inclination of 13.9 degrees. The final RL10 engine burn will fire until depletion of the Centaur upper stage\u2019s propellant, giving the AEHF 6 satellite the most favorable orbit possible before spacecraft separation.<\/figcaption><\/figure>\n<p><strong>T+5:40:56.9: AEHF 6 Separation<\/strong><\/p>\n<figure id=\"attachment_44247\" aria-describedby=\"caption-attachment-44247\" style=\"width: 900px\" class=\"wp-caption alignnone\"><img loading=\"lazy\" decoding=\"async\" class=\"size-full wp-image-44247\" src=\"http:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_sep.jpg\" alt=\"\" width=\"900\" height=\"506\" srcset=\"https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_sep.jpg 900w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_sep-300x169.jpg 300w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_sep-768x432.jpg 768w, https:\/\/spaceflightnow.com\/wp-content\/uploads\/2020\/03\/aehf6_sep-678x381.jpg 678w\" sizes=\"auto, (max-width: 900px) 100vw, 900px\"><figcaption id=\"caption-attachment-44247\" class=\"wp-caption-text\">The AEHF 6 spacecraft deploys from the Centaur upper stage.<\/figcaption><\/figure>\n<p><b><i>Email the author.<\/i><\/b><\/p>\n<p><em><strong>Follow Stephen Clark on Twitter: @StephenClark1.<\/strong><\/em><\/p>\n","protected":false},"excerpt":{"rendered":"<p>A United Launch Atlas 5 rocket is set to launch the U.S. Air Force\u2019s sixth and final Advanced Extremely High Frequency communications satellite from Cape Canaveral. This timeline shows the major mission events planned over a nearly six-hour flight to an optimized geostationary transfer orbit. The 197-foot-tall (60-meter) rocket, propelled by an RD-180 main engine [&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":[2278,864,1056,1709,724,2279,1708,1608],"class_list":["post-12568","post","type-post","status-publish","format-standard","hentry","category-news","tag-aehf-6","tag-aerojet-rocketdyne","tag-air-force-research-laboratory","tag-aj-60a","tag-atlas-5","tag-av-086","tag-complex-41","tag-cubesats"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/12568"}],"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=12568"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/12568\/revisions"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=12568"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=12568"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=12568"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}