{"id":39186,"date":"2015-11-28T01:36:12","date_gmt":"2015-11-27T17:36:12","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/nasa-identifies-secondary-payloads-for-slss-em-1-mission\/"},"modified":"2015-11-28T01:36:12","modified_gmt":"2015-11-27T17:36:12","slug":"nasa-identifies-secondary-payloads-for-slss-em-1-mission","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/nasa-identifies-secondary-payloads-for-slss-em-1-mission\/","title":{"rendered":"NASA identifies secondary payloads for SLS\u2019s EM-1 mission"},"content":{"rendered":"<p>As NASA continues to progress toward the debut flight of SLS in 2018, the agency is now examining additional secondary payloads to fly on the EM-1 mission. These secondary payloads will involve Cubesats designed to investigate lunar and human biology aspects of spaceflight as well as Near Earth Asteroid reconnaissance.<\/p>\n<p>EM-1 secondary payloads:<\/p>\n<p>A major factor contributing to the decision to co-manifest small Cubesat payloads on the EM-1 (Exploration Mission -1) flight of SLS and Orion in 2018 stems from the identification of Strategic Knowledge Gaps (SKGs) that need to\/should be addressed prior to undertaking human missions into the inner solar system.<\/p>\n<p>The SKGs identified by the Human Exploration Operations Mission Directorate\u2019s (HEOMD\u2019s) Advanced Exploration Systems (AES) division relate to \u201chuman health\/performance in high-radiation environments, lunar resource potential, and human NEA mission target identification and interaction with NEA surface.\u201d<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>SLS Forum Section<\/li>\n<li>L2 SLS Section<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>Based on the identified SKGs, the HEOMD AES has chosen three concepts for further refinement toward inclusion on the EM-1 flight.<\/p>\n<p>These three concepts include BioSential, Lunar Flashlight, and Near Earth Asteroid Scout.<\/p>\n<p>All three were chosen from the same set of criteria: \u201cRelevance to Space Exploration SKGs, life cycle cost, synergistic use of previously demonstrated technologies, and optimal use of available civil servant workforce.\u201d<\/p>\n<p>BioSential:<\/p>\n<p>Aerospace &amp; Defense<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>SpaceX<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 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>\n<p>     (adsbygoogle = window.adsbygoogle || []).push({});<\/p>\n<p>BioSential will specifically address the SKG relating to human health and performance in high radiation environments, notes the HEOMD AES presentation from 4 November 2015.<\/p>\n<p>BioSential\u2019s design will allow it to \u201cStudy radiation-induced DNA damage of live organisms in cislunar space\u201d and \u201ccorrelate [those] measurements\u201d with other results gained from studies on the International Space Station and on Earth.<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" class=\"alignleft size-medium wp-image-42690\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183815-350x288.jpg\" alt=\"2015-11-27-183815\" width=\"350\" height=\"288\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183815-350x288.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183815.jpg 393w\" sizes=\"(max-width: 350px) 100vw, 350px\">Specifically, BioSential will examine the effect of radiation in variable gravity environments \u2013 an aspect of radiation exposure that has not been systematically studied before.<\/p>\n<p>To accomplish this, BioSential will use a radiation biosensor of yeast (a eukaryotic microorganism) to \u201cgauge the genetic (DNA) damage and repair caused by space radiation\u201d to a strain of yeast that responds to Double Strand Break, states the AES presentation.<\/p>\n<p>Linear Energy Transfer and Total Ionizing Dose sensors on BioSential will monitor radiation exposure levels.<\/p>\n<p>In all, BioSential will be a 6U Cubesat with a 3U BioSensor and a 1U radiation spectrometer and dosimeter \u2013 with identical BioSential payloads for the Space Station and ground operations.<\/p>\n<p>The entire BioSential payload will require less than 10 W of average power over the lifetime of the mission.<\/p>\n<p>Lunar Flashlight:<\/p>\n<p>For Lunar Flashlight, the AES division selected this payload to address the SKG related to the pool of potential resources on the lunar surface \u2013 specifically, understanding the quantity and distribution of water and other volatiles in lunar cold traps.<\/p>\n<p>*Grab your 2016 NASASpaceFlight.com Calendar!*<\/p>\n<p>As has become a major focus for NASA and other space companies looking to mount human expeditions to celestial bodies in the inner solar system, the use of in-situ resources has become a significant point of discussion.<\/p>\n<p>In the case of the moon, the primary in-situ resource is water.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42691\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183854-350x237.jpg\" alt=\"2015-11-27-183854\" width=\"350\" height=\"237\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183854-350x237.