{"projectId":16680,"project":{"projectId":16680,"title":"Modular Electric Propulsion Test Bed Aircraft","startDate":"2013-05-23","startYear":2013,"startMonth":5,"endDate":"2014-05-22","endYear":2014,"endMonth":5,"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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These include zero, or near zero emissions, increased reliability and safety with only one moving part, reduced noise and vibration, increased comfort, and reduced maintenance. RHRC and the University of Illinois propose to develop an all electric test bed aircraft able to systematically evaluate new and existing technologies, which will make these systems, safe, reliable, and cost effective.","benefits":"An advanced aircraft electric propulsion system will have significant potential application across a wide range of NASA aircraft including both manned and unmanned systems. With two of NASA's primary goals being reduced aircraft emissions and noise, a realizable, efficient, and competitive aircraft electric propulsion system is a highly sought after commodity. The test bed aircraft will allow NASA personnel to quickly and rigorously evaluate multiple electrical propulsion systems in a cost effective and timely manner. The test bed will enable component optimization and a variety of operational studies to be performed, all of which will help define the important aspects and characteristics for a successful all-electric aircraft. The test bed can also be used to study new propulsion systems such as turboelectric distributed systems and hybrid electric systems. NASA will be eager to exploit the new test bed platform.<br /> <br />The potential for an advanced electric propulsion aircraft is quite good. If results from the test bed aircraft show that an all electric propulsion aircraft can be produced which can compete with a conventionally powered aircraft on both a performance and cost basis, the system will be in extremely high demand. The system's emissionless, or near emissionless operation will be highly desirable in an increasingly environmentally conscious world where ever more stringent emissions and noise standards are continually being enacted. 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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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Although there is a great deal of effort being put into advanced batteries, the most practical solution in the near term is to utilize a hybrid electric system. The proposed Phase II program builds upon the Phase I results by developing a detailed propulsion system simulator model for hybrid electric propulsion systems, with the ultimate goal of a bench test model of the propulsion system. Using a detailed multi-platform/mission trade study, a coupled parallel, uncoupled series, and split series-parallel hybrid system architecture will be compared to determine the most advantageous and efficient. The propulsion system simulator will also be used to perform a sensitivity analysis of each architecture to determine critical performance aspects for individual components.","benefits":"The NASA commercialization potential for an efficient, viable hybrid electric aircraft propulsion system is quite promising. The NASA Subsonic Fixed Wing (SFW) project has identified ambitious goals for the next three generations of aircraft, N+1, N+2, and N+3. For the N+3 generation (2025 timeframe), these include a -52 dB noise reduction relative to stage 4 noise limit, an -80% reduction in NOx emissions, and a -60% reduction in total mission energy consumption. Various forms of electric and hybrid electric propulsion hold a great deal of potential to make significant contributions towards these goals. NASA is currently investigating various technologies, ranging from advanced aerodynamics, superconducting electronics and electromechanical devices to advanced structures, under a program called Large Electric Aircraft Propulsion Technology (LEAP Tech). The proposed hybrid electric test bed will be an important tool in developing appropriate hybrid aircraft technologies to address these problems. The aircraft hybrid electric architecture simulation system, trade study results, and test bed will significantly enhance NASA's ability to meet the SFW N+3 goals, advancing the state-of-the-art to make hybrid electric systems efficient, competitive, safe, reliable, and cost effective.<br /> <br />The commercialization potential for an efficient, viable hybrid electric aircraft propulsion system is quite promising. The commercialization potential for a hybrid electric, multi-architecture propulsion system simulator is also quite good. The development of a tool for both detailed and preliminary design for hybrid electric propulsion systems will be highly sought after as hybrid electric propulsion systems become increasingly attractive and more prevalent. The development of a research test bed for studying all aspects of hybrid electric aircraft propulsion will act as a technical enabler. The propulsion system simulator will enable component optimization and a variety of operational studies to be performed, all of which will help define the important aspects and characteristics for a successful hybrid electric aircraft propulsion system. With the knowledge gained from this project, and the likely follow-on research, RHRC will be well positioned to team with aircraft manufacturers interested in producing hybrid electric aircraft propulsion systems. The propulsion system simulator coupled with a working testbed will be a key technology demonstration package with the capability to evaluate new components or concepts as they are developed. RHRC can also use the knowledge and experience gained during the program to develop hybrid