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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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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 -
GaN Bulk Growth and Epitaxy from Ca-Ga-N Solutions
SBC: The IIIAN Company, LLC Topic: O107The innovations proposed here are Ka-band (38 GHz) group III-nitride power FETs and the dislocation density reducing epitaxial growth methods (LPE) needed for their optimal performance and reliability.Ka-band power transistors with>60% Power Added Efficiency (PAE) are not commercially available. The primary limitations to their manufacture are lack of mature process technology at major GaN foundri ...
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 -
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 -
High Power Narrow Linewidth 1.26 Micron Ho-Doped Fiber Amplifier
SBC: N.P. PHOTONICS, INC. Topic: S101This proposal is for the development of an innovative, high power, and extremely reliable 1.26-micron Ho-doped fluoride fiber amplifier. The proposed fiber amplifier consists of a Ho-doped fluoride fiber pre-amplifier and power amplifier. Laser at 1187 nm will be used as a resonant pump laser source for Ho3+-doped fiber laser. High gain per unit length at 1.2 micron can be achieved in Ho-doped f ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
Tunable Narrow Linewidth, Low Noise 2.05 Micron Single Frequency Seeder Laser
SBC: N.P. PHOTONICS, INC. Topic: S101We propose an all-fiber based 2.05-micron single frequency, narrow linewidth seeder laser with 10 nm tuning range and 5GHz frequency modulation for next generation LIDAR system. Highly Tm-doped fiber laser is used as a resonant pump source in order to reduce the phase noise and laser linewidth. An environment insensitive package will be used to minimize the laser phase noise and linewidth. Ho3+- ...
SBIR Phase II 2011 National Aeronautics and Space Administration -
Verification and Validation of an Innovative Inflatable Structure
SBC: PARAGON SPACE DEVELOPMENT CORPORATION Topic: X402An inflatable habitat is a pressure vessel with flexible shell. Notable features such as low weight, large inflated operational volume, and small pre-deployment volume offer significant advantages over traditional rigid metallic and composite habitat structures. Conventional designs suffer from indeterminacy of load sharing between meridional and circumferential members as well as the internally r ...
SBIR Phase II 2011 National Aeronautics and Space Administration