{"projectId":17840,"project":{"projectId":17840,"title":"Cellular Load Responsive MLI: Structural In-Air and In-Space LH2 Insulation","startDate":"2014-06-20","startYear":2014,"startMonth":6,"endDate":"2014-12-19","endYear":2014,"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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CLR could provide 92% lower heat leak in-air during ground hold, and 97% lower heat leak in-space than SOFI. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. In this Phase I program, a CLRMLI system would be modeled, analyzed, designed, fabricated, installed on a cryotank, and tested for thermal performance for ground/ascent and in-space operation. CLRMLI could provide a robust SOFI replacement, with higher performance, lower mass, able to eliminate freezing/cryopumping of air components during ground and ascent stages. CLRMLI could help meet NASA's cryogenic fluid management requirements such as Zero Boil Off for cryogenic propellant storage and transfer.","benefits":"Cellular Load Responsive Multi-Layer Insulation (CLR) could provide a high performance thermal insulation by forming a light-weight vacuum cell layer integrated with load bearing LRMLI insulation layers. Preliminary thermal and structural modeling indicates this system could be a robust SOFI replacement that would offer a strong structural element and provide good thermal performance both in-air during ground and ascent phase operation, and in-space. This thermal insulation system could benefit NASA for both LH2 storage for long duration nuclear thermal propelled vehicles for deep space exploration, as well as cryogenic propellant storage for conventional LH2/LOX chemical propulsion systems. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. CLR MLI could provide 92% lower heat flux than current SOFI insulation for in-air use and 97% lower heat flux in-space. CLR might be a preferred thermal insulation for future NASA mission use, with a combination of high thermal performance, good structural strength, operable in both in-air and in-space environments, and it can be engineered for specific mission requirements.<br /> <br />Several aerospace prime contractors have interest in Quest/Ball IMLI and related insulation systems. CLRMLI could significantly improve launch vehicle insulation, reducing cryopropellant boiloff losses and increasing mission capabilities. High performance CLRMLI system can replace SOFI in cryogenic upper stages such as ACES, iCPS and SLS. Advances in thermal insulation developed for space cryogenics thermal control have relevance to terrestrial industrial applications. Reducing thermal conductivity and heat leak could have significant impact on Earth-based heating and cooling industrial processes and needs, for green energy and high energy efficiency. IMLI and derivatives might be able to provide improved thermal insulation for storage and preservation of cryogens for a variety of industrial uses, such as insulation for dewars for commercial, medical, industrial and research uses. Large LNG tanks could benefit from improved thermal insulation. CLRMLI might prove beneficial for liquid hydrogen storage for hydrogen fueled aircraft and ground vehicles. Quest's IMLI may play a beneficial role in reducing energy use. LRMLI has 24X lower heat leak than foam for use in refrigerator/freezers. LRMLI has 100X lower thermal conductivity than silica, and may keep molten salt batteries hot for electric vehicle use. 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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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CLR could provide 92% lower heat leak in-air during ground hold, and 97% lower heat leak in-space than SOFI. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. In this Phase I program, a CLRMLI system would be modeled, analyzed, designed, fabricated, installed on a cryotank, and tested for thermal performance for ground/ascent and in-space operation. CLRMLI could provide a robust SOFI replacement, with higher performance, lower mass, able to eliminate freezing/cryopumping of air components during ground and ascent stages. CLRMLI could help meet NASA's cryogenic fluid management requirements such as Zero Boil Off for cryogenic propellant storage and transfer.","benefits":"Cellular Load Responsive Multi-Layer Insulation (CLR) could provide a high performance thermal insulation by forming a light-weight vacuum cell layer integrated with load bearing LRMLI insulation layers. Preliminary thermal and structural modeling indicates this system could be a robust SOFI replacement that would offer a strong structural element and provide good thermal performance both in-air during ground and ascent phase operation, and in-space. This thermal insulation system could benefit NASA for both LH2 storage for long duration nuclear thermal propelled vehicles for deep space exploration, as well as cryogenic propellant storage for conventional LH2/LOX chemical propulsion systems. