{"project":{"acronym":"","projectId":33710,"title":"Compact Ultrasensitive Erbium-doped Waveguide Optical Gyros","primaryTaxonomyNodes":[{"taxonomyNodeId":10976,"taxonomyRootId":8816,"parentNodeId":10973,"level":3,"code":"TX17.2.3","title":"Navigation Sensors","definition":"This area covers technologies for onboard sensors/sensor systems (sensor hardware and embedded sensor software) for taking measurements required to estimate flight path/orbit/trajectory parameters. This area includes navigation sensors/sensor systems for both absolute navigation function and relative navigation functions.","exampleTechnologies":"Inertial Measurement Units (IMUs), precision gyroscopes, accelerometers, GPS/Global Navigation Satellite System (GNSS) receivers, LIDARs, laser rangefinders, laser altimeters, radio frequency (RF)-based inter-spacecraft ranging systems, visible wavelength cameras, infrared wavelength cameras, precision frequency and timing devices such as oscillators and clocks, cold atom sensors, navigation transponders, navigation beacons, velocimeters, radars","hasChildren":false,"hasInteriorContent":true}],"startTrl":2,"currentTrl":4,"endTrl":4,"benefits":"The primary focus of this program is to provide high-performance low c-SWaP optical gyroscopes to NASA for evaluation on the ISS. The program goal is the integration of these small and lightweight sensors into space subsystems, pico satellites, and space vehicles.
Other Government organizations: UAVs, UUVs and Unmanned Land Vehicles, Gimbal and turret stabilization, Emergency and firefighter vehicle navigation. Commercial applications: Vehicle navigation and safety devices (business and private vehicles), Surveying, Smart phones, and Computer games.","description":"In this program, we propose to develop a new photonic-integration platform that incorporates optical gain in resonant waveguide optical gyroscopes. This new photonic integration platform is based on our existing low-loss SiN/SiO2 PLC photonic integration technology and incorporates a doped Aluminum Oxide layer for gain. One key resonant waveguide optical gyro design constraint is the relationship between the waveguide length, which can increase the Sagnac effect, and waveguide loss, which decreases the gyro resolution. Freedom Photonics' low loss SiN PLC platform is clearly an adequate path forward for record-breaking Gyro performance. With introduction of gain into the PLC, new possibilities arise for enhanced sensitivity, simplified control electronics, and ultra compact and robust designs.","startYear":2015,"startMonth":6,"endYear":2015,"endMonth":12,"statusDescription":"Completed","principalInvestigators":[{"contactId":168612,"canUserEdit":false,"firstName":"Gordon","lastName":"Morrison","fullName":"Gordon Morrison","fullNameInverted":"Morrison, Gordon","primaryEmail":"Gordon@Freedomphotonics.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":133813,"canUserEdit":false,"firstName":"Edward","lastName":"Davis","fullName":"Edward P Davis","fullNameInverted":"Davis, Edward P","middleInitial":"P","primaryEmail":"edward.p.davis@nasa.gov","publicEmail":true,"nacontact":false},{"contactId":461333,"canUserEdit":false,"firstName":"Theresa","lastName":"Stanley","fullName":"Theresa M Stanley","fullNameInverted":"Stanley, Theresa 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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
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