{"project":{"acronym":"","projectId":8539,"title":"Membrane Water Recuperator","primaryTaxonomyNodes":[{"taxonomyNodeId":10684,"taxonomyRootId":8816,"parentNodeId":10682,"level":3,"code":"TX06.1.2","title":"Water Recovery and Management","definition":"Water recovery and management provides a safe and reliable supply of potable water to meet crew consumption and operational needs, including supply and storage, recycling, and management through dormant mission periods.","exampleTechnologies":"Wastewater collection, wastewater processing, brine processing, potable water microbial control","hasChildren":false,"hasInteriorContent":true}],"startTrl":2,"currentTrl":3,"endTrl":3,"benefits":"After heating and cooling, humidity control is the next major element of indoor air quality control. Removing humidity is a major driver of the energy requirement for conditioning the air. Humidity can be removed in several ways including condensation on a cold surface or chemical absorption. Both of these methods require large amounts of energy. Another means of humidity removal is to exchange the water vapor from a wet stream to a dry stream using a membrane barrier. A highly selective membrane barrier will allow water to pass without losing the content of the main air stream. This membrane water recuperator could be easily developed to transfer water from fresh air makeup to exhaust air as a means to lessen the load on a condenser prior to cooling the air. By reducing the cooling load, it allows the use of more fresh air makeup, which in turn improves the quality of indoor air in modern air tight buildings. A successful Phase I development program would aid in the development of a working relationship with major corporations in the heating/air conditioning industry.
This proposed membrane water recuperator has immediate application in the current NASA vision for space exploration. As an add-on component to the CAMRAS, the recuperator provides water recovery capability for long duration missions (lunar habitat and Mars exploration) that require high degrees of loop closure. Other Air Revitalization components that exhaust a humid gas stream (such as Sabatier) could also benefit from water recovery using a membrane recuperator. Other NASA applications include integration of the membrane recuperator into other technology systems that vent humidified gaseous products, such as the Sabatier system. A 6 crew size Sabatier loses up to 80 kg/year by venting a humidified methane product. Also, the membrane recuperator can be integrated into systems designed for cryogenic storage of reactants (vis-à-vis ISRU methane/oxygen storage) to reduce/remove the moisture before the gas is liquefied.","description":"One of the CO2 reduction technologies currently being developed by NASA is the CO2 and Moisture Removal Amine Swing-bed System (CAMRAS). One of the disadvantages of the CAMRAS for long duration missions is that it removes moisture in addition to CO2. One way to minimize the water loss from the atmosphere, yet still be able to implement the highly desirable CO2 removal function of the CAMRAS, is to implement a membrane water exchanger, or recuperator, at the inlet of the CAMRAS system. The water exchanger passes humidified, CO2 laden air on one side of a membrane. The water vapor passes through the membrane leaving the CO2 laden air to be treated by the amine system. The air returning from the amine system is dry and CO2 free, as its remaining moisture and CO2 have been absorbed by the amine beads. This dry air passes on the second side of the membrane. Its low dew point provides the driving force for the moisture that passes through from the inlet stream. The CO2 free air becomes re-humidified, thus conserving water in the overall system mass balance. The membrane is highly selective for water, and not for CO2. The amount of carbon dioxide passing through the membrane and returning to the cabin is negligible; therefore the functionality of the CAMRAS as a CO2 removal system will not be impeded. The improvement over the current state-of-the-art is a reduction in power and the elimination of moving parts.","startYear":2010,"startMonth":1,"endYear":2010,"endMonth":7,"statusDescription":"Completed","principalInvestigators":[{"contactId":259781,"canUserEdit":false,"firstName":"Karen","lastName":"Murdoch","fullName":"Karen