{"project":{"acronym":"","projectId":8625,"title":"Unconditionally Stable Low Dropout Regulators for Extreme Environments","primaryTaxonomyNodes":[{"taxonomyNodeId":10784,"taxonomyRootId":8816,"parentNodeId":10780,"level":3,"code":"TX10.1.4","title":"Hazard Assessment","definition":"Hazard assessment technologies evaluate whether the state of the environment, the state of the system, and/or their interaction pose a threat to the safety of actions (or inactions) that are contemplated, which could compromise the system or mission.","exampleTechnologies":"Terrain hazard assessment for spacecraft planetary landing, traversability analysis for surface mobility, collision-risk assessment of aerial mobility, safety-assessment for a life-support system","hasChildren":false,"hasInteriorContent":true}],"startTrl":4,"currentTrl":5,"endTrl":5,"benefits":"Low dropout regulators are ubiquitous in commercial consumer electronics and automotive systems. A non-hardened version of the regulator we are proposing to develop will be inexpensive to manufacture using high volume commercial CMOS foundries. Our business models suggest that such a component can be manufactured at a cost per die that is competitive with existing products but without the need for an external compensation capacitor thereby reducing the overall costs and part count of the power management system. If this is confirmed our regulator component has the potential for widespread commercial adoption. Other non-NASA commercial applications of our patented transistor technology include low power transceivers for medical implants that use the FCC approved MICS band as well as for data telemetry within the Industrial, Scientific & Medical (ISM) bands. Our MESFET technology is capable of higher voltage operation than the CMOS transistors making it very suitable as the input/output device in commercial ASICs such as those offered by Honeywell and our other Phase 3 commercialization partners.
Radiation tolerant low dropout regulators capable of operating in extreme environments with fewer external components will be of widespread use to NASA missions that target the moon, Mars and Europa. The LDO regulator is a key component in most power management systems including point-of-load supplies. By developing power management components for wide temperature range operation (-180C to +150C) we are enabling missions that will benefit from components mounted directly in the Lunar and Martian environments i.e. outside of any thermally controlled warm box. These components will also be of use in missions to Venus that employ environmental chambers with temperatures controlled to >10V. NASA faces challenges with component obsolescence due to the reduction in supply voltage of application specific integrated circuits (ASICs) with each new CMOS generation. Our MESFET component has the potential for extending the life of an ASIC product without the expense of a complete re-design.","description":"We have developed a fully integrated LDO regulator using a patented transistor technology that can be manufactured in high volume commercial semiconductor foundries with no changes to the process flow. The regulator is stable under all load conditions without the need for an external compensation capacitor thereby reducing the mass/volume of the power management system and increasing reliability. The existing LDO component has very competitive figures of merit (dropout voltage, transient response, power supply rejection) compared to existing components targeting commercial consumer electronics. The work we are proposing for this Phase 1 activity will confirm the expected wide temperature range operation (-180C to +150C) and radiation tolerance (200krads(Si) to 1 Mrad(Si)) of the existing component. Based on these measurements we shall design, simulate and layout LDO regulators for nominal load currents of 100 mA and 1A