{"projectId":89700,"project":{"projectId":89700,"title":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities","startDate":"2016-06-10","startYear":2016,"startMonth":6,"endDate":"2016-12-09","endYear":2016,"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. 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. Phase III contracts are funded from sources other than the SBIR and STTR programs and may be awarded without further competition.</li></ul><p><strong>Opportunity for Continued Technology Development Post-Phase II</strong>:</p><p>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.&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? Visit the program FAQs</p>","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":73,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer","manageGaps":false,"acronymOrTitle":"SBIR/STTR"},"description":"Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specified requirements over the operational envelope before the first flight. The development of advanced ground test technology components and systems that are capable of enhancing environment simulation, minimizing program test time, cost and risk and meeting environmental and safety regulations is focused on near-term products that augment existing state-of-the-art propulsion system test facilities. Thus improved capabilities to model and predict component behavior in harsh ground test environments are needed for enhanced facility design. In particular, components such as valves, check valves and chokes that are subjected to high pressure, high flow rate cryogenic environments will experience potentially damaging two phase flow effects such as cavitation. Robust cryogenic cavitation models for real fluids equations of state in the presence of mixed supersonic/subsonic flows are demonstrated to deal with poor solution convergence and numerical instabilities. The proposed innovation leverages modifications to the local preconditioning formulation of the Roe flux with a barotropic equation of state and uses a representative component flow problem to demonstrate the effectiveness of enhanced modifications to the cryogenic liquid tabular equation of state. Instabilities arising from the single temperature assumption in the two phase mixture equation of state, which must often be evaluated by extrapolating data too far from the saturation curve, are eliminated with a nonlinear temperature limiter that precludes non-physical behavior, such as imaginary mixture sound speeds. The result is an efficient, robust cryogenic cavitation model suitable for application to propulsion systems ground test facility component design and analysis efforts.","benefits":"This technology will provide NASA with an efficient, robust cryogenic cavitation modeling and prediction tool suitable for application to propulsion systems ground test facility component design and analysis. The research product will provide enabling engineering and scientific technologies to predict complex cryogenic flow problems, reduce ground test facility costs and overall system risk while increasing test productivity. Potential enhancements include improved treatment of evaporation and condensation rates, turbulence/cavitation interaction modeling, liquid/vapor thermal interface effects, variable transport properties, expanded thermodynamic databases and extended model validation. The proposed cavitation modeling tool is also applicable to hydrogen inducers, impellers and pumps operating at high vapor fraction.<br /> <br />The growing trend toward coupled multi-physics analyses is opening significant new markets as more difficult problems can be addressed using advanced computational techniques. The ability to robustly model complex cryogenic flows with cavitation will allow the commercial aerospace and defense industries to improve design and development of new products and streamline ground testing. Our analysis software can also be applied to marine propellers, boiler feed pumps and refrigerant systems. The basic architecture of the modeling framework can remain the same while new plug-in modules are developed to address different physics and design requirements.","releaseStatus":"Released","status":"Completed","viewCount":623,"destinationType":["Foundational_Knowledge"],"trlBegin":3,"trlCurrent":4,"trlEnd":4,"lastUpdated":"01/22/26","favorited":false,"detailedFunding":false,"projectContacts":[{"contactId":3164534,"canUserEdit":false,"firstName":"Daniel","lastName":"Allgood","fullName":"Daniel Allgood","fullNameInverted":"Allgood, Daniel","email":"Daniel.C.Allgood@nasa.gov","receiveEmail":"Subscribed_Contact","projectContactRole":"Project_Manager","projectContactId":545331,"projectId":89700,"programContactRolePretty":"","projectContactRolePretty":"Project Manager"},{"contactId":3251129,"canUserEdit":false,"firstName":"Rex","lastName":"Chamberlain","fullName":"Rex Chamberlain","fullNameInverted":"Chamberlain, Rex","email":"rex@tetraresearch.com","receiveEmail":"Subscribed_Contact","projectContactRole":"Principal_Investigator","projectContactId":545332,"projectId":89700,"programContactRolePretty":"","projectContactRolePretty":"Principal Investigator"},{"contactId":398219,"canUserEdit":false,"firstName":"Robert","lastName":"Chamberlain","fullName":"Robert