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183854.jpg 442w\" sizes=\"(max-width: 350px) 100vw, 350px\">To this end, Lunar Flashlight will \u201cLocate ice deposits in the Moon\u2019s permanently shadowed craters\u201d and will \u201cidentify favorable locations for in-situ utilization.\u201d<\/p>\n<p>In this way, Lunar Flashlight will follow-up on recent revelations regarding the presence of water ice in the moon\u2019s permanently shadowed polar regions as well as anomalous reflectivity observations in lunar regions of \u201ccoldest year-round temperatures\u201d that could very well be water frost.<\/p>\n<p>Lunar Flashlight will conduct its mission through the use of four 50-75 watt pulsed Lasers that will \u201cilluminate 1 square kilometer of the lunar surface and define the four spectral bands of interest\u201d for the mission.<\/p>\n<p>Onboard the spacecraft, a two-channel near Infrared spectrometer will then observe the detected spectral bands from 1-2mm at a lunar altitude of 20 kilometers.<\/p>\n<p>Overall, this will require Lunar Flashlight to be a 6U Cubesat capable of producing a 290 m\/s delta V through a green propellant system.<\/p>\n<p>Near Earth Asteroid Scout:<\/p>\n<p>Thirdly, the AES division has selected a Near Earth Asteroid (NEA) scout mission to accompany SLS on her maiden voyage in order to investigate environmental elements surrounding an NEA.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42693\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-184313-350x239.jpg\" alt=\"2015-11-27-184313\" width=\"350\" height=\"239\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-184313-350x239.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-184313.jpg 429w\" sizes=\"(max-width: 350px) 100vw, 350px\">Specifically, the NEA scout mission is tasked with determining the size, rotational state, surface properties, and interaction environment of an NEA.<\/p>\n<p>This will be accomplished via a flyby or rendezvous with and characterization of an NEA that is \u201crepresentative of a potential human mission target,\u201d notes the AES presentation.<\/p>\n<p>Key parameters of this mission include cartography operations equal to or more than 80% of the target NEA\u2019s surface at resolutions of less than or equal to 50 cm\/px and equal to or greater than 30% surface mapping at less than or equal to 10 cm\/px.<\/p>\n<p>Specifically, the NEA scout will have an 85 square meter solar sail which will allow it to target an NEA within 1 AU (Astronomical Unit \u2013 average one-orbit distance between the Sun and the Earth) of Earth.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-medium wp-image-42692\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183920-350x249.jpg\" alt=\"2015-11-27-183920\" width=\"350\" height=\"249\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183920-350x249.jpg 350w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183920-492x350.jpg 492w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2015\/11\/2015-11-27-183920.jpg 567w\" sizes=\"(max-width: 350px) 100vw, 350px\">In fact, that 1 AU distance limitation is solely due to telecommunication limits and not the solar sail itself or the SLS rocket that it will hitch a ride with.<\/p>\n<p>Moreover, this Cubesat will help demonstrate emerging Solar Sail technology and will demonstrate the HEOMD\u2019s ability to perform low-cost reconnaissance missions with a 6U Cubesat.<\/p>\n<p>In this way, NASA\u2019s various divisions are working in tandem to&nbsp;deliver human missions to the Martian system in the 2030s and 2040s by utilizing small-class reconnaissance missions in conjunction with larger agency operations to leverage all of the assets available to the U.S. space agency.<\/p>\n<p>(Images: NASA and L2 \u2013 including SLS renders from L2 artist Nathan Koga \u2013 The full gallery of Nathan\u2019s (SpaceX Dragon to MCT, SLS, Commercial Crew and more) L2 images can be *found here*)<\/p>\n<p>(To join L2, click here:&nbsp;http:\/\/www.nasaspaceflight.com\/l2\/)<\/p>\n","protected":false},"excerpt":{"rendered":"<p>As NASA continues to progress toward the debut flight of SLS in 2018, the agency is now examining additional secondary payloads to fly on the EM-1 mission. These secondary payloads will involve Cubesats designed to investigate lunar and human biology aspects of spaceflight as well as Near Earth Asteroid reconnaissance. EM-1 secondary payloads: A major [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":30101,"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":[3718,624],"class_list":["post-39186","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-em-1","tag-sls"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39186"}],"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=39186"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/39186\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/30101"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=39186"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=39186"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=39186"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}