{"projectId":89494,"project":{"projectId":89494,"title":"Ultrasonic Additive Manufacturing for Capillary Heat Transfer Devices and Integrated Heat Exchangers","startDate":"2016-04-18","startYear":2016,"startMonth":4,"endDate":"2019-12-31","endYear":2019,"endMonth":12,"programId":73,"program":{"ableToSelect":false,"acronym":"SBIR/STTR","isActive":true,"description":"<p>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. 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The embedded heat exchanger is part of a multifunctional three dimensional structure that will simultaneously accommodate thermal and mechanical loads, and offer radiation protection via multi-material laminates. Non-NASA commercial application of this technology has started with aerospace and defense companies who are already customers. These firms are early adopters of additive manufacturing because it enables lightweight designs and the production of parts with complex geometries. Additionally, aerospace and defense manufacturers frequently incorporate high value materials, and additive manufacturing allows them to maintain fine control of material properties and reduce raw material waste. There are very few additive approaches for fabricating metallic load-bearing structure with embedded multi-functional capability. Traditional fusion based welding and/or thermomechanical processes used for fabricating metallic structure would destroy delicate instruments. 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Advance new processes and model-based manufacturing capabilities for more affordable and higher performance products (mass reduction/affordability challenge). Cube Sat components will have very small masses, and their temperatures are highly sensitive to variations in the component power output and spacecraft environmental temperature. The advanced thermal devices developed here will be capable of maintaining components within their specified temperature ranges, with excellent reliability of single piece structures, while concurrently minimizing added weight. The technology being developed in this effort directly addresses the two overarching themes of NASA's technology plan, critical attributes and technology themes required by every mission architecture: multifunctional and lightweight.<br /> <br />This program produces high performance heat exchangers embedded in structures with integrated temperature monitoring sensors. The embedded heat exchanger is part of a multifunctional three dimensional structure that will simultaneously accommodate thermal and mechanical loads, and offer radiation protection via multi-material laminates. Non-NASA commercial application of this technology has started with aerospace and defense companies who are already customers. These firms are early adopters of additive manufacturing because it enables lightweight designs and the production of parts with complex geometries. Additionally, aerospace and defense manufacturers frequently incorporate high value materials, and additive manufacturing allows them to maintain fine control of material properties and reduce raw material waste. There are very few additive approaches for fabricating metallic load-bearing structure with embedded multi-functional capability. Traditional fusion based welding and/or thermomechanical processes used for fabricating metallic structure would destroy delicate instruments. 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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.</p><p><strong>The SBIR and STTR programs have 3 phases</strong>:</p><ul><li><strong>Phase I</strong> is the opportunity to establish the scientific, technical, and commercial feasibility of the proposed innovation in fulfillment of NASA needs.</li><li><strong>Phase II</strong> is focused on the development, demonstration and delivery of the proposed innovation.</li></ul><p>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.</p><ul><li><strong>Phase III</strong> is the commercialization of innovative technologies, products, and services resulting from either a Phase I or Phase II contract. 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Specifically, the NASA SBIR/STTR Program has the Phase II Enhancement (Phase II-E) and Phase II eXpanded (Phase II-X) contract options.&nbsp;</p><p><strong>Please review the links below to obtain more information on the SBIR/STTR programs.</strong></p><ul><li><strong><a target=\"_blank\" href=\"http://sbir.gsfc.nasa.gov/sites/default/files/ParticipationGuide.pdf\">Participation Guide</a></strong></li></ul><p>Provides an overview of the SBIR and STTR programs as implemented by NASA</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/solicitations\">Program Solicitations</a></strong></li></ul><p>Provides access to the annual SBIR/STTR Solicitations containing detailed information on the program eligibility requirements, proposal instructions and research topics and subtopics</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/prg_sched_anncmnt\">Schedule and Awards</a></strong></li></ul><p>Schedule and links for the SBIR/STTR solicitations and selection announcements</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/content/additional-sources-assistance\">Sources of Assistance</a></strong></li></ul><p>Federal and non-Federal sources of assistance for small business</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/abstract_archives\">Awarded Abstracts</a></strong></li></ul><p>Search our complete archive of awarded project abstracts to learn about what NASA has funded</p><ul><li><strong><a href=\"http://sbir.gsfc.nasa.gov/content/frequently-asked-questions\">Frequently Asked Questions</a></strong></li></ul><p>&nbsp;Still have questions? 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This includes pumped integrated heat exchangers for fluid loops, integrated heat pipes, and integrated wick systems. By combining two functions (structure/thermal) it will be shown that a lighter weight, higher performance solution can be built in a shorter time period. The project team will demonstrate technical feasibility in Phase I. In Phase II the team will use UAM to 3D print an aluminum structure capable of carrying structural loads with integrated thermal management passages as may be used in a pumped integrated heat exchanger. This demonstration unit will be delivered to NASA for testing at the completion of the Phase II contract.","benefits":"UAM-enabled thermal management + structural devices are an important enabler for not-too-distant deep space missions, where UAM-enabled devices permit more system integration and autonomy while reducing mass and volume. For application in deep space missions this paradigm shift is similar to the change from a few day Lunar mission (Apollo) to a multiple year low earth orbit habitat (Space Station). Typical initial UAM applications would include integrating structure and thermal control of parts of the Mars Science Laboratory Curiosity Rover, followed by components of advanced small spacecraft that have very small masses with their temperatures highly sensitive to variations in the component power output and spacecraft environmental temperature. In both applications, UAM addresses competing system requirements for managing primary load paths and integrating thermal management into the structure.<br /> <br />The initial application of high performance UAM-enabled thermal management devices will likely be in NASA, defense and commercial space structure programs, in that order. This estimate recognizes the high performance technology leading nature of the organizations and their missions. 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