R Chamberlain","fullNameInverted":"Chamberlain, Robert R","middleInitial":"R","email":"rex@tetraresearch.com","receiveEmail":"Subscribed_User","projectContactRole":"Principal_Investigator","projectContactId":545333,"projectId":89700,"programContactRolePretty":"","projectContactRolePretty":"Principal Investigator"}],"programContacts":[],"leadOrganization":{"organizationId":4287,"organizationName":"Tetra Research Corporation","organizationType":"Industry","city":"Princeton","stateTerritoryId":39,"stateTerritory":{"abbreviation":"IL","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Illinois","stateTerritoryId":39,"isTerritory":false},"country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"zipCode":"61356-1934","cageCode":"088X4","projectId":89700,"projectOrganizationId":573207,"organizationRole":"Lead_Organization","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"Lead Organization","organizationTypePretty":"Industry"},"otherOrganizations":[{"organizationId":4287,"organizationName":"Tetra Research Corporation","organizationType":"Industry","city":"Princeton","stateTerritoryId":39,"stateTerritory":{"abbreviation":"IL","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Illinois","stateTerritoryId":39,"isTerritory":false},"country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"zipCode":"61356-1934","cageCode":"088X4","projectId":89700,"projectOrganizationId":573207,"organizationRole":"Lead_Organization","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"Lead Organization","organizationTypePretty":"Industry"},{"organizationId":4859,"organizationName":"Stennis Space Center","acronym":"SSC","organizationType":"NASA_Center","city":"Stennis Space Center","stateTerritoryId":41,"stateTerritory":{"abbreviation":"MS","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Mississippi","stateTerritoryId":41,"isTerritory":false},"country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"zipCode":"39529-6000","projectId":89700,"projectOrganizationId":573206,"organizationRole":"Supporting_Organization","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"Supporting Organization","organizationTypePretty":"NASA Center"}],"primaryTx":{"taxonomyNodeId":11308,"taxonomyRootId":8817,"parentNodeId":11304,"code":"TX11.2.4","title":"Science Modeling","description":"Science modeling uses mathematical or heuristical models to quantify the physical processes as a function of underlying variables.","exampleTechnologies":"Fortran compatible and interoperable parallel libraries, high performance processor toolset for science modeling, quality metrics for science data, toolset for concurrent data diagnostics and acquisition for science modeling, software infrastructure for sensor webs, planetary contaminant modeling","level":3,"hasChildren":false,"selected":false,"isPrimary":true,"hasInteriorContent":true},"primaryTxTree":[[{"taxonomyNodeId":11293,"taxonomyRootId":8817,"code":"TX11","title":"Software, Modeling, Simulation, and Information Processing","level":1,"hasChildren":true,"selected":false,"hasInteriorContent":true},{"taxonomyNodeId":11304,"taxonomyRootId":8817,"parentNodeId":11293,"code":"TX11.2","title":"Modeling","description":"Modeling technologies support autonomous, integrated, and interoperable modeling capabilities throughout NASA's mission portfolios.","level":2,"hasChildren":true,"selected":false,"hasInteriorContent":true},{"taxonomyNodeId":11308,"taxonomyRootId":8817,"parentNodeId":11304,"code":"TX11.2.4","title":"Science Modeling","description":"Science modeling uses mathematical or heuristical models to quantify the physical processes as a function of underlying variables.","exampleTechnologies":"Fortran compatible and interoperable parallel libraries, high performance processor toolset for science modeling, quality metrics for science data, toolset for concurrent data diagnostics and acquisition for science modeling, software infrastructure for sensor webs, planetary contaminant modeling","level":3,"hasChildren":false,"selected":true,"hasInteriorContent":true}]],"technologyOutcomes":[{"technologyOutcomeId":95678,"projectId":89700,"project":{"projectId":89700,"title":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities","startDate":"2016-06-10","startYear":2016,"startMonth":6,"endDate":"2016-12-09","endYear":2016,"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. 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. Phase III contracts are funded from sources other than the SBIR and STTR programs and may be awarded without further competition.</li></ul><p><strong>Opportunity for Continued Technology Development Post-Phase II</strong>:</p><p>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.