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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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Advanced Aerodynamic Analysis For Propulsion Airframe Integration
SBC: RESEARCH IN FLIGHT LLC Topic: A105Research in Flight is proposing to develop a fundamentally new, lower order, high fidelity solution approach for the aerodynamic analysis required for engine integration studies. This new approach is based on a new tool known as Flightstream. Flightstream is a surface vorticity based solver which uses an unstructured surface geometry, and a correlation for skin friction which is based on the sur ...
SBIR Phase I 2015 National Aeronautics and Space Administration -
Advanced Crew Escape System Simulation Tool for Future Launch Vehicles
SBC: CFD RESEARCH CORPORATION Topic: N/AA computational technique that utilizes an innovative tightly coupled combination of CFD, 6-DoF and blast wave simulation methods is proposed for the analysis of crew escape systems for future launch vehicles. An existing high-fidelity simulation program, well validated for military crew escape systems, will be leveraged to meet the challenges of simulating escape system operation for launch abort ...
SBIR Phase I 2003 National Aeronautics and Space Administration -
Advanced Zirconium Carbide Tie-Tubes for NTP
SBC: Plasma Processes, LLC Topic: H202Nuclear Thermal Propulsion (NTP) has been identified as a critical technology needed for human missions to Mars due to its increased specific impulse (Isp) as compared to traditional chemical propulsion systems. To achieve this high Isp, NTP reactors must operate at extremely high temperatures (i.e., >2400K) for long periods of time. However, many of the best materials for some reactor component ...
SBIR Phase I 2015 National Aeronautics and Space Administration -
A Hybrid Pyrolysis/Incineration System for Solid Waste Resource Recovery
SBC: ADVANCED FUEL RESEARCH, INC. Topic: N/ABoth pyrolysis and incineration steps have been considered as the key solid waste processing step for a Controlled Ecological Life Support System (CELSS). Pyrolysis is more amenable to handling mixed solid waste streams in a microgravity environment, but produces a more complex product stream. Incineration produces a simpler product stream, but the incineration of mixed solids is a complex unit op ...
SBIR Phase I 2003 National Aeronautics and Space Administration -
A Multi-Wavelength Seed Derived Laser for In-Situ Validation of Airborne Remote Sensing Instruments
SBC: ADVR, INC. Topic: S107This Phase I SBIR will establish the feasibility of developing a collinear three wavelength source for an in-situ, 1800, back scatter nephelometer. The three wavelength source is being developed to facilitate on-board validation measurements of airborne remote backscatter lidar. Currently, commercial nephelometers utilized for in-situ validation measurements employ wavelengths that are both not ...
SBIR Phase I 2015 National Aeronautics and Space Administration -
A New Methodology for Calculating Launch Vehicle Ascent Loads
SBC: Dynamic Concepts, Inc. Topic: N/ADetermining an effective structural design of a launch vehicle is critical to both mission success and crew safety. In order to evaluate the adequacy of a launch vehicle?s structural design, the ascent loads experienced by the vehicle must be determined. Computation of the ascent loads is a complex, multi-disciplined undertaking that involves an assessment of both natural and induced environments. ...
SBIR Phase I 2003 National Aeronautics and Space Administration -
Artificial Neural Net Chemistry Module for Large Eddy Simulations
SBC: CFD RESEARCH CORPORATION Topic: N/ACombustion Large Eddy Simulation (LES) is a vastly improved method of modeling turbulent-combustion in gas turbine combustors, and will provide improved emissions/instability prediction capability of UEET combustors. It is widely recognized that one of the best subgrid turbulence-combustion models is the Linear Eddy Mixing (LEM) model with multi-step reactions. However, this model is not commonly ...
SBIR Phase I 2003 National Aeronautics and Space Administration -
Carbon-Supported Amine Sorbent Monoliths for Carbon Dioxide Removal
SBC: ADVANCED FUEL RESEARCH, INC. Topic: N/AThe NASA objective of expanding the human experience into the far reaches of space will require the development of regenerable life support systems. On-board carbon dioxide (CO2) removal units play a key role in such systems ensuring high quality cabin air for crew members. Similar but more compact units are needed for extravehicular activities (space suit). The overall objective is to develop a C ...
SBIR Phase I 2003 National Aeronautics and Space Administration -
Cascaded Injection Locked Diode Laser Transmitter For Lidar Measurements
SBC: ADVR, INC. Topic: N/AA lidar laser transmitter useful for profiling of clouds, aerosols, and differential absorption measurements of atmospheric trace constituents such as carbon dioxide, water vapor, and ozone is proposed. The proposed laser transmitter is based on a master tunable external cavity diode laser (ECDL) used to injection lock a series of free running laser diodes (FRLD's). The FRDL's amplify the injected ...
STTR Phase I 2003 National Aeronautics and Space Administration -
Compact, Rugged and Low-Cost Atmospheric Ozone DIAL Transmitter
SBC: Bridger Photonics, Inc. Topic: S101Bridger Photonics Inc. (Bridger) proposes developing the most efficient, compact, rugged, low-power consumption and cost-effective UV ozone differential absorption lidar (DIAL) transmitter available. Bridger will demonstrate pulse energies above 0.5 mJ with a goal of 1 mJ/pulse with a pulse repetition frequency of 1 kHz. The proposed transmitter will enable widespread deployment of ozone DIAL s ...
SBIR Phase I 2015 National Aeronautics and Space Administration