electric propulsion systems for existing aircraft.","releaseStatus":"Released","status":"Completed","destinationType":["Foundational_Knowledge"],"trlBegin":3,"trlCurrent":5,"trlEnd":5,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":62051,"canUserEdit":false,"firstName":"Carlos","lastName":"Torrez","fullName":"Carlos Torrez","fullNameInverted":"Torrez, Carlos","email":"carlos.torrez@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":606,"programId":73,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":206378,"canUserEdit":false,"firstName":"Jason","lastName":"Kessler","fullName":"Jason L Kessler","fullNameInverted":"Kessler, Jason L","middleInitial":"L","email":"jason.l.kessler@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":607,"programId":73,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Dec 2016","startDateString":"Sep 2014"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2014-09-12","technologyOutcomePath":"Advanced_To","infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Modular Electric Propulsion Test Bed Aircraft)","isIndirect":false,"infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateFullString":"September 2014","technologyOutcomeDateString":"Sep 2014","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced To","technologyOutcomeRationalePretty":""},{"technologyOutcomeId":93752,"projectId":16680,"project":{"projectId":16680,"title":"Modular Electric Propulsion Test Bed Aircraft","startDate":"2013-05-23","startYear":2013,"startMonth":5,"endDate":"2014-05-22","endYear":2014,"endMonth":5,"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":"An all electric aircraft test bed is proposed to provide a dedicated development environment for the rigorous study and advancement of electrically powered aircraft. The new test bed aircraft will be developed from an existing conventional airframe and provide a dedicated platform to study, design, and test electrically powered propulsion systems for use in commercial, military, and general aviation vehicles and UAV systems. The test bed aircraft will allow various electrical propulsion system technologies to be tested to determine performance, reliability, safety, and cost. These include various motors, motor controllers, batteries, fuel cells, super capacitors, and propeller technologies. Additionally, the platform could be used to investigate performance characteristics unique to electric propulsion, determine the most accurate methods for measuring energy used and remaining, research redundancy possibilities unique to electric aircraft, and possible hybrid-electric power plant systems. An electric aircraft has several significant advantages over a conventional internal combustion driven aircraft. These include zero, or near zero emissions, increased reliability and safety with only one moving part, reduced noise and vibration, increased comfort, and reduced maintenance. RHRC and the University of Illinois propose to develop an all electric test bed aircraft able to systematically evaluate new and existing technologies, which will make these systems, safe, reliable, and cost effective.","benefits":"An advanced aircraft electric propulsion system will have significant potential application across a wide range of NASA aircraft including both manned and unmanned systems. With two of NASA's primary goals being reduced aircraft emissions and noise, a realizable, efficient, and competitive aircraft electric propulsion system is a highly sought after commodity. The test bed aircraft will allow NASA personnel to quickly and rigorously evaluate multiple electrical propulsion systems in a cost effective and timely manner. The test bed will enable component optimization and a variety of operational studies to be performed, all of which will help define the important aspects and characteristics for a successful all-electric aircraft. The test bed can also be used to study new propulsion systems such as turboelectric distributed systems and hybrid electric systems. NASA will be eager to exploit the new test bed platform.<br /> <br />The potential for an advanced electric propulsion aircraft is quite good. If results from the test bed aircraft show that an all electric propulsion aircraft can be produced which can compete with a conventionally powered aircraft on both a performance and cost basis, the system will be in extremely high demand. The system's emissionless, or near emissionless operation will be highly desirable in an increasingly environmentally conscious world where ever more stringent emissions and noise standards are continually being enacted. The additional benefits of electric propulsion including increased reliability, low maintenance and maintenance costs coupled with low noise and reduced vibration will make the system highly attractive to commercial, military, and general aviation markets for both manned and unmanned systems.","releaseStatus":"Released","status":"Completed","destinationType":["Earth"],"trlBegin":3,"trlCurrent":3,"trlEnd":3,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":62051,"canUserEdit":false,"firstName":"Carlos","lastName":"Torrez","fullName":"Carlos Torrez","fullNameInverted":"Torrez, Carlos","email":"carlos.torrez@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":606,"programId":73,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":206378,"canUserEdit":false,"firstName":"Jason","lastName":"Kessler","fullName":"Jason L Kessler","fullNameInverted":"Kessler, Jason L","middleInitial":"L","email":"jason.l.kessler@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":607,"programId":73,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"May 2014","startDateString":"May 2013"},"relatedProjectId":17873,"relatedProject":{"projectId":17873,"title":"Modular Electric Propulsion Test Bed Aircraft","startDate":"2014-09-12","startYear":2014,"startMonth":9,"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":"A hybrid electric aircraft simulation system and test bed is proposed to provide a dedicated development environment for the rigorous study and advancement of hybrid electric powered aircraft. 