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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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MULTIPLE PREHENSION MANIPULATOR
SBC: Robo-tech Systems Topic: N/ATHE NEED FOR ADVANCED END EFFECTORS IN SATELLITE SERVICING AND MAINTAINANCE HAS EMPHASIZED THE MANY TECHNICAL CHALLENGES IN END EFFECTOR DESIGN. ADVANCED SENSORS, COMPUTER CONTROLS AND ARTIFICIAL INTELLIGENCE HAVE RECENTLY OPENED NEW DOORS TO THE TRADITIONAL PROBLEMS OF SLIP, GRIP WITHOUT CRUSH AND PREHENSILE PATTERN RECOGNITION. THIS PROGRAM WILL USE COMPUTER SIMULATION TO DEVELOP KINEMATICS FOR ...
SBIR Phase I 1985 National Aeronautics and Space Administration -
Affordable Resins for High-Performance, Ablative Thermal Protection Systems
SBC: CORNERSTONE RESEARCH GROUP INC Topic: H701Cornerstone Research Group Inc. (CRG) proposes to advance fundamental material development of a high-temperature resistant, multifunctional polymer system conceived and demonstrated previously by CRG, which will provide NASA with an innovative, low-cost material for thermal protection systems. The proposed material technology results in a polymer system that transitions from a thermoplastic at tem ...
SBIR Phase I 2014 National Aeronautics and Space Administration -
Integration of Complex Geometry, 3D Woven Preforms via Innovative Stitching Technique
SBC: T.E.A.M., INC. Topic: H701Thick, 3D woven carbon/phenolic composites offer potential improvement over legacy thermal protection systems (TPS) for re-entry vehicle heat shield applications. However due to the scale and complexity of typical re-entry vehicle structures, it is likely that multiple 3D woven panels would need to laid up to create the overall heat shield, creating a potential weak spots at the panel joints. ...
SBIR Phase I 2014 National Aeronautics and Space Administration -
Domain Specific Language for Geant4 Parallelization for Space-Based Applications
SBC: RNET TECHNOLOGIES INC Topic: S501A major limiting factor in HPC growth is the requirement to parallelize codes to leverage emerging architectures, especially as single core performance has plateaued and architectures like short vector units (e.g., AVX), Intel Xeon Phi, and GPUs are embraced by hardware manufactures. The proposed SIMD/SIMT vectorization tools for emerging accelerator-based compute architectures will impact a world ...
SBIR Phase I 2014 National Aeronautics and Space Administration -
Physics-Based Selection of SLM Process Parameters to Mitigate Defects and to Control Deposit Microstructure
SBC: APPLIED OPTIMIZATION, INC. Topic: T1204The research objectives of this proposal are to: (1) To adapt the thermal-fluid science procedures for the prediction of weld defects to the prediction and control of surface defects and melt pool instability during the deposition of single tracks in SLM and to control the as-deposited microstructure. (2) Utilize physics-based analysis to predict variability caused in the individual SLM track cros ...
STTR Phase I 2014 National Aeronautics and Space Administration -
Fine-Filament Magnesium Diboride Superconductor Wire for Turboelectric Propulsion Systems
SBC: HYPER TECH RESEARCH INC Topic: A303This SBIR Phase II proposal overcomes technology barriers for developing highly efficient all electric aircraft systems for the future, with limited impact to the environment. Turboelectric propulsion for aircraft applications is envisioned, and cryogenic and superconducting components are sought. In particular, low AC loss superconducting wires for the stator windings and superconducting wires wi ...
SBIR Phase II 2014 National Aeronautics and Space Administration -
Improved Attachment Design for Ceramic Turbine Blades Via Hybrid Concepts
SBC: N&R ENGNERING MGT SUPPORT SVCS Topic: A307This proposal presents a hybrid metal-CMC turbine blade. A SiC/SiC CMC airfoil section will be bonded to a single crystal superalloy root section in order to mitigate risks associated with an all-CMC blade inserted in a superalloy disk. This allows current blade attachment technology (SX blade with a dovetail attachment to a slotted Ni disk) to be used with a ceramic airfoil. The bond between ...
SBIR Phase I 2014 National Aeronautics and Space Administration -
Microfluidic System for CO2 Reduction to Hydrocarbons in Microgravity
SBC: Faraday Technology, Inc. Topic: H101In the combined Phase I and Phase II programs Faraday and our MIT collaborators will demonstrate the feasibility of low-cost fabrication of high-efficiency, microchannel-plate reactors for the electrocatalytic reduction of CO2 to CH4. The proposed concept is founded on FARADAYIC® Through-Mask Etching of metallic (e.g., stainless steel and titanium) substrates to form suitable microchannel electr ...
SBIR Phase I 2014 National Aeronautics and Space Administration -
UAS Power Amplifier for Extended Range of Non-Payload Communication Devices (UPEND)
SBC: Nu Waves Ltd. Topic: A201The integration of Unmanned Aircraft Systems (UAS) into the National Airspace System (NAS) requires a robust, reliable communication link between the Unmanned Aerial Vehicle (UAV) and its operators. Constant communication is a necessity. New and innovative approaches are needed to provide high-bandwidth Control and Non-Payload Communications (CNPC). To enable the CNPC system and increase the util ...
SBIR Phase I 2014 National Aeronautics and Space Administration -
Compact Kinetic Mechanisms for Petroleum-Derived and Alternative Aviation Fuels
SBC: SPECTRAL ENERGIES LLC Topic: A303To be useful for computational combustor design and analysis using tools like the National Combustion Code (NCC), low-dimensional chemical kinetic mechanisms for modeling of real fuel combustion chemistry must be sufficiently compact so that they can be utilized in multi-dimensional, multi-physics, reacting computational fluid dynamics (CFD) simulations. Despite advances in CFD-appropriate kinetic ...
SBIR Phase I 2014 National Aeronautics and Space Administration