&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? Visit the program FAQs</p>","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":73,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer","manageGaps":false,"acronymOrTitle":"SBIR/STTR"},"description":"Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specified requirements over the operational envelope before the first flight. The development of advanced ground test technology components and systems that are capable of enhancing environment simulation, minimizing program test time, cost and risk and meeting environmental and safety regulations is focused on near-term products that augment existing state-of-the-art propulsion system test facilities. Thus improved capabilities to model and predict component behavior in harsh ground test environments are needed for enhanced facility design. In particular, components such as valves, check valves and chokes that are subjected to high pressure, high flow rate cryogenic environments will experience potentially damaging two phase flow effects such as cavitation. Robust cryogenic cavitation models for real fluids equations of state in the presence of mixed supersonic/subsonic flows are demonstrated to deal with poor solution convergence and numerical instabilities. The proposed innovation leverages modifications to the local preconditioning formulation of the Roe flux with a barotropic equation of state and uses a representative component flow problem to demonstrate the effectiveness of enhanced modifications to the cryogenic liquid tabular equation of state. Instabilities arising from the single temperature assumption in the two phase mixture equation of state, which must often be evaluated by extrapolating data too far from the saturation curve, are eliminated with a nonlinear temperature limiter that precludes non-physical behavior, such as imaginary mixture sound speeds. The result is an efficient, robust cryogenic cavitation model suitable for application to propulsion systems ground test facility component design and analysis efforts.","benefits":"This technology will provide NASA with an efficient, robust cryogenic cavitation modeling and prediction tool suitable for application to propulsion systems ground test facility component design and analysis. The research product will provide enabling engineering and scientific technologies to predict complex cryogenic flow problems, reduce ground test facility costs and overall system risk while increasing test productivity. Potential enhancements include improved treatment of evaporation and condensation rates, turbulence/cavitation interaction modeling, liquid/vapor thermal interface effects, variable transport properties, expanded thermodynamic databases and extended model validation. The proposed cavitation modeling tool is also applicable to hydrogen inducers, impellers and pumps operating at high vapor fraction.<br /> <br />The growing trend toward coupled multi-physics analyses is opening significant new markets as more difficult problems can be addressed using advanced computational techniques. The ability to robustly model complex cryogenic flows with cavitation will allow the commercial aerospace and defense industries to improve design and development of new products and streamline ground testing. Our analysis software can also be applied to marine propellers, boiler feed pumps and refrigerant systems. The basic architecture of the modeling framework can remain the same while new plug-in modules are developed to address different physics and design requirements.","releaseStatus":"Released","status":"Completed","destinationType":["Foundational_Knowledge"],"trlBegin":3,"trlCurrent":4,"trlEnd":4,"favorited":false,"detailedFunding":false,"programContacts":[],"endDateString":"Dec 2016","startDateString":"Jun 2016"},"technologyOutcomeDate":"2016-12-09","technologyOutcomePath":"Closed_Out","files":[{"title":"Final Summary Chart","file":{"fileExtension":"pdf","fileId":362708,"fileName":"SBIR_16_1_H10_02-7667","fileSize":116654,"objectId":95678,"objectType":"technologyOutcomeFiles","presignedUpload":false,"fileSizeString":"113.9 KB"},"technologyOutcomeId":95678,"fileId":362708}],"infoText":"Closed out","infoTextExtra":"Project closed out","isIndirect":false,"infusionPretty":"","isBiDirectional":false,"technologyOutcomeDateString":"Dec 2016","technologyOutcomeDateFullString":"December 2016","technologyOutcomePartnerPretty":"","technologyOutcomePathPretty":"Closed Out","technologyOutcomeRationalePretty":""},{"technologyOutcomeId":95679,"projectId":89700,"project":{"projectId":89700,"title":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities","startDate":"2016-06-10","startYear":2016,"startMonth":6,"endDate":"2016-12-09","endYear":2016,"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. 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. Phase III contracts are funded from sources other than the SBIR and STTR programs and may be awarded without further competition.</li></ul><p><strong>Opportunity for Continued Technology Development Post-Phase II</strong>:</p><p>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.