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Although there is a great deal of effort being put into advanced batteries, the most practical solution in the near term is to utilize a hybrid electric system. The proposed Phase II program builds upon the Phase I results by developing a detailed propulsion system simulator model for hybrid electric propulsion systems, with the ultimate goal of a bench test model of the propulsion system. Using a detailed multi-platform/mission trade study, a coupled parallel, uncoupled series, and split series-parallel hybrid system architecture will be compared to determine the most advantageous and efficient. The propulsion system simulator will also be used to perform a sensitivity analysis of each architecture to determine critical performance aspects for individual components.","benefits":"The NASA commercialization potential for an efficient, viable hybrid electric aircraft propulsion system is quite promising. 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The aircraft hybrid electric architecture simulation system, trade study results, and test bed will significantly enhance NASA's ability to meet the SFW N+3 goals, advancing the state-of-the-art to make hybrid electric systems efficient, competitive, safe, reliable, and cost effective.<br /> <br />The commercialization potential for an efficient, viable hybrid electric aircraft propulsion system is quite promising. The commercialization potential for a hybrid electric, multi-architecture propulsion system simulator is also quite good. The development of a tool for both detailed and preliminary design for hybrid electric propulsion systems will be highly sought after as hybrid electric propulsion systems become increasingly attractive and more prevalent. The development of a research test bed for studying all aspects of hybrid electric aircraft propulsion will act as a technical enabler. The propulsion system simulator will enable component optimization and a variety of operational studies to be performed, all of which will help define the important aspects and characteristics for a successful hybrid electric aircraft propulsion system. With the knowledge gained from this project, and the likely follow-on research, RHRC will be well positioned to team with aircraft manufacturers interested in producing hybrid electric aircraft propulsion systems. The propulsion system simulator coupled with a working testbed will be a key technology demonstration package with the capability to evaluate new components or concepts as they are developed. RHRC can also use the knowledge and experience gained during the program to develop hybrid electric propulsion systems for existing aircraft.","releaseStatus":"Released","status":"Completed","destinationType":["Foundational_Knowledge"],"trlBegin":3,"trlCurrent":5,"trlEnd":5,"favorited":false,"detailedFunding":false,"programContacts":[{"contactId":62051,"canUserEdit":false,"firstName":"Carlos","lastName":"Torrez","fullName":"Carlos Torrez","fullNameInverted":"Torrez, Carlos","email":"carlos.torrez@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Manager","programContactId":606,"programId":73,"programContactRolePretty":"Program Manager","projectContactRolePretty":""},{"contactId":206378,"canUserEdit":false,"firstName":"Jason","lastName":"Kessler","fullName":"Jason L Kessler","fullNameInverted":"Kessler, Jason L","middleInitial":"L","email":"jason.l.kessler@nasa.gov","receiveEmail":"Subscribed_User","programContactRole":"Program_Director","programContactId":607,"programId":73,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Dec 2016","startDateString":"Sep 2014"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2014-09-12","technologyOutcomePath":"Advanced_To","infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Modular Electric Propulsion Test Bed Aircraft)","isIndirect":true,"infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateFullString":"September 2014","technologyOutcomeDateString":"Sep 2014","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced To","technologyOutcomeRationalePretty":""}],"primaryImage":{"file":{"fileExtension":"jpg","fileId":357155,"presignedUpload":false,"fileSizeString":"0 Byte"},"libraryItemId":356550,"description":"Modular Electric Propulsion Test Bed Aircraft","projectId":16680,"publishedDateString":"","entryDateString":"","libraryItemTypePretty":"","modifiedDateString":""},"libraryItems":[{"file":{"fileExtension":"jpg","fileId":357155,"fileName":"STTR_2012_1_BC_T9_01-9754","fileSize":136104,"objectId":356550,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"132.9 KB"},"files":[{"fileExtension":"jpg","fileId":357155,"fileName":"STTR_2012_1_BC_T9_01-9754","fileSize":136104,"objectId":356550,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"132.9 KB"}],"libraryItemId":356550,"title":"Project Image","description":"Modular Electric Propulsion Test Bed Aircraft","libraryItemType":"Image","projectId":16680,"isPrimary":true,"internalOnly":false,"publishedDateString":"","entryDateString":"01/22/25 01:10 AM","libraryItemTypePretty":"Image","modifiedDateString":"01/08/24 08:27 PM"}],"states":[{"abbreviation":"CA","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"California","stateTerritoryId":59,"isTerritory":false},{"abbreviation":"IL","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Illinois","stateTerritoryId":39,"isTerritory":false}],"endDateString":"May 2014","startDateString":"May 2013"}}