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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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METHODS FOR REDUCING PLASMA EFFECTS ON THE NASP
SBC: ACCURATE AUTOMATION CORPORATION Topic: N/AWE PROPOSE THE DEVELOPMENT OF AN INNOVATIVE NEUROCONTROLLER THAT GENERATES TRAJECTORIES WHICH REDUCE PLASMA EFFECTS ON THE COMMUNICATION SYSTEM OF THE NASP. WE WILL MODEL PLASMA SHEATH GENERATION AND INCORPORATE THIS MODEL INTO A GHAME FLIGHT SIMULATOR ON A SILICON GRAPHICS WORKSTATION. THIS MODEL WILL THEN BE USED IN THE DEVELOPMENT OF THE CONTROLLER AND SUITABLE ADAPTATION LAWS. COST FUNCTIONS W ...
SBIR Phase II 1993 Department of DefenseAir Force -
PARALLEL NEURAL NETWORK TOOLBOX FOR SUPERCOMPUTERS
SBC: ACCURATE AUTOMATION CORPORATION Topic: N/ATHIS PROPOSAL INVOLVES RESEARCH INTO A SUPERCOMPUTER-BASED ENVIRONMENT FOR RESEARCH INTO MASSIVELY PARALLEL NEURAL-NETWORK ALGORITHMS FOR LARGE SCALE, COMPUTATIONALLY INTENSE PROBLEMS. THIS ENVIRONMENT WILL HAVE APPLICATION TO AREAS SUCH AS IMAGE PROCESSING, PATTERN RECOGNITION, CONTROL SIGNAL PROCESSING, DATA COMPRESSION, AND FAULT DIAGNOSIS. ALL OF THESE ARE AREAS WHICH INVOLVE MASSIVE AMOUNTS O ...
SBIR Phase II 1993 Department of DefenseAir Force -
Ontogenic Neural Networks for Avionics Applications
SBC: ACCURATE AUTOMATION CORPORATION Topic: N/AThe study of neural networks which possess the capability to learn and grow with little or no supervision will be explored during this research effort. These networks exhibit ontogenic behavior and are termed ontogenic neural networks. This reasearch effort explores the use of hybrid neural network structures which are capable of self-organization, feature discovery and self generation in a compos ...
SBIR Phase I 1993 Department of DefenseAir Force -
Neural Network Methods for Preventing Unstarts
SBC: ACCURATE AUTOMATION CORPORATION Topic: N/AN/A
SBIR Phase I 1993 Department of DefenseAir Force -
Sensor Fusion in a Dynamic Model-Based System
SBC: ACCURATE AUTOMATION CORPORATION Topic: N/AN/A
SBIR Phase I 1993 Department of DefenseAir Force -
A Variable Thurst Detonation Wave Engine, DWE, for Mach 0 to 3 Applications
SBC: Advanced Projects Research, Incorporated Topic: N/AThis proposal describes a novel, high thrust density Detonation Wave Engine (DWE) applicable to the Mach range of 0 to 3. The geometry of this novel engine concept naturally provides for integration into a new Combined Cycle Engine with Ramjets. The concept is an intermittent combustion jet engine that harnesses travelling detonation waves to accomplish compression and chemical reaction. The goal ...
SBIR Phase I 1993 Department of DefenseAir Force -
A Variable Thrust Detonation Wave Engine DWE for Mach 0 to 3
SBC: Advanced Projects Research, Incorporated Topic: N/AAn innovative actively cooled structure concept is proposed which integrates proven cooling techniques and state-of-the-art fabrication methods to extend the maximum combustor wall temperature, thereby reducing cooling requirements and aircraft weight while improving engine performance. Specifically, CONvective and TRANspiration cooling (CONTRAN) are uniquely combined, relying on hydrogen coolant ...
SBIR Phase I 1993 Department of DefenseAir Force -
Hy-Scram: An Oblique Detonation Wave Hypervelocity Scramjet Engine
SBC: Advanced Projects Research, Incorporated Topic: N/AN/A
SBIR Phase I 1993 Department of DefenseAir Force -
Instrumentation for Non-Intrusive Water Droplet Size and Mass Flux Measurements Utilizing the Phase Doppler Method
SBC: Aerometrics Inc. Topic: N/AThere is a need for non-intrusive instrumentation to characterize the drop size distribution and volume flux in support of on-line engine/inlet icing tests. The ducts may vary from three to twelve feet in diameter with flow field speeds from Mach 0.2 to 0.5. The Phase Doppler technique offers the best potential for making these measurements non-intrusively and with sufficient accuracy to meet the ...
SBIR Phase I 1993 Department of DefenseAir Force -
Characterization of Simulated Weather Environments In Aerospace Ground Test Cells.
SBC: Aerometrics Inc. Topic: N/AN/A
SBIR Phase I 1993 Department of DefenseAir Force