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. CLR MLI could provide 92% lower heat flux than current SOFI insulation for in-air use and 97% lower heat flux in-space. CLR might be a preferred thermal insulation for future NASA mission use, with a combination of high thermal performance, good structural strength, operable in both in-air and in-space environments, and it can be engineered for specific mission requirements.<br /> <br />Several aerospace prime contractors have interest in Quest/Ball IMLI and related insulation systems. CLRMLI could significantly improve launch vehicle insulation, reducing cryopropellant boiloff losses and increasing mission capabilities. High performance CLRMLI system can replace SOFI in cryogenic upper stages such as ACES, iCPS and SLS. Advances in thermal insulation developed for space cryogenics thermal control have relevance to terrestrial industrial applications. Reducing thermal conductivity and heat leak could have significant impact on Earth-based heating and cooling industrial processes and needs, for green energy and high energy efficiency. IMLI and derivatives might be able to provide improved thermal insulation for storage and preservation of cryogens for a variety of industrial uses, such as insulation for dewars for commercial, medical, industrial and research uses. Large LNG tanks could benefit from improved thermal insulation. CLRMLI might prove beneficial for liquid hydrogen storage for hydrogen fueled aircraft and ground vehicles. Quest's IMLI may play a beneficial role in reducing energy use. LRMLI has 24X lower heat leak than foam for use in refrigerator/freezers. LRMLI has 100X lower thermal conductivity than silica, and may keep molten salt batteries hot for electric vehicle use. 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CLRMLI could help meet NASA's cryogenic fluid management requirements such as Zero Boil Off for cryogenic propellant storage and transfer.","benefits":"Cellular Load Responsive Multi-Layer Insulation (CLR) could provide a high performance thermal insulation by forming a light-weight vacuum cell layer integrated with load bearing LRMLI insulation layers. Preliminary thermal and structural modeling indicates this system could be a robust SOFI replacement that would offer a strong structural element and provide good thermal performance both in-air during ground and ascent phase operation, and in-space. This thermal insulation system could benefit NASA for both LH2 storage for long duration nuclear thermal propelled vehicles for deep space exploration, as well as cryogenic propellant storage for conventional LH2/LOX chemical propulsion systems. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. CLR MLI could provide 92% lower heat flux than current SOFI insulation for in-air use and 97% lower heat flux in-space. CLR might be a preferred thermal insulation for future NASA mission use, with a combination of high thermal performance, good structural strength, operable in both in-air and in-space environments, and it can be engineered for specific mission requirements.<br /> <br />Several aerospace prime contractors have interest in Quest/Ball IMLI and related insulation systems. CLRMLI could significantly improve launch vehicle insulation, reducing cryopropellant boiloff losses and increasing mission capabilities. High performance CLRMLI system can replace SOFI in cryogenic upper stages such as ACES, iCPS and SLS. Advances in thermal insulation developed for space cryogenics thermal control have relevance to terrestrial industrial applications. Reducing thermal conductivity and heat leak could have significant impact on Earth-based heating and cooling industrial processes and needs, for green energy and high energy efficiency. IMLI and derivatives might be able to provide improved thermal insulation for storage and preservation of cryogens for a variety of industrial uses, such as insulation for dewars for commercial, medical, industrial and research uses. Large LNG tanks could benefit from improved thermal insulation. CLRMLI might prove beneficial for liquid hydrogen storage for hydrogen fueled aircraft and ground vehicles. Quest's IMLI may play a beneficial role in reducing energy use. LRMLI has 24X lower heat leak than foam for use in refrigerator/freezers. LRMLI has 100X lower thermal conductivity than silica, and may keep molten salt batteries hot for electric vehicle use. Wrapped MLI has 12X lower heat leak than MLI, and may enable high performance vacuum jacketed pipe insulation for industrial cold transfer piping.","releaseStatus":"Released","status":"Completed","destinationType":["Mars"],"trlBegin":2,"trlCurrent":4,"trlEnd":4,"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":194,"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":143,"programId":73,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Dec 2014","startDateString":"Jun 2014"},"relatedProjectId":33271,"relatedProject":{"projectId":33271,"title":"Cellular Load Responsive MLI: Structural In-Air and In-Space LH2 Insulation","startDate":"2015-05-30","startYear":2015,"startMonth":5,"endDate":"2018-08-15","endYear":2018,"endMonth":8,"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","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","acronymOrTitle":"SBIR/STTR"},"description":"Advanced