{"id":40166,"date":"2012-03-31T01:11:46","date_gmt":"2012-03-30T17:11:46","guid":{"rendered":"https:\/\/wp-productionenv-bjg9h2g2bgg5b8aa.southeastasia-01.azurewebsites.net\/news\/deep-space-habitat-module-concepts-outlined-for-beo-exploration\/"},"modified":"2012-03-31T01:11:46","modified_gmt":"2012-03-30T17:11:46","slug":"deep-space-habitat-module-concepts-outlined-for-beo-exploration","status":"publish","type":"post","link":"https:\/\/starpath.global\/news\/deep-space-habitat-module-concepts-outlined-for-beo-exploration\/","title":{"rendered":"Deep Space Habitat module concepts outlined for BEO exploration"},"content":{"rendered":"<p>With the push for exploration Beyond Earth Orbit (BEO) increasing, a proposed habitat for human exploration outside the confines of Earth\u2019s immediate space is taking shape as NASA presses forward with the development of its new Deep Space Habitat (DSH) \u2013 a module-based habitation facility that will be used as part of manned exploration missions to the moon, asteroids, and eventually Mars.<\/p>\n<p>Deep Space Habitat \u2013&nbsp;Building on the modular success of the ISS:<\/p>\n<p>As presented by the AES Habitation Project, the Future In-Space Operations presentation outlines NASA\u2019s progress-to-date, as well as future uses for, the Deep Space Habitat (DSH).<\/p>\n<p><img fetchpriority=\"high\" decoding=\"async\" class=\"alignleft size-full wp-image-23785\" title=\"Z3\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z322.jpg\" alt=\"\" width=\"349\" height=\"270\">\u201cDevelop DSH concepts based on International Space Station Systems,\u201d states the presentation \u2013 available for download on L2 (L2 Link).<\/p>\n<p>With an initial size capable of accommodating four (4) crewmembers for a 60-day mission, the DSH will be comprised of a newly-constructed or refurbished HAB module along with a docked Orion space capsule.<\/p>\n<p>Building from this 60-day configuration, the DSH will carry the capability of expanding to a 500-day configuration, which would see the incorporation of an MPLM (Multi-Purpose Logistics Module) to the HAB\/Orion duo.<\/p>\n<p>With initial studies completed in the fall of 2011, the HAB\/MPLM structure emerged as the current project baseline, allowing for the subsequent and ongoing development of a \u201cDeep Space Command Post concept for Earth-Moon L1 or L2 locations.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-23787\" title=\"Z4\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z422.jpg\" alt=\"\" width=\"349\" height=\"230\">The benefits of using already exiting modules \u2013 such as the MPLMs \u2013 provides for already on-orbit service verification through the modules\u2019 usage in the construction, utilization, and continuation of the International Space Station.<\/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>Technology News<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>As noted by the presentation, the potential benefits of using ISS MPLM- and HAB-sized (ISS Lab-sized) modules is that \u201cISS hardware is flight qualified; the mass may be higher but utilization could reduce overall project cost, schedule, and risk; Incorporates ISS utilization into the program; and it offers an approach to incorporating International participation.\u201d<\/p>\n<p>Ground rules and assumptions:<\/p>\n<p>As with all elements of space travel, the DSH comes with certain ground rules and assumptions for its construction, outfitting, and utilization.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-23788\" title=\"Z5\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z519.jpg\" alt=\"\" width=\"351\" height=\"263\">Specifically, the Future In-Space Operations presentation notes that the DSH\u2019s design is \u201cintended to meet HAT (Human spaceflight Architecture Team) missions with modifications as required to utilize current ISS and MPCV (Multi-Purpose Crew Vehicle, also known at Orion) systems and technologies.\u201d<\/p>\n<p>For 60-day missions, the DSH could be utilized by a crew of four astronauts for Earth-Moon Lagrangian Point 1 (EM L1) missions, EM L2 missions, GEO satellite servicing missions, ES (Earth-Sun) L2 missions, Lunar orbit missions, and microgravity free-flyer missions.