&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? Visit the program FAQs</p>","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":73,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer","manageGaps":false,"acronymOrTitle":"SBIR/STTR"},"description":"Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specified requirements over the operational envelope before the first flight. The development of advanced ground test technology components and systems that are capable of enhancing environment simulation, minimizing program test time, cost and risk and meeting environmental and safety regulations is focused on near-term products that augment existing state-of-the-art propulsion system test facilities. Thus improved capabilities to model and predict component behavior in harsh ground test environments are needed for enhanced facility design. In particular, components such as valves, check valves and chokes that are subjected to high pressure, high flow rate cryogenic environments will experience potentially damaging two phase flow effects such as cavitation. Robust cryogenic cavitation models for real fluids equations of state in the presence of mixed supersonic/subsonic flows are demonstrated to deal with poor solution convergence and numerical instabilities. The proposed innovation leverages modifications to the local preconditioning formulation of the Roe flux with a barotropic equation of state and uses a representative component flow problem to demonstrate the effectiveness of enhanced modifications to the cryogenic liquid tabular equation of state. Instabilities arising from the single temperature assumption in the two phase mixture equation of state, which must often be evaluated by extrapolating data too far from the saturation curve, are eliminated with a nonlinear temperature limiter that precludes non-physical behavior, such as imaginary mixture sound speeds. The result is an efficient, robust cryogenic cavitation model suitable for application to propulsion systems ground test facility component design and analysis efforts.","benefits":"This technology will provide NASA with an efficient, robust cryogenic cavitation modeling and prediction tool suitable for application to propulsion systems ground test facility component design and analysis. The research product will provide enabling engineering and scientific technologies to predict complex cryogenic flow problems, reduce ground test facility costs and overall system risk while increasing test productivity. Potential enhancements include improved treatment of evaporation and condensation rates, turbulence/cavitation interaction modeling, liquid/vapor thermal interface effects, variable transport properties, expanded thermodynamic databases and extended model validation. The proposed cavitation modeling tool is also applicable to hydrogen inducers, impellers and pumps operating at high vapor fraction.<br /> <br />The growing trend toward coupled multi-physics analyses is opening significant new markets as more difficult problems can be addressed using advanced computational techniques. The ability to robustly model complex cryogenic flows with cavitation will allow the commercial aerospace and defense industries to improve design and development of new products and streamline ground testing. Our analysis software can also be applied to marine propellers, boiler feed pumps and refrigerant systems. The basic architecture of the modeling framework can remain the same while new plug-in modules are developed to address different physics and design requirements.","releaseStatus":"Released","status":"Completed","destinationType":["Foundational_Knowledge"],"trlBegin":3,"trlCurrent":4,"trlEnd":4,"favorited":false,"detailedFunding":false,"programContacts":[],"endDateString":"Dec 2016","startDateString":"Jun 2016"},"relatedProjectId":93738,"relatedProject":{"projectId":93738,"title":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities","startDate":"2017-04-19","startYear":2017,"startMonth":4,"endDate":"2019-04-18","endYear":2019,"endMonth":4,"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. 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. Phase III contracts are funded from sources other than the SBIR and STTR programs and may be awarded without further competition.</li></ul><p><strong>Opportunity for Continued Technology Development Post-Phase II</strong>:</p><p>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.&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? Visit the program FAQs</p>","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":73,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer","manageGaps":false,"acronymOrTitle":"SBIR/STTR"},"description":"Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specified requirements over the operational envelope before the first flight. The development of advanced ground test technology components and systems that are capable of enhancing environment simulation, minimizing program test time, cost and risk and meeting environmental and safety regulations is focused on near-term products that augment existing state-of-the-art propulsion system test facilities. Thus improved capabilities to model and predict component behavior in harsh ground test environments are needed for enhanced facility design. In particular, components such as pumps, turbines, valves and chokes may experience vibration and damage due to cavitation in the flowing liquid, and any reduction in the severity of the operating conditions would provide expanded test and performance benefits. The proposed innovation is to develop an unsteady cavitation model based on a tabular equation of state and a representation of cavitation bubble dynamics that together describe the growth and collapse of nucleated bubbles in a liquid cryogen. Important nonequilibrium mechanical and thermal effects will be considered by using a drift-flux model and adding an additional energy equation for the liquid temperature. Validation