space propulsion systems are a critical need for future NASA deep space missions. High thrust engines could revolutionize space exploration. Nuclear Thermal Propulsion (\"NTP\") is a high thrust/high Isp propulsion technology. Reduced or Zero Boil Off of LH2 propellant for long duration missions is among the critical technology advancements needed for cryogenic propellant storage for both NTP and chemical propulsion. Quest proposes to continue development of Cellular Load Responsive MLI (CLRMLI), an innovative, high performance thermal insulation system. CLRMLI is a novel technology with a cryopumping cellular core containing Load Responsive MLI layers. This new form of insulation uses cryosorption cryopumping to self-evacuate when in contact with cryogenic propellant tanks, allowing high thermal performance in-air and in-space. The Phase I program successfully demonstrated CLRMLI is a feasible and attractive insulation for new launch vehicle platforms and LH2 or LNG powered aircraft. CLRMLI has a measured heat flux of 11.4W/m2, 25X lower than SOFI (vacuum). NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the","benefits":"CLRMLI is a novel high performance thermal insulation offering dramatically better thermal performance than SOFI both in-air and in-space. CLRMLI could be a good SOFI replacement for launch vehicle platforms, such as SLS, where it could help solve cryogenic propellant boiloff concerns. SLS is baselining using SOFI at 1.2\", nearly double the usual thickness, to reduce boiloff. CLRMLI, with a measured heat flux of 46 W/m2 in-air and 11 W/m2, offers much lower heat leak than SOFI (289 W/m2). Boeing has indicated strong interest in CLRMLI (and the companion VCMLI concept), and will support this Phase II work with engineering support. CLRMLI could benefit NASA for LH2 storage for long duration nuclear thermal propelled vehicles for deep space exploration, as well as cryogenic propellant storage for conventional LH2/LOX chemical propulsion systems. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. CLRMLI could provide 92% lower heat flux than current SOFI insulation for in-air use and 97% lower heat flux in-space. CLRMLI might be a preferred thermal insulation for future NASA mission use, with a combination of high thermal performance, good structural strength, operable in both in-air and in-space environments, and it can be engineered for specific mission requirements.<br /> <br />Several aerospace prime contractors have interest in Quest/Ball IMLI and related insulation systems. CLRMLI could significantly improve launch vehicle insulation, reduce cryopropellant boiloff and increase mission capabilities. High performance CLRMLI system can replace SOFI in cryogenic upper stages such as AC, ACES and SLS. CLRMLI is ideal insulation for LH2 powered aircraft such as Boeing's Phantom Eye, and for LNG fueled aircraft. Advances in thermal insulation developed for space cryogenics thermal control have relevance to terrestrial industrial applications. Reducing thermal conductivity and heat leak could have significant impact on Earth-based heating and cooling industrial processes and needs, for green energy and high energy efficiency. IMLI and derivatives might be able to provide improved thermal insulation for storage and preservation of cryogens for a variety of industrial uses. LNG tanks could benefit from improved thermal insulation, and CLRMLI might benefit LH2 storage for hydrogen fueled aircraft and ground vehicles.","releaseStatus":"Released","status":"Completed","destinationType":["Mars"],"trlBegin":4,"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":194,"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":143,"programId":73,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Aug 2018","startDateString":"May 2015"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2015-05-30","technologyOutcomePath":"Advanced_To","infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Cellular Load Responsive MLI: Structural In-Air and In-Space LH2 Insulation)","isIndirect":false,"technologyOutcomeRationalePretty":"","infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateString":"May 2015","technologyOutcomeDateFullString":"May 2015","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced To"},{"technologyOutcomeId":94605,"projectId":17840,"project":{"projectId":17840,"title":"Cellular Load Responsive MLI: Structural In-Air and In-Space LH2 Insulation","startDate":"2014-06-20","startYear":2014,"startMonth":6,"endDate":"2014-12-19","endYear":2014,"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","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","acronymOrTitle":"SBIR/STTR"},"description":"Advanced space propulsion systems are a critical need for future NASA deep space missions. High thrust or high Isp engines could revolutionize space exploration. Nuclear Thermal Propulsion (\"NTP\") is a high thrust/high Isp propulsion technology, with a demonstrated Isp ~850, twice that of chemical rockets. Zero boil off of LH2 propellant for long duration missions is among the critical technology advancements needed for NTP. Quest proposes to develop and test an innovative, high performance thermal insulation system, designed to provide high performance on large LH2 tanks. Cellular Load Responsive (\"CLR\") multilayer insulation integrates a mid-size cryopumping self-evacuating vacuum cell core with load bearing LRMLI within the compartments. CLR can offer a structural, high performance insulation system, that is damage tolerant, can support external loads such as thermal shields, and provides good thermal insulation both in-air (for ground and ascent phases) and in-vacuum (once in-space). CLR could provide 92% lower heat leak in-air during ground hold, and 97% lower heat leak in-space than SOFI. