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Award Data
The Award database is continually updated throughout the year. As a result, data for FY24 is not expected to be complete until March, 2025.
Download all SBIR.gov award data either with award abstracts (290MB)
or without award abstracts (65MB).
A data dictionary and additional information is located on the Data Resource Page. Files are refreshed monthly.
The SBIR.gov award data files now contain the required fields to calculate award timeliness for individual awards or for an agency or branch. Additional information on calculating award timeliness is available on the Data Resource Page.
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Advanced Epitaxial Lift-Off Quantum Dot Photovoltaic Devices
SBC: MICROLINK DEVICES INC Topic: T301We propose to develop a high-efficiency, triple-junction, epitaxial lift-off (ELO) solar cell by incorporating quantum dots (QDs) within the current-limiting subcell. We intend to leverage existing QD epitaxy processes developed by the Rochester Institute of Technology and combine this with MicroLink's expertise in multi-junction cell growth and ELO technology. We will employ QDs to enhance ...
STTR Phase I 2012 National Aeronautics and Space Administration -
Infrared Microspectrometer based on MEOMS Lamellar Grating Interferometer
SBC: EPIR TECHNOLOGIES INC Topic: T401Infrared spectroscopy is an invaluable detection and measurement tool intensively used in Earth Science, Solar Physics and Astrophysics experiments pursued from satellite platforms. The geometrical characteristics and sensitivity of satellite infrared spectroscopy systems is often determined or limited by their optical elements. Improvements in optical components allow one to reduce the mass and i ...
STTR Phase I 2012 National Aeronautics and Space Administration -
Advanced Flow Analysis Tools for Transient Solid Rocket Motor Simulations
SBC: Tetra Research Corporation Topic: T901The goals of reducing total cost and increasing reliability and safety of access to space continue to be top priorities for NASA. The most immediate propulsion launch challenge involves increasing lift weight from 70 to 130 metric tons by developing the heavy lift Space Launch System (SLS). Solid rocket motor analysis tools are needed to simulate ignition and propellant recession during the burn ...
STTR Phase II 2012 National Aeronautics and Space Administration -
High-Speed Electronically Tunable Multi Fiber-Optic Wavelength Filter based on Ultra-High-Resolution Super-Compact Grating on Silicon-Photonic Platfor
SBC: Optonet, Inc Topic: N12AT005The proposed project will undertake the research, design, and development of key concepts and technologies for a high-speed electronically tunable channel filter, based on monolithically integrated ultra-high-resolution super-compact grating (UHR-SCG) technology that has been developed in OptoNet. The grating will be realized on Silicon-Photonic Electronic-Photonic Integrated (EPIC) Platform that ...
STTR Phase I 2012 Department of DefenseNavy -
Affordable CMAS-Resistant Thermal Barrier Coatings
SBC: QUESTEK INNOVATIONS LLC Topic: N12AT019A notable failure mechanism in thermal barrier coatings (TBCs) is the attack by calcium-magnesium-alumino silicate (CMAS) deposits resulting from the ingestion of siliceous minerals with the intake of air. Existing TBC systems such as yittria partially stabilized zirconia (YSZ) are highly susceptible to CMAS infiltration. In this STTR program, QuesTek Innovations LLC, a leader in the field of comp ...
STTR Phase I 2012 Department of DefenseNavy -
Insert ear-probe assembly for high-quality otoacoustic-emission (OAE) measurements in adults
SBC: ETYMOTIC RESEARCH, INC. Topic: N10AT032Current otoacostic emission probes used diagnostic evaluation middle and inner ear components of hearing are not capable of producing well-calibrated and high-quality acoustic stimuli that cover the entire frequency range of human hearing and are thus unsuited for rapid evaluation of the range of inner ear damage from ototoxic drugs, noise and the normal process of aging. The accuracy of stimulus ...
STTR Phase II 2012 Department of DefenseNavy -
Advanced Materials for the Design of Lightweight JP5/JP8/DS2 Fueled Engines for Unmanned Aerial Vehicles (UAVs)
SBC: Innovative Design & Research Inc. Topic: N10AT001The XS-Air engine should provide the highest power density with both diesel and gasoline piston engines. This would be especially true in smaller engines in where turbos or blowers are impractical. The XS-Air engine can solve the aviation industry problem of the potential phasing out Av-gas. The spark ignition XS-Air engine should be able to burn pump gas and still generate extreme power densities ...
STTR Phase II 2012 Department of DefenseNavy -
Large-Area, UV-Optimized, Back-Illuminated Silicon Photomultiplier Arrays
SBC: VOXTEL, INC. Topic: S105Large-area (3m2), UV-sensitive focal plane arrays are needed for observation of air showers from ultra-high energy cosmic rays (JEM-EUSO) as well as for visible-wavelength spectrographic and photometric instruments planned for future telescopes (OWL). Existing photocathode-based technologies for visible and UV instruments lack sensitivity, are bulky, and have limited reliability. Solid-state silic ...
SBIR Phase II 2012 National Aeronautics and Space Administration -
The Conductive Thermal Control Material Systems for Space Applications
SBC: APPLIED MATERIAL SYSTEMS ENGINEERING, INC. Topic: S302This Phase II proposal is submitted to further develop and Validate materials and process engineering of the space environment stable, multifunctional conductive thermal control material system (TCMS) that can be applied to space hardware and can enables the hardware to carry higher leakage current through engineering the high electrical conductivity. An innovative space environmental stable TCMS ...
SBIR Phase II 2012 National Aeronautics and Space Administration -
Reservoir Cathode for Electric Space Propulsion
SBC: E BEAM INC Topic: X204We propose a hollow reservoir cathode to improve performance in ion and Hall thrusters. We will adapt our existing reservoir cathode technology to this purpose. Reservoir cathodes are the only emission sources that are capable of supplying the necessary current density (>5.0 A/cm2) and life (>100,000 hours) for next generation high-power thrusters. More powerful thrusters are needed for interpl ...
SBIR Phase II 2012 National Aeronautics and Space Administration