of the advanced cavitation models will be accomplished for both steady and unsteady flows by comparing surface pressure and temperature data and computing power spectra from frequency domain analyses. The final analysis tool will be used to demonstrate the significant nonequilibrium flow behavior for both the validation cases and actual production analysis problems of interest to NASA.","benefits":"This technology will provide NASA with an efficient, robust cryogenic cavitation simulation tool suitable for use in propulsion systems ground test facility component design and analysis as well as other in advanced applications. The research product will provide enabling engineering and scientific technologies to predict complex cryogenic flow problems with nonequilibrium cavitation, resulting in reduced ground test facility costs and system risk by increasing test productivity. Potential enhancements include modified treatment of evaporation and condensation rates, turbulence/cavitation interaction modeling, detailed liquid/vapor thermal interface effects, variable transport properties, expanded thermodynamic databases and extended model validation. The proposed cavitation modeling tool is also applicable to hydrogen inducers, impellers and pumps operating at high vapor fraction.<br /> <br />The growing trend toward coupled multi-physics analyses is opening significant new markets as more difficult problems can be addressed using advanced computational techniques. The ability to robustly model complex cryogenic flows with cavitation will allow the commercial aerospace and defense industries to improve design and development of new products and streamline ground testing. Our analysis software can also be applied in the fields of medicine (magnetic resonance imaging), food processing (ultrasonic freezing) and semiconductor processing (plasma etching and vacuum pumping of gas contaminants). The basic architecture of the modeling framework can remain the same while new plug-in modules are developed to address different physics and design requirements.","releaseStatus":"Released","status":"Completed","destinationType":["Foundational_Knowledge"],"trlBegin":4,"trlCurrent":6,"trlEnd":6,"favorited":false,"detailedFunding":false,"programContacts":[],"endDateString":"Apr 2019","startDateString":"Apr 2017"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2017-04-19","technologyOutcomePath":"Advanced_To","infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities)","isIndirect":false,"infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateString":"Apr 2017","technologyOutcomeDateFullString":"April 2017","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced To","technologyOutcomeRationalePretty":""},{"technologyOutcomeId":97401,"projectId":89700,"project":{"projectId":89700,"title":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities","startDate":"2016-06-10","startYear":2016,"startMonth":6,"endDate":"2016-12-09","endYear":2016,"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. 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. Phase III contracts are funded from sources other than the SBIR and STTR programs and may be awarded without further competition.</li></ul><p><strong>Opportunity for Continued Technology Development Post-Phase II</strong>:</p><p>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.&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? Visit the program FAQs</p>","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":73,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer","manageGaps":false,"acronymOrTitle":"SBIR/STTR"},"description":"Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specified requirements over the operational envelope before the first flight. The development of advanced ground test technology components and systems that are capable of enhancing environment simulation, minimizing program test time, cost and risk and meeting environmental and safety regulations is focused on near-term products that augment existing state-of-the-art propulsion system test facilities. Thus improved capabilities to model and predict component behavior in harsh ground test environments are needed for enhanced facility design. In particular, components such as valves, check valves and chokes that are subjected to high pressure, high flow rate cryogenic environments will experience potentially damaging two phase flow effects such as cavitation. Robust cryogenic cavitation models for real fluids equations of state in the presence of mixed supersonic/subsonic flows are demonstrated to deal with poor solution convergence and numerical instabilities. The proposed innovation leverages modifications to the local preconditioning formulation of the Roe flux with a barotropic equation of state and uses a representative component flow problem to demonstrate the effectiveness of enhanced modifications to the cryogenic liquid tabular equation of state. Instabilities arising from the single temperature assumption in the two phase mixture equation of state, which must often be evaluated by extrapolating data too far from the saturation curve, are eliminated with a nonlinear temperature limiter that precludes non-physical behavior, such as imaginary mixture sound speeds. The result