<\/p>\n<p>Likewise, and more importantly, the 500-day missions of the DSH would see a crew of four astronauts use the complex for Near Earth Asteroid missions and Mars transit and orbital missions.<\/p>\n<h4 class=\"widget-title penci-border-arrow\">See Also<\/h4>\n<ul>\n<li>Orion Forum Section<\/li>\n<li>L2 Orion Section (Extensive)<\/li>\n<li>Click here to Join L2<\/li>\n<\/ul>\n<p>The DSH itself will be \u201csized for Existing Launch Vehicle Systems. DSH can be broken down into smaller modular elements for EELV (Enhanced Expendable Launch Vehicle) launch and\/or outfitted at ISS,\u201d notes the presentation.<\/p>\n<p>The presentation does specifically note, however, that DSH is not included for launch at this time on NASA\u2019s upcoming successor to the Space Shuttle, the massive SLS (Space Launch System) rocket.<\/p>\n<p>\u201cSLS utilization not included but should be possible.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-23796\" title=\"Z6\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z610.jpg\" alt=\"\" width=\"351\" height=\"249\">The DSH can be assembled and serviced at the International Space Station, and the habitat\u2019s propulsion and control will be provided by a docked MPCV\/Orion capsule, CPS (Cryogenic Propulsion Stage), and\/or SEP (Space Electric Propulsion).<\/p>\n<p>Basic vehicle elements of the DSH will include the MPCV\/Orion, a utility tunnel\/Airlock with attached FlexCraft or MMSEV (Multi-Mission Science Exploration Vehicle), a HAB module, a CPS sized for the specific mission at hand, and an MPLM for 500-day missions.<\/p>\n<p>Currently, the DHS teams are working four issues, which include the launch of existing modules on EELVs, Galactic Cosmic Radiation protection concepts, microgravity concerns, and mission integration.<\/p>\n<p>DSH structures and protecting a crew in deep space:<\/p>\n<p>The structures for the DSH will be ISS derived \u2013 utilizing known technologies to spur humankind\u2019s exploration beyond Earth orbit.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-23798\" title=\"Z7\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z712.jpg\" alt=\"\" width=\"352\" height=\"261\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z712.jpg 352w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z712-350x260.jpg 350w\" sizes=\"(max-width: 352px) 100vw, 352px\">This ISS derived decision is seen with DSH in the form of its STA (Static Test Assembly) configuration with a mock-up Lab\/HAB module.<\/p>\n<p>This STA has provided engineers with understood and known mass and fabrication materials\/processes.<\/p>\n<p>The same MPLM design used for Leonardo and Raffaello during the Shuttle era served as the base for the design of the MPLM to be used as part of the DSH. One notable exception to the traditional MPLM design is the addition of one more Common Berthing Mechanism (CBM), bringing the total number of CBMs for the DSH MPLM to three.<\/p>\n<p>As noted by the presentation, \u201cAll ports will be CBM-sized and use ISS mass for these components. A NASA Docking System (NDS) adapter will be used for MPCV interface.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-23800\" title=\"Z9\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z93.jpg\" alt=\"\" width=\"350\" height=\"260\">Moreover, the connection between the MPLM and the HAB module for 500-day missions will be a special utility tunnel.<\/p>\n<p>\u201cThe tunnel\/contingency airlock structure mass is based on ISS airlock areal mass, is assumed to be fabricated in a similar manner. External secondary structure for radiators, meteor debris shielding and power systems are estimated at 20% of the mass to be supported.\u201d<\/p>\n<p>Should the decision be made to launch the DSH components on EELV rockets, a new launch adapter will need to be developed to connect the ISS elements.<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-23801\" title=\"Z10\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z102.jpg\" alt=\"\" width=\"352\" height=\"244\" srcset=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z102.jpg 352w, https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z102-350x243.jpg 350w\" sizes=\"(max-width: 352px) 100vw, 352px\">Furthermore, just like the ISS, the DSH will need to have an ECLSS (Environmental Control and Life Support Systems).