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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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Integrated Reacting Fluid Dynamics and Predictive Materials Degradation Models for Propulsion System Conditions
SBC: CFD RESEARCH CORPORATION Topic: T1202Computational fluid dynamics (CFD) simulations are routinely used by NASA to optimize the design of propulsion systems. Current methods for CFD modeling rely on general materials properties to determine fluid structure interactions. This introduces uncertainty when modeling extreme conditions, where materials degrade and properties may change as a consequence. This also limits the use of CFD as a ...
STTR Phase I 2015 National Aeronautics and Space Administration -
Improved Forecasting of Solar Particle Events and their Effects on Space Electronics
SBC: CFD RESEARCH CORPORATION Topic: T602High-energy space radiation from Galactic Cosmic Rays and Solar Particle Events (SPEs) pose significant risks to equipment and astronaut health in NASA missions. In particular, energetic particles from SPEs associated with flares and coronal mass ejections (CMEs) constitute a highly dynamic and penetrating radiation environment that may adversely affect not only beyond-Low-Earth-Orbit missions, bu ...
STTR Phase I 2015 National Aeronautics and Space Administration -
Ultra Low Air and H2 Permeability Cryogenic Bladder Materials for Inflatable Habitats
SBC: NANOSONIC INC. Topic: T1203NanoSonic has recently developed a hydrogen (H2) dispenser hose to realize H2 as a safe, reliable, and cost competitive replacement for gasoline. NanoSonic's ultra-low glass transition temperature (Tg of -100 ?C) is expected to meet the service requirement of 25,550 fills/year (70 fills/day for 2 years) at a combined ultra-high pressure of 875-bar and very wide service temperature range of -50?C ...
STTR Phase I 2015 National Aeronautics and Space Administration -
Advanced Hybrid Stage
SBC: GLOYER-TAYLOR LABORATORIES INC Topic: T101The proposed technology builds off GTL's advanced solid ramjet fuel. The method uses additive manufacturing methods to produce an innovative new type of fuel grain that regresses quickly and has a high Isp and combustion efficiency. With this technology, the performance of a liquid rocket engine can be had with a hybrid rocket system. This technology allows for a simple, low cost, high performanc ...
STTR Phase I 2015 National Aeronautics and Space Administration -
Multi Domain Modeling for Space Systems
SBC: METAMORPH INC Topic: T1102A comprehensive model-based approach will be enabled for space systems design via the work started on Phase I of this project. The OpenMETA toolkit is a cyber-physical modeling tool for the design and virtual integration of complex systems, developed under the DARPA AVM Program. OpenMETA will be leveraged and extended to support NASA/JPL goals for multi-physics, multi-domain modeling, analysis, ...
STTR Phase I 2015 National Aeronautics and Space Administration -
High Temperature Multimode Harvester for Wireless Strain Applications
SBC: Prime Photonics, LC Topic: T301Monitoring of structural strain is a well-established method for assessing the fatigue life and operational loads of aerospace vessels, aircraft, bridges, and other load-bearing structures. Information from extensive instrumentation using 100's to 1000's of strain gages can be fed into a condition based maintenance (CBM) algorithm to improve structural health assessments, detect damage, and lowe ...
STTR Phase I 2015 National Aeronautics and Space Administration -
High Figure-of-Merit Macro-Structured Thermoelectric Materials
SBC: MICROXACT INC. Topic: T301Thermoelectric devices are critical to multiple NASA missions for power conversion with radioisotope sources. At present, commercially available TE devices typically offer limited heat-to-electricity conversion efficiencies, well below the fundamental thermodynamic limit, calling for the development of higher efficiency materials. The team of MicroXact Inc. and Virginia Tech is proposing to develo ...
STTR Phase I 2015 National Aeronautics and Space Administration -
Configurable, Multi-Beam, Doppler Ladar Based Precision Landing Sensor
SBC: FIBERTEK, INC. Topic: T901Fibertek proposes a configurable, multi-beam, 1.5 um Doppler Lidar sensor, enabled by high-speed non-mechanical beam steering (NMBS). NMBS uses state-of-the-art, high-speed liquid-crystal based components, to provide wide-angle (up to +/- 45 degree), large-aperture, optical beam steering, at speeds of up to 10 kHz. Furthermore, this is integrated into a very compact optical transmit/receive termin ...
STTR Phase I 2015 National Aeronautics and Space Administration -
Modified Acoustic Emission for Prognostic Health Monitoring
SBC: Prime Photonics, LC Topic: T1201A variety of nondestructive inspection (NDI) techniques are already available for detection of small defects within structures. These techniques, although useful, provide little insight in terms of the remaining useful life of components or structures. Furthermore, NDI techniques rely on statistical analyses of historical usage records and can often result in situations where maintenance schedul ...
STTR Phase I 2015 National Aeronautics and Space Administration -
Distributed, Passivity-Based, Aeroservoelastic Control (DPASC) of Structurally Efficient Aircraft in the Presence of Gusts
SBC: Tao Of Systems Integration Inc Topic: T401Control of extremely lightweight, long endurance aircraft poses a challenging aeroservoelastic (ASE) problem due to significantly increased flexibility, and aerodynamic, structural, and actuator nonlinearities. To obtain the benefits of increased aerostructural efficiency, the controller needs to trim at a specified optimal shape while minimizing structural fatigue from gust disturbances. Tao Syst ...
STTR Phase II 2015 National Aeronautics and Space Administration