for fabrication at two rad-hard CMOS foundries during a follow-on Phase 2 activity. The LDO regulators will be designed as drop-in replacements for many existing components. They can also be integrated directly on chip as part of an application specific integrated circuit thereby reducing the chip count still further.","startYear":2010,"startMonth":1,"endYear":2010,"endMonth":7,"statusDescription":"Completed","principalInvestigators":[{"contactId":431051,"canUserEdit":false,"firstName":"Seth","lastName":"Wilk","fullName":"Seth Wilk","fullNameInverted":"Wilk, Seth","primaryEmail":"swilk@sjtmicropower.com","publicEmail":true,"nacontact":false}],"programDirectors":[{"contactId":206378,"canUserEdit":false,"firstName":"Jason","lastName":"Kessler","fullName":"Jason L Kessler","fullNameInverted":"Kessler, Jason L","middleInitial":"L","primaryEmail":"jason.l.kessler@nasa.gov","publicEmail":true,"nacontact":false}],"programExecutives":[{"contactId":215154,"canUserEdit":false,"firstName":"Jennifer","lastName":"Gustetic","fullName":"Jennifer L Gustetic","fullNameInverted":"Gustetic, Jennifer L","middleInitial":"L","primaryEmail":"jennifer.l.gustetic@nasa.gov","publicEmail":true,"nacontact":false}],"programManagers":[{"contactId":62051,"canUserEdit":false,"firstName":"Carlos","lastName":"Torrez","fullName":"Carlos Torrez","fullNameInverted":"Torrez, Carlos","primaryEmail":"carlos.torrez@nasa.gov","publicEmail":true,"nacontact":false}],"projectManagers":[{"contactId":188536,"canUserEdit":false,"firstName":"Jack","lastName":"Shue","fullName":"Jack Shue","fullNameInverted":"Shue, Jack","primaryEmail":"John.L.Shue@nasa.gov","publicEmail":true,"nacontact":false},{"contactId":461333,"canUserEdit":false,"firstName":"Theresa","lastName":"Stanley","fullName":"Theresa M Stanley","fullNameInverted":"Stanley, Theresa M","middleInitial":"M","primaryEmail":"theresa.m.stanley@nasa.gov","publicEmail":true,"nacontact":false}],"website":"","libraryItems":[],"transitions":[{"transitionId":68211,"projectId":8625,"transitionDate":"2010-07-01","path":"Closed Out","closeoutDocuments":[{"title":"Final Summary Chart","file":{"fileExtension":"pdf","fileId":307388,"fileName":"SBIR_2009_1_FSC_X1.03-9811","fileSize":228278,"objectId":68211,"objectType":{"lkuCodeId":1841,"code":"TRANSITION_FILES","description":"Transition Files","lkuCodeTypeId":182,"lkuCodeType":{"codeType":"OBJECT_TYPE","description":"Object Type"}},"fileSizeString":"222.9 KB"},"transitionId":68211,"fileId":307388}],"infoText":"Closed out","infoTextExtra":"","dateText":"July 2010"},{"transitionId":68212,"projectId":8625,"partner":"Other","transitionDate":"2011-06-01","path":"Advanced To","relatedProjectId":9641,"relatedProject":{"acronym":"","projectId":9641,"title":"Unconditionally Stable Low Dropout Regulators for Extreme Environments","startTrl":5,"currentTrl":6,"endTrl":6,"benefits":"Low dropout regulators are ubiquitous in commercial consumer electronics and automotive systems. A non-hardened version of the regulator we are proposing to develop will be inexpensive to manufacture using high volume commercial CMOS foundries. Our business models show that such a component can be manufactured at a cost per die that is competitive with existing products but without the need for an external compensation capacitor thereby reducing the overall costs and part count of the power management system. If this is confirmed our regulator component has the potential for widespread commercial adoption. We are working with our commercialization partners at On Semiconductor and Honeywell to develop these non-NASA applications. As well as a standalone product, we are developing the low dropout linear regulator as a scalable design that can be included in application specific integrated circuits (ASICs) as a licensed 'IP block'. ASICs are widely used for non-NASA applications by the Department of Defense and aerospace companies.
