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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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High Power High Thrust Ion Thruster (HPHTion): 50 CM Ion Thruster for Near-Earth Applications
SBC: Electrodynamic Applications Inc Topic: T301Advances in high power, photovoltaic technology has enabled the possibility of reasonably sized, high specific power, high power, solar arrays. New thin film solar arrays have demonstrated specific powers of over 4000 W/kg (exceeding the current SOA of ~130 W/kg). At high specific powers, power levels ranging from 50 to several hundred kW are feasible for communication satellites. Coupled with ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Innovative Solid State Lighting Replacements for Industrial and Test Facility Locations
SBC: Energy Focus, Inc. Topic: T1002The proposed innovation is the replacement of existing test stand and parking lot fixtures with current SSL LED technology. The replacement fixtures will reduce energy consumption, generate less heat and provide maintenance free operation for over 50,000 hours. An explosion-proof fixture is capable of containing an internal combustion event without allowing flames or hot gasses to escape to the s ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Time-Domain Terahertz Reflection Holograhic Tomography Nondestructive Evaluation System
SBC: TeraMetrix, LLC Topic: T701We propose to demonstrate key elements of feasibility for a single-sided time-domain terahertz reflection holographic tomographic imaging (TD-THz RHT) nondestructive evaluation (NDE) system which will provide high quality three dimensional images of the interior of complex aerospace composite structures. Time-domain terahertz imaging in the 0.1 to 3 THz spectral range is currently being used to c ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Reliable Autonomous Surface Mobility (RASM) in Support of Human Exploration
SBC: PROTOINNOVATIONS, LLC Topic: T102ProtoInnovations, LLC and Carnegie Mellon University have formed a partnership to commercially develop rover-autonomy technologies into Reliable Autonomous Surface Mobility (RASM). Our aim is to provide safe and reliable means for lunar rovers to travel at substantial speeds and operate in proximity to astronauts and other vehicles. Our unique partnership brings together state-of-art technologie ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Gaseous Helium Reclamation at Rocket Test Systems
SBC: Sierra Lobo, Inc. Topic: T1001The ability to restore large amounts of vented gaseous helium (GHe) at rocket test sites preserves the GHe and reduces operating cost. The used GHe is vented into the atmosphere, is non-recoverable, and costs NASA millions dollars per year. Helium, which is non-renewable and irreplaceable once released into the atmosphere, is continuously consumed by rocket test facilities at NASA centers such a ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Hybrid Integrated Photonics for Ultrahigh Throughput Optical Signal Processing
SBC: STRUCTURED MATERIALS INDUSTRIES, INC. Topic: T401Structured Materials Industries, Inc. and Cornell University propose to develop high speed integrated photonic switches and WDM for LIDAR applications. The team has recently shown that single mode silicon nitride (Si3N4) waveguides to have very low propagation losses. This material is an ideal candidate for the propagation and manipulation of optical signals at LIDAR wavelengths (1.06 μm). It is ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Next-Generation Ion Thruster Design Tool to Support Future Space Missions
SBC: TECH-X CORPORATION Topic: T301Computational tools that accurately predict the performance of electric propulsion devices are highly desirable by NASA and the broader electric propulsion community. Large investments in running the long duration test programs (> 20 kHrs) at NASA GRC can be reduced with computer models and allow more focus on exploring the NEXT ion thruster design for future space missions. The current state of e ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Scalable Gravity Offload System
SBC: ASTROBOTIC TECHNOLOGY INC Topic: T602The proposed innovation is a scalable gravity off-load system that enables controlled integrated testing of Surface System elements such as rovers, habitats, and space suits in planet-relevant gravity which addresses T6.02 in the direct solicitation of a gravity off-load system. Phase I delivers a nominal design in the form of a final report, Phase II builds this design and delivers hardware, and ...
STTR Phase I 2010 National Aeronautics and Space Administration -
An Automated High Aspect Ratio Mesher for Computational Fluid Dynamics
SBC: Ciespace Corporation Topic: T801Computational fluid dynamics (CFD) simulations are routinely used while designing, analyzing, and optimizing air- and spacecraft. An important component of CFD simulations is mesh generation, or discretization into polygonal or polyhedral cells, of the domain being analyzed. The overall computational cost and accuracy of simulations depend heavily on mesh quality the size, shape, and structur ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Advanced Unsteady Turbulent Combustion Simulation Capability for Space Propulsion Systems
SBC: STREAMLINE NUMERICS, INC. Topic: T901The innovation proposed here is a high performance, high fidelity simulation capability to enable accurate, fast and robust simulation of unsteady turbulent, reacting flows involving cryogenic propellants (such as LOX/LH2 and LOX/LCH4). The key features of this proposed capability are: (a) Hybrid RANS-LES (HRLES) methodology, and (b) flamelet modeling for turbulent combustion incorporated in a pr ...
STTR Phase I 2010 National Aeronautics and Space Administration