E Murdoch","fullNameInverted":"Murdoch, Karen E","middleInitial":"E","primaryEmail":"karen@wolf-engineering.com","publicEmail":true,"nacontact":false}],"programDirectors":[{"contactId":206378,"canUserEdit":false,"firstName":"Jason","lastName":"Kessler","fullName":"Jason L Kessler","fullNameInverted":"Kessler, Jason L","middleInitial":"L","primaryEmail":"jason.l.kessler@nasa.gov","publicEmail":true,"nacontact":false}],"programExecutives":[{"contactId":215154,"canUserEdit":false,"firstName":"Jennifer","lastName":"Gustetic","fullName":"Jennifer L Gustetic","fullNameInverted":"Gustetic, Jennifer L","middleInitial":"L","primaryEmail":"jennifer.l.gustetic@nasa.gov","publicEmail":true,"nacontact":false}],"programManagers":[{"contactId":62051,"canUserEdit":false,"firstName":"Carlos","lastName":"Torrez","fullName":"Carlos Torrez","fullNameInverted":"Torrez, Carlos","primaryEmail":"carlos.torrez@nasa.gov","publicEmail":true,"nacontact":false}],"projectManagers":[{"contactId":453303,"canUserEdit":false,"firstName":"Suzanne","lastName":"Curley","fullName":"Suzanne Curley","fullNameInverted":"Curley, Suzanne","primaryEmail":"su.curley-1@nasa.gov","publicEmail":true,"nacontact":false},{"contactId":461333,"canUserEdit":false,"firstName":"Theresa","lastName":"Stanley","fullName":"Theresa M Stanley","fullNameInverted":"Stanley, Theresa M","middleInitial":"M","primaryEmail":"theresa.m.stanley@nasa.gov","publicEmail":true,"nacontact":false}],"website":"","libraryItems":[],"transitions":[{"transitionId":66561,"projectId":8539,"transitionDate":"2010-07-01","path":"Closed Out","closeoutDocuments":[{"title":"Final Summary Chart","file":{"fileExtension":"pdf","fileId":306409,"fileName":"SBIR_2009_1_FSC_X2.01-8301","fileSize":32798,"objectId":66561,"objectType":{"lkuCodeId":1841,"code":"TRANSITION_FILES","description":"Transition Files","lkuCodeTypeId":182,"lkuCodeType":{"codeType":"OBJECT_TYPE","description":"Object Type"}},"fileSizeString":"32.0 KB"},"transitionId":66561,"fileId":306409}],"infoText":"Closed out","infoTextExtra":"","dateText":"July 2010"}],"responsibleMd":{"acronym":"STMD","canUserEdit":false,"city":"","external":false,"linkCount":0,"organizationId":4875,"organizationName":"Space Technology Mission Directorate","organizationType":"NASA_Mission_Directorate","naorganization":false,"organizationTypePretty":"NASA Mission Directorate"},"program":{"acronym":"SBIR/STTR","active":true,"description":"
The NASA SBIR and STTR programs fund the research, development, and demonstration of innovative technologies that fulfill NASA needs as described in the annual Solicitations and have significant potential for successful commercialization. If you are a small business concern (SBC) with 500 or fewer employees or a non-profit RI such as a university or a research laboratory with ties to an SBC, then NASA encourages you to learn more about the SBIR and STTR programs as a potential source of seed funding for the development of your innovations.
The SBIR and STTR programs have 3 phases:
The SBIR and STTR Phase I contracts last for 6 months with a maximum funding of $125,000, and Phase II contracts last for 24 months with a maximum funding of $750,000 - $1.5 million.
Opportunity for Continued Technology Development Post-Phase II:
The NASA SBIR/STTR Program currently has in place two initiatives for supporting its small business partners past the basic Phase I and Phase II elements of the program that emphasize opportunities for commercialization. Specifically, the NASA SBIR/STTR Program has the Phase II Enhancement (Phase II-E) and Phase II eXpanded (Phase II-X) contract options.
Please review the links below to obtain more information on the SBIR/STTR programs.
Provides an overview of the SBIR and STTR programs as implemented by NASA
Provides access to the annual SBIR/STTR Solicitations containing detailed information on the program eligibility requirements, proposal instructions and research topics and subtopics
Schedule and links for the SBIR/STTR solicitations and selection announcements
Federal and non-Federal sources of assistance for small business
Search our complete archive of awarded project abstracts to learn about what NASA has funded
Still have questions? Visit the program FAQs
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