The MESFET-based linear regulator technology has the potential for widespread NASA applications in power management systems exposed to extreme environments. The high radiation tolerance we have demonstrated is attractive for orbital earth science studies as well as lunar and interplanetary missions. Our technology may even be suitable for spacecraft exposed to high radiation environments such as the Europa Jupiter System Mission. Missions to the outer reaches of the solar system that depend on a radiothermal generator are exposed to on-board radiation from the RTG and require the high level of radiation tolerance we expect from the final MESFET regulator component. We expect the MESFET technology to be relatively immune to single event effects and therefore suitable for solar observatories and lunar sensors exposed to solar flares. The MESFET technology can operate over the -196C<+150C temperature range, making it useful for robotic systems on the Moon or Mars. The current Martian rovers use a thermally controlled warm-electronics-box (WEB). Innovations on the Mars Science Laboratory have allowed wide temperature range electronics to be placed outside the WEB thereby reducing weight and increasing reliability. Our wide temperature range MESFET technology will enable further innovation for missions to hostile and extreme environments. This includes missions to Venus that employ environmental chambers with temperatures controlled to T<150C.","description":"We have developed a low dropout (LDO) regulator using a patented MESFET transistor technology that can be manufactured in commercial CMOS foundries with no changes to the process flow. The regulator is stable under all load conditions without an external compensation capacitor, thereby reducing the mass/volume of the power management system and increasing reliability. The MESFET-based LDO component has very competitive figures of merit (dropout voltage, transient response, power supply rejection) compared to existing components. During Phase 1 we confirmed that the components were unconditionally stable without an external compensation capacitor over the temperature range -196C to +150C and for radiation doses up to 1 Mrad(Si). We shall build on the Phase 1 design effort to demonstrate two fully integrated LDO regulators rated up to 1A with dropout voltages of less than 50 mV. One part will be fabricated using a qualified rad-hard SOI CMOS foundry in collaboration with Honeywell, one of our commercialization partners. The other component will be fabricated using the low-cost/high-volume foundry available from IBM. Both parts will have a nominal output voltage of 1.8V with 1% accuracy. Other designs will target user adjustable voltages in the range 1.2-2V. The feasibility of using the MESFET technology for low voltage applications (e.g. 0.8V) will be explored. All parts will be tested over the temperature range -150C to +150C and after irradiation exposure to a TID of 1 Mrad from a Co-60 source. The enhanced low dose rate sensitivity (ELDRS) of the components will be studied using a low dose rate Cs-137 source. The characteristics of all the components will be documented, and parts made available to NASA and potential customers as deliverables from the Phase 2 activity. We shall work with our commercialization partners to have the LDO regulator design adopted as a licensed 'IP block' and to develop low cost versions for the wider consumer electronics market.","startYear":2011,"startMonth":6,"endYear":2014,"endMonth":3,"statusDescription":"Completed","website":"","program":{"acronym":"SBIR/STTR","active":true,"description":"
The NASA SBIR and STTR programs fund the research, development, and demonstration of innovative technologies that fulfill NASA needs as described in the annual Solicitations and have significant potential for successful commercialization. If you are a small business concern (SBC) with 500 or fewer employees or a non-profit RI such as a university or a research laboratory with ties to an SBC, then NASA encourages you to learn more about the SBIR and STTR programs as a potential source of seed funding for the development of your innovations.
The SBIR and STTR programs have 3 phases:
The SBIR and STTR Phase I contracts last for 6 months with a maximum funding of $125,000, and Phase II contracts last for 24 months with a maximum funding of $750,000 - $1.5 million.
Opportunity for Continued Technology Development Post-Phase II:
The NASA SBIR/STTR Program currently has in place two initiatives for supporting its small business partners past the basic Phase I and Phase II elements of the program that emphasize opportunities for commercialization. Specifically, the NASA SBIR/STTR Program has the Phase II Enhancement (Phase II-E) and Phase II eXpanded (Phase II-X) contract options.
Please review the links below to obtain more information on the SBIR/STTR programs.