<\/p>\n<p>According to the Future In-Space Operations presentation, \u201cMass of ISS subsystems, expendables, usage and failure rates are used in determining the mass allotments of ECLSS components and spares.\u201d<\/p>\n<p>A total of two water ISPR racks will be included in \u201cISS-packaged configuration\u201d with the remaining ECLSS subsystems repackaged for the DSH.&nbsp; This is based on the assumption that a more light-weight arrangement for the secondary structure can be developed.<\/p>\n<p>The ECLSS will provide 21 days of \u201copen-loop contingency margin on consumables (food, water, O2) for the 60-day mission and 60 days contingency for the 500-day mission.\u201d<\/p>\n<p><img loading=\"lazy\" decoding=\"async\" class=\"alignleft size-full wp-image-23802\" title=\"Z11\" src=\"https:\/\/www.nasaspaceflight.com\/wp-content\/uploads\/2012\/03\/Z111.jpg\" alt=\"\" width=\"351\" height=\"285\">This is all based on a well-characterized water balance on the ISS in both the open loop and closed loop configurations.<\/p>\n<p>Moreover, thermal control within the DSH will be controlled\/maintained through active waste heat collection via redundant internal and external pumped loops with cold plates and heat exchangers.<\/p>\n<p>Active waste heat rejection will be accomplished through radiators \u2013 which will be \u201cdeployed, non-articulating in flight.\u201d<\/p>\n<p>On the other hand, passive thermal control will be maintained through Multi-Layer Insulation blankets on the MPLM, HAB, and tunnel pressure shells.<\/p>\n<p>For crew safety and protection, external Micrometeoroid Debris Protection Shields (MDPS) will be installed on the MPLM, HAB, and tunnel adapter. These MDPSs will be derived from the shielding used on the Shuttle MPLMs.<\/p>\n<p>Moreover, an interior radiation water wall will be incorporated in the DHS HAB design to protect crews from Solar Particle Events.<\/p>\n<p>The water wall, in both the 60-day and 500-day configurations, will consist of a 0.55 cm thick polyethylene tank and a 9.9 cm thick water wall for a total protection rating of 11g\/cm squared.<\/p>\n<p>(Images: Via L2 DSH Presentation). L2\u2019s new Orion and Future Spacecraft specific L2 section includes, presentations, videos, graphics and internal updates&nbsp;on Orion and other future spacecraft.<\/p>\n<p>(L2 is \u2013 as it has been for the past several years \u2013 providing full exclusive future vehicle coverage, available no where else on the internet. To join L2, click here: http:\/\/www.nasaspaceflight.com\/l2\/)<\/p>\n","protected":false},"excerpt":{"rendered":"<p>With the push for exploration Beyond Earth Orbit (BEO) increasing, a proposed habitat for human exploration outside the confines of Earth\u2019s immediate space is taking shape as NASA presses forward with the development of its new Deep Space Habitat (DSH) \u2013 a module-based habitation facility that will be used as part of manned exploration missions [&hellip;]<\/p>\n","protected":false},"author":1,"featured_media":30422,"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":[9015,9034,7873,640,624],"class_list":["post-40166","post","type-post","status-publish","format-standard","has-post-thumbnail","hentry","category-news","tag-dsh","tag-hlv","tag-neo","tag-orion","tag-sls"],"acf":[],"_links":{"self":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/40166"}],"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=40166"}],"version-history":[{"count":0,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/posts\/40166\/revisions"}],"wp:featuredmedia":[{"embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media\/30422"}],"wp:attachment":[{"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/media?parent=40166"}],"wp:term":[{"taxonomy":"category","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/categories?post=40166"},{"taxonomy":"post_tag","embeddable":true,"href":"https:\/\/starpath.global\/blog\/wp-json\/wp\/v2\/tags?post=40166"}],"curies":[{"name":"wp","href":"https:\/\/api.w.org\/{rel}","templated":true}]}}