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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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Natural Adjuvants to Enhance Efficacy of Viral Vaccines for Mariculture
SBC: ProFishent Inc Topic: 812Marine aquaculture production now exceeds 20 million metric tons annually (FAO 2010) but viral diseases are still a major threat to the expansion of sustainable mariculture systems (National Marine Fisheries Service 2007). Pathogenic viruses continue to devastate many fish and shellfish operations every year (ICES Mariculture Committee 2004, Lightner 2011). To date, vaccines against aquatic anim ...
SBIR Phase II 2011 Department of CommerceNational Oceanic and Atmospheric Administration -
GPU-Accelerated Sparse Matrix Solvers for Large-Scale Simulations
SBC: EM PHOTONICS INC Topic: S601At the heart of scientific computing and numerical analysis are linear algebra solvers. In scientific computing, the focus is on the partial differential equations (PDEs) that arise from computational fluid dynamics (CFD), climate modeling, astrophysics, and structural and heat analysis that cannot be solved analytically. Certain problem formulations lead to sparse matrices, in which the majority ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
On-Line Flutter Prediction Tool for Wind Tunnel Flutter Testing using Parameter Varying Estimation Methodology
SBC: ZONA TECHNOLOGY INC Topic: A204ZONA Technology, Inc. (ZONA) proposes to develop an on-line flutter prediction tool using the parameter varying estimation (PVE) methodology, called the PVE Toolbox, to ensure the flight safety during the flight flutter test and to prevent the damage to the wind tunnel hardware from the structural failure of the flutter model during wind tunnel flutter test. This tool can be applied to rapidly ide ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
Novel Active Combustion Control Concept for High-Frequency Modulation of Atomized Fuel Flow
SBC: JANSEN'S AIRCRAFT SYSTEMS CONTROLS, INC. Topic: A202This proposal by Jansen's Aircraft Systems Controls, Inc. presents an innovative solution for Active Combustion Control.Relative to the state of the art, this concept has the ability to provide frequency modulation (greater than 1000[Hz]) in combination with high amplitude modulation (in excess of 30% flow) and can be adapted to a large range of fuel injector sizes. Existing state-of-the-art ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
High Power Room Temperature Terahertz Local Oscillator
SBC: Desert Beam Technologies, LLC Topic: S104The motivation of the proposed SBIR is to develop, demonstrate and commercialize a compact, low-mass, high output power (1-10 milliwatt), tunable source of CW THz radiation operating at room temperature. The source will be useful both as a narrow band frequency stable sources for driving heterodyne receivers at key frequencies between 1 and 5 THz (1.4, 1.9, 2.7, 4.7 etc..) or for laboratory source ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
Low Mass Electromagnetic Plasmoid Thruster with Integrated PPU
SBC: MSNW LLC Topic: S304The Electromagnetic Plasmoid Thruster (EMPT) is a revolutionary electric propulsion thruster and power processing (PPU) system that will allow a dramatic decrease in system mass and increase in thrust efficiency over traditional 500-3000 W propulsion systems. The high specific power (>700 W/kg) and high efficiency of EMPT will enable a wide range of deep space missions such as Neptune, Pluto and O ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
RF Front End Based on MEMS Components for Miniaturized Digital EVA Radio
SBC: ALPHASENSE, INC. Topic: O104In this SBIR project, AlphaSense, Inc. and the Carnegie Mellon University propose to develop a RF receiver front end based on CMOS-MEMS components for miniaturized digital EVA radio applications. In Phase I, we have proven the feasibility of implementing a compact, low power and high performance S band receiver front end based on CMOS- MEMS components. Specifically, we conducted link budget analys ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
Integrated Sublimator Driven Coldplate for use in Active Thermal Control System
SBC: PARAGON SPACE DEVELOPMENT CORPORATION Topic: X205The original Sublimator Driven Coldplate (SDC) design sought to provide significant mass savings over a traditional pumped fluid loop by combining the functions of a cold plate and a sublimator and eliminating the fluid loop (Leimkuehler, et. al., "Design of a Sublimator Driven Coldplate Development Unit," 2008-01-2169). The target application was to provide heat rejection for the ascent module of ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
Contaminant Robust System for Oxygen Production from Lunar and Martian Resources
SBC: PARAGON SPACE DEVELOPMENT CORPORATION Topic: X301Extended duration missions to the Moon and Mars will require the use of In-situ resources to generate propellants and life support consumables. Many of the processes for in-situ resource utilization (ISRU) produce water, along with a variety of acid gases and other water soluble contaminants. Paragon proposes to develop membrane technology to separate water vapor from contaminants in the ISRU sy ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
Flight Dynamic Simulation with Nonlinear Aeroelastic Interaction using the ROM-ROM Procedure
SBC: ZONA TECHNOLOGY INC Topic: A207ZONA Technology, Inc. proposes to develop an integrated flight dynamics simulation capability with nonlinear aeroelastic interactions by combining a flight dynamics model and an add-on nonlinear aeroelastic solver in a Simulink environment. This nonlinear aeroelastic solver is generated by interacting a nonlinear structural Reduced Order Model (ROM) with a Neural-Network-based (NN-based) aerodyna ...
SBIR Phase II 2011 National Aeronautics and Space Administration