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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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QMU in Integrated Spacecraft System Models
SBC: ACTA, LLC Topic: T5ACTA and Sandia National Laboratories propose to quantify and propagate substructure modeling uncertainty for reduced-order substructure models to higher levels of system assembly, thereby enabling predictive simulations of engineering designs with quantified margins and uncertainties for model-based flight qualification of complete spacecraft. A critical part of this process is the accurate mode ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization
SBC: AMERICAN GNC CORPORATION Topic: T1In providing an innovative solution to improving information technologies and health management systems, AGNC is proposing a significant technological achievement with the Advanced Structural Health Monitoring System for Comprehensive Real-Time Vehicle Characterization. During in-flight conditions, this system is able to not only provide the status of information such as regarding the flight envel ...
STTR Phase I 2010 National Aeronautics and Space Administration -
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 -
Biotemplated Nano-Structured Materials for Advanced Li-ion Batteries
SBC: CFX BATTERY, INC. Topic: T301NASA has identified a critical need for pioneering advances in battery technology to give high performance, low-weight, durable and long-life power sources for future missions. In this Phase I proposal, CFX Battery, Inc. and Georgia Institute of Technology propose the chemical conversion of micron-sized, nano-structured templates available from renewable resources into functional electrode materia ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Advanced Li/CFx Primary Batteries with Non-Flammable Electrolytes
SBC: CFX BATTERY, INC. Topic: T601NASA seeks to develop high specific energy primary batteries that are safe and capable of performing under a wide temperature range, for manned space missions. To meet this goal, CFX Battery Inc. proposes to develop, characterize, and establish technological feasibility of a new Li/SF-CFx based high capacity lithium primary battery that offers higher rate capability and enhanced safety than conven ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Highly Reliable Structural Health Monitoring of Smart Composite Vanes for Jet Engine
SBC: INTELLIGENT FIBER OPTIC SYSTEMS CORP Topic: T201Intelligent Fiber Optic Systems and Auburn University propose a Fiber Bragg Grating (FBG) integrated Structural Health Monitoring (SHM) sensor system capable of providing in-situ crack detection, location and quantification of damage, as well as validating structural models, using recent advances in non-contact, non-destructive dynamic testing of composite structures. The key innovation is an FBG- ...
STTR Phase I 2010 National Aeronautics and Space Administration -
Quantification of Uncertainties in Integrated Spacecraft System Models
SBC: M4 ENGINEERING, INC. Topic: T501The proposed effort is to investigate a novel uncertainty quantification (UQ) approach based on non-intrusive polynomial chaos (NIPC) for computationally efficient and accurate quantification of uncertainties in spacecraft system models within a multidisciplinary analysis and optimization (MAO) framework. The UQ approach will include the modeling of both inherent (probabilistic) and epistemic unc ...
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 -
Microchannel Thermo Catalytic Ignition for Advanced Mono- and Bipropellants
SBC: Plasma Processes, LLC Topic: T301Small and micro-spacecrafts require the efficient, micro-propulsion systems. Chemical micro-propulsion is best suited for use as primary thrust, orbital insertion and attitude control because of its high energy density. When grouped into arrays for larger thrust applications, micro-propulsion devices provide high propulsive flexibility or can be used as igniters. The proposed effort will focus ...
STTR Phase I 2010 National Aeronautics and Space Administration