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. In this Phase I program, a CLRMLI system would be modeled, analyzed, designed, fabricated, installed on a cryotank, and tested for thermal performance for ground/ascent and in-space operation. CLRMLI could provide a robust SOFI replacement, with higher performance, lower mass, able to eliminate freezing/cryopumping of air components during ground and ascent stages. CLRMLI could help meet NASA's cryogenic fluid management requirements such as Zero Boil Off for cryogenic propellant storage and transfer.","benefits":"Cellular Load Responsive Multi-Layer Insulation (CLR) could provide a high performance thermal insulation by forming a light-weight vacuum cell layer integrated with load bearing LRMLI insulation layers. Preliminary thermal and structural modeling indicates this system could be a robust SOFI replacement that would offer a strong structural element and provide good thermal performance both in-air during ground and ascent phase operation, and in-space. This thermal insulation system could benefit NASA for both LH2 storage for long duration nuclear thermal propelled vehicles for deep space exploration, as well as cryogenic propellant storage for conventional LH2/LOX chemical propulsion systems. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. CLR MLI could provide 92% lower heat flux than current SOFI insulation for in-air use and 97% lower heat flux in-space. CLR might be a preferred thermal insulation for future NASA mission use, with a combination of high thermal performance, good structural strength, operable in both in-air and in-space environments, and it can be engineered for specific mission requirements.<br /> <br />Several aerospace prime contractors have interest in Quest/Ball IMLI and related insulation systems. CLRMLI could significantly improve launch vehicle insulation, reducing cryopropellant boiloff losses and increasing mission capabilities. High performance CLRMLI system can replace SOFI in cryogenic upper stages such as ACES, iCPS and SLS. Advances in thermal insulation developed for space cryogenics thermal control have relevance to terrestrial industrial applications. Reducing thermal conductivity and heat leak could have significant impact on Earth-based heating and cooling industrial processes and needs, for green energy and high energy efficiency. IMLI and derivatives might be able to provide improved thermal insulation for storage and preservation of cryogens for a variety of industrial uses, such as insulation for dewars for commercial, medical, industrial and research uses. Large LNG tanks could benefit from improved thermal insulation. CLRMLI might prove beneficial for liquid hydrogen storage for hydrogen fueled aircraft and ground vehicles. Quest's IMLI may play a beneficial role in reducing energy use. LRMLI has 24X lower heat leak than foam for use in refrigerator/freezers. LRMLI has 100X lower thermal conductivity than silica, and may keep molten salt batteries hot for electric vehicle use. Wrapped MLI has 12X lower heat leak than MLI, and may enable high performance vacuum jacketed pipe insulation for industrial cold transfer piping.","releaseStatus":"Released","status":"Completed","destinationType":["Mars"],"trlBegin":2,"trlCurrent":4,"trlEnd":4,"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":194,"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":143,"programId":73,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Dec 2014","startDateString":"Jun 2014"},"relatedProjectId":33271,"relatedProject":{"projectId":33271,"title":"Cellular Load Responsive MLI: Structural In-Air and In-Space LH2 Insulation","startDate":"2015-05-30","startYear":2015,"startMonth":5,"endDate":"2018-08-15","endYear":2018,"endMonth":8,"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","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","acronymOrTitle":"SBIR/STTR"},"description":"Advanced space propulsion systems are a critical need for future NASA deep space missions. High thrust engines could revolutionize space exploration. Nuclear Thermal Propulsion (\"NTP\") is a high thrust/high Isp propulsion technology. Reduced or Zero Boil Off of LH2 propellant for long duration missions is among the critical technology advancements needed for cryogenic propellant storage for both NTP and chemical propulsion. Quest proposes to continue development of Cellular Load Responsive MLI (CLRMLI), an innovative, high performance thermal insulation system. CLRMLI is a novel technology with a cryopumping cellular core containing Load Responsive MLI layers. This new form of insulation uses cryosorption cryopumping to self-evacuate when in contact with cryogenic propellant tanks, allowing high thermal performance in-air and in-space. The Phase I program successfully demonstrated CLRMLI is a feasible and attractive insulation for new launch vehicle platforms and LH2 or LNG powered aircraft. CLRMLI has a measured heat flux of 11.4W/m2, 25X lower than SOFI (vacuum). NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the","benefits":"CLRMLI is a novel high performance thermal insulation offering dramatically better thermal performance than SOFI both in-air and in-space. CLRMLI could be a good SOFI replacement for launch vehicle platforms, such as SLS, where it could help solve cryogenic propellant boiloff concerns. SLS is baselining using SOFI at 1.2\", nearly double the usual thickness, to reduce boiloff. CLRMLI, with a measured heat flux of 46 W/m2 in-air and 11 W/m2, offers much lower heat leak than SOFI (289 W/m2). Boeing has indicated strong interest in CLRMLI (and the companion VCMLI concept), and will support this Phase II work with engineering support. CLRMLI could benefit NASA for LH2 storage for long duration nuclear thermal propelled vehicles for deep space exploration, as well as cryogenic propellant storage for conventional LH2/LOX chemical propulsion systems. NASA's Technology Roadmaps call \"Zero Boil Off storage of cryogenic propellants for long duration missions\" and \"Nuclear Thermal Propulsion components and systems\" the #2 and #7 ranked technical challenge for future NASA missions. CLRMLI could provide 92% lower heat flux than current SOFI insulation for in-air use and 97% lower heat flux in-space. CLRMLI might be a preferred thermal insulation for future NASA mission use, with a combination of high thermal performance, good structural strength, operable in both in-air and in-space environments, and it can be engineered for specific mission requirements.<br /> <br />Several aerospace prime contractors have interest in Quest/Ball IMLI and related insulation systems. CLRMLI could significantly improve launch vehicle insulation, reduce cryopropellant boiloff and increase mission capabilities. High performance CLRMLI system can replace SOFI in cryogenic upper stages such as AC, ACES and SLS. CLRMLI is ideal insulation for LH2 powered aircraft such as Boeing's Phantom Eye, and for LNG fueled aircraft. Advances in thermal insulation developed for space cryogenics thermal control have relevance to terrestrial industrial applications. Reducing thermal conductivity and heat leak could have significant impact on Earth-based heating and cooling industrial processes and needs, for green energy and high energy efficiency. IMLI and derivatives might be able to provide improved thermal insulation for storage and preservation of cryogens for a variety of industrial uses. LNG tanks could benefit from improved thermal insulation, and CLRMLI might benefit LH2 storage for hydrogen fueled aircraft and ground vehicles.","releaseStatus":"Released","status":"Completed","destinationType":["Mars"],"trlBegin":4,"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":194,"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":143,"programId":73,"programContactRolePretty":"Program Director","projectContactRolePretty":""}],"endDateString":"Aug 2018","startDateString":"May 2015"},"technologyOutcomePartner":"Other","technologyOutcomeDate":"2015-05-30","technologyOutcomePath":"Advanced_To","infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Cellular Load Responsive MLI: Structural In-Air and In-Space LH2 Insulation)","isIndirect":true,"technologyOutcomeRationalePretty":"","infusionPretty":"","isBiDirectional":true,"technologyOutcomeDateString":"May 2015","technologyOutcomeDateFullString":"May 2015","technologyOutcomePartnerPretty":"Other","technologyOutcomePathPretty":"Advanced To"}],"libraryItems":[{"file":{"fileExtension":"jpg","fileId":358050,"fileName":"SBIR_2014_1_BC_H2_03-8602","fileSize":60115,"objectId":357297,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"58.7 KB"},"files":[{"fileExtension":"jpg","fileId":358050,"fileName":"SBIR_2014_1_BC_H2_03-8602","fileSize":60115,"objectId":357297,"objectType":"libraryItemFiles","presignedUpload":false,"fileSizeString":"58.7 KB"}],"libraryItemId":357297,"title":"Briefing Chart Image","description":"Cellular Load Responsive MLI: Structural In-Air and In-Space LH2 Insulation, Phase I","libraryItemType":"Image","projectId":17840,"isPrimary":false,"internalOnly":false,"publishedDateString":"","entryDateString":"01/22/25 01:10 AM","libraryItemTypePretty":"Image","modifiedDateString":"01/08/24 08:27 PM"}],"states":[{"abbreviation":"AL","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Alabama","stateTerritoryId":18,"isTerritory":false},{"abbreviation":"CO","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Colorado","stateTerritoryId":15,"isTerritory":false}],"endDateString":"Dec 2014","startDateString":"Jun 2014"}}