is an efficient, robust cryogenic cavitation model suitable for application to propulsion systems ground test facility component design and analysis efforts.","benefits":"This technology will provide NASA with an efficient, robust cryogenic cavitation modeling and prediction tool suitable for application to propulsion systems ground test facility component design and analysis. The research product will provide enabling engineering and scientific technologies to predict complex cryogenic flow problems, reduce ground test facility costs and overall system risk while increasing test productivity. Potential enhancements include improved treatment of evaporation and condensation rates, turbulence/cavitation interaction modeling, liquid/vapor thermal interface effects, variable transport properties, expanded thermodynamic databases and extended model validation. The proposed cavitation modeling tool is also applicable to hydrogen inducers, impellers and pumps operating at high vapor fraction.<br /> <br />The growing trend toward coupled multi-physics analyses is opening significant new markets as more difficult problems can be addressed using advanced computational techniques. The ability to robustly model complex cryogenic flows with cavitation will allow the commercial aerospace and defense industries to improve design and development of new products and streamline ground testing. Our analysis software can also be applied to marine propellers, boiler feed pumps and refrigerant systems. The basic architecture of the modeling framework can remain the same while new plug-in modules are developed to address different physics and design requirements.","releaseStatus":"Released","status":"Completed","destinationType":["Foundational_Knowledge"],"trlBegin":3,"trlCurrent":4,"trlEnd":4,"favorited":false,"detailedFunding":false,"programContacts":[],"endDateString":"Dec 2016","startDateString":"Jun 2016"},"relatedProjectId":93738,"relatedProject":{"projectId":93738,"title":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities","startDate":"2017-04-19","startYear":2017,"startMonth":4,"endDate":"2019-04-18","endYear":2019,"endMonth":4,"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. 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. Phase III contracts are funded from sources other than the SBIR and STTR programs and may be awarded without further competition.</li></ul><p><strong>Opportunity for Continued Technology Development Post-Phase II</strong>:</p><p>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.&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? Visit the program FAQs</p>","parentProgram":{"ableToSelect":false,"isActive":true,"description":"Catalyst is a portfolio of early stage programs that specialize in different innovation constituencies and mechanisms to push the state of the art in aerospace technology development","programId":92327,"responsibleMd":{"canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":""},"title":"Catalyst","manageGaps":false,"acronymOrTitle":"Catalyst"},"parentProgramId":92327,"programId":73,"responsibleMd":{"organizationId":4875,"organizationName":"Space Technology Mission Directorate","acronym":"STMD","organizationType":"NASA_Mission_Directorate","canUserEdit":false,"locationEdit":false,"organizationRolePretty":"","organizationTypePretty":"NASA Mission Directorate"},"responsibleMdOffice":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer","manageGaps":false,"acronymOrTitle":"SBIR/STTR"},"description":"Rigorous ground testing mitigates space propulsion system risk by enabling advanced component and system level rocket propulsion development and by demonstrating that designs reliably meet the specified requirements over the operational envelope before the first flight. The development of advanced ground test technology components and systems that are capable of enhancing environment simulation, minimizing program test time, cost and risk and meeting environmental and safety regulations is focused on near-term products that augment existing state-of-the-art propulsion system test facilities. Thus improved capabilities to model and predict component behavior in harsh ground test environments are needed for enhanced facility design. In particular, components such as pumps, turbines, valves and chokes may experience vibration and damage due to cavitation in the flowing liquid, and any reduction in the severity of the operating conditions would provide expanded test and performance benefits. The proposed innovation is to develop an unsteady cavitation model based on a tabular equation of state and a representation of cavitation bubble dynamics that together describe the growth and collapse of nucleated bubbles in a liquid cryogen. Important nonequilibrium mechanical and thermal effects will be considered by using a drift-flux model and adding an additional energy equation for the liquid temperature. Validation of the advanced cavitation models will be accomplished for both steady and unsteady flows by comparing surface pressure and temperature data and computing power spectra from frequency domain analyses. The final analysis tool will be used to demonstrate the significant nonequilibrium flow behavior for both the validation cases and actual production analysis