Provides an overview of the SBIR and STTR programs as implemented by NASA
Provides access to the annual SBIR/STTR Solicitations containing detailed information on the program eligibility requirements, proposal instructions and research topics and subtopics
Schedule and links for the SBIR/STTR solicitations and selection announcements
Federal and non-Federal sources of assistance for small business
Search our complete archive of awarded project abstracts to learn about what NASA has funded
Still have questions? Visit the program FAQs
","programId":73,"responsibleMd":{"acronym":"STMD","canUserEdit":false,"city":"","external":false,"linkCount":0,"organizationId":4875,"organizationName":"Space Technology Mission Directorate","organizationType":"NASA_Mission_Directorate","naorganization":false,"organizationTypePretty":"NASA Mission Directorate"},"responsibleMdId":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer"},"lastUpdated":"2024-1-10","releaseStatusString":"Released","viewCount":676,"endDateString":"Mar 2014","startDateString":"Jun 2011"},"infoText":"Advanced within the program","infoTextExtra":"Another project within the program (Unconditionally Stable Low Dropout Regulators for Extreme Environments)","dateText":"June 2011"}],"responsibleMd":{"acronym":"STMD","canUserEdit":false,"city":"","external":false,"linkCount":0,"organizationId":4875,"organizationName":"Space Technology Mission Directorate","organizationType":"NASA_Mission_Directorate","naorganization":false,"organizationTypePretty":"NASA Mission Directorate"},"program":{"acronym":"SBIR/STTR","active":true,"description":"The NASA SBIR and STTR programs fund the research, development, and demonstration of innovative technologies that fulfill NASA needs as described in the annual Solicitations and have significant potential for successful commercialization. If you are a small business concern (SBC) with 500 or fewer employees or a non-profit RI such as a university or a research laboratory with ties to an SBC, then NASA encourages you to learn more about the SBIR and STTR programs as a potential source of seed funding for the development of your innovations.
The SBIR and STTR programs have 3 phases:
The SBIR and STTR Phase I contracts last for 6 months with a maximum funding of $125,000, and Phase II contracts last for 24 months with a maximum funding of $750,000 - $1.5 million.
Opportunity for Continued Technology Development Post-Phase II:
The NASA SBIR/STTR Program currently has in place two initiatives for supporting its small business partners past the basic Phase I and Phase II elements of the program that emphasize opportunities for commercialization. Specifically, the NASA SBIR/STTR Program has the Phase II Enhancement (Phase II-E) and Phase II eXpanded (Phase II-X) contract options.
Please review the links below to obtain more information on the SBIR/STTR programs.
Provides an overview of the SBIR and STTR programs as implemented by NASA
Provides access to the annual SBIR/STTR Solicitations containing detailed information on the program eligibility requirements, proposal instructions and research topics and subtopics
Schedule and links for the SBIR/STTR solicitations and selection announcements
Federal and non-Federal sources of assistance for small business
Search our complete archive of awarded project abstracts to learn about what NASA has funded
Still have questions? Visit the program FAQs
","programId":73,"responsibleMd":{"acronym":"STMD","canUserEdit":false,"city":"","external":false,"linkCount":0,"organizationId":4875,"organizationName":"Space Technology Mission Directorate","organizationType":"NASA_Mission_Directorate","naorganization":false,"organizationTypePretty":"NASA Mission Directorate"},"responsibleMdId":4875,"stockImageFileId":36648,"title":"Small Business Innovation Research/Small Business Tech Transfer"},"leadOrganization":{"canUserEdit":false,"city":"Fountain Hills","congressionalDistrict":"Arizona 01","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"external":true,"linkCount":0,"organizationId":3241,"organizationName":"SJT Micropower","organizationType":"Industry","stateTerritory":{"abbreviation":"AZ","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Arizona","stateTerritoryId":45},"stateTerritoryId":45,"ein":"270176027 ","uei":"QWH4TNSN2CY6","naorganization":false,"organizationTypePretty":"Industry"},"supportingOrganizations":[{"acronym":"GSFC","canUserEdit":false,"city":"Greenbelt","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"external":false,"linkCount":0,"organizationId":4947,"organizationName":"Goddard Space Flight Center","organizationType":"NASA_Center","stateTerritory":{"abbreviation":"MD","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Maryland","stateTerritoryId":3},"stateTerritoryId":3,"naorganization":false,"organizationTypePretty":"NASA Center"}],"statesWithWork":[{"abbreviation":"AZ","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Arizona","stateTerritoryId":45},{"abbreviation":"MD","country":{"abbreviation":"US","countryId":236,"name":"United States"},"countryId":236,"name":"Maryland","stateTerritoryId":3}],"lastUpdated":"2024-1-10","releaseStatusString":"Released","viewCount":439,"endDateString":"Jul 2010","startDateString":"Jan 2010"}}