problems of interest to NASA.","benefits":"This technology will provide NASA with an efficient, robust cryogenic cavitation simulation tool suitable for use in propulsion systems ground test facility component design and analysis as well as other in advanced applications. The research product will provide enabling engineering and scientific technologies to predict complex cryogenic flow problems with nonequilibrium cavitation, resulting in reduced ground test facility costs and system risk by increasing test productivity. Potential enhancements include modified treatment of evaporation and condensation rates, turbulence/cavitation interaction modeling, detailed liquid/vapor thermal interface effects, variable transport properties, expanded thermodynamic databases and extended model validation. The proposed cavitation modeling tool is also applicable to hydrogen inducers, impellers and pumps operating at high vapor fraction.<br /> <br />The growing trend toward coupled multi-physics analyses is opening significant new markets as more difficult problems can be addressed using advanced computational techniques. The ability to robustly model complex cryogenic flows with cavitation will allow the commercial aerospace and defense industries to improve design and development of new products and streamline ground testing. Our analysis software can also be applied in the fields of medicine (magnetic resonance imaging), food processing (ultrasonic freezing) and semiconductor processing (plasma etching and vacuum pumping of gas contaminants). The basic architecture of the modeling framework can remain the same while new plug-in modules are developed to address different physics and design requirements.","releaseStatus":"Released","status":"Completed","destinationType":["Foundational_Knowledge"],"trlBegin":4,"trlCurrent":6,"trlEnd":6,"favorited":false,"detailedFunding":false,"programContacts":[],"endDateString":"Apr 2019","startDateString":"Apr 2017"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2017-04-19","technologyOutcomePath":"Advanced_To","infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities)","isIndirect":true,"infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateString":"Apr 2017","technologyOutcomeDateFullString":"April 2017","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced To","technologyOutcomeRationalePretty":""}],"primaryImage":{"file":{"fileExtension":"jpg","fileId":362706,"presignedUpload":false,"fileSizeString":"0 Byte"},"libraryItemId":361331,"description":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities, Phase I","projectId":89700,"publishedDateString":"","entryDateString":"","libraryItemTypePretty":"","modifiedDateString":""},"libraryItems":[{"file":{"fileExtension":"pdf","fileId":362704,"fileName":"SBIR_2016_1_BC_H10_02-7667","fileSize":80624,"objectId":361329,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"78.7 KB"},"files":[{"fileExtension":"pdf","fileId":362704,"fileName":"SBIR_2016_1_BC_H10_02-7667","fileSize":80624,"objectId":361329,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"78.7 KB"}],"libraryItemId":361329,"title":"Briefing Chart","description":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities, Phase I Briefing Chart","libraryItemType":"Document","projectId":89700,"isPrimary":false,"internalOnly":false,"publishedDateString":"","entryDateString":"01/22/25 01:10 AM","libraryItemTypePretty":"Document","modifiedDateString":"01/08/24 08:27 PM"},{"file":{"fileExtension":"jpg","fileId":362706,"fileName":"SBIR_2016_1_BC_H10_02-7667","fileSize":61976,"objectId":361331,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"60.5 KB"},"files":[{"fileExtension":"jpg","fileId":362706,"fileName":"SBIR_2016_1_BC_H10_02-7667","fileSize":61976,"objectId":361331,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"60.5 KB"}],"libraryItemId":361331,"title":"Briefing Chart Image","description":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities, Phase I","libraryItemType":"Image","projectId":89700,"isPrimary":true,"internalOnly":false,"publishedDateString":"","entryDateString":"01/22/25 01:10 AM","libraryItemTypePretty":"Image","modifiedDateString":"01/08/24 08:27 PM"},{"file":{"fileExtension":"jpg","fileId":362707,"fileName":"SBIR_16_1_H10_02-7667","fileSize":80803,"objectId":361332,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"78.9 KB"},"files":[{"fileExtension":"jpg","fileId":362707,"fileName":"SBIR_16_1_H10_02-7667","fileSize":80803,"objectId":361332,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"78.9 KB"}],"libraryItemId":361332,"title":"Final Summary Chart Image","description":"Robust Cryogenic Cavitation Modeling for Propulsion Systems Ground Test Facilities, Phase I Project Image","libraryItemType":"Image","projectId":89700,"isPrimary":false,"internalOnly":false,"publishedDateString":"","entryDateString":"01/22/25 01:10 AM","libraryItemTypePretty":"Image","modifiedDateString":"01/08/24 08:27 PM"}],"states":[{"abbreviation":"MS","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Mississippi","stateTerritoryId":41,"isTerritory":false},{"abbreviation":"VT","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Vermont","stateTerritoryId":4,"isTerritory":false}],"endDateString":"Dec 2016","startDateString":"Jun 2016"}}