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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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Temporally and Spatially Resolved Spectrograph for 15-300 keV X-Rays
SBC: ALAMEDA APPLIED SCIENCES CORPORATION Topic: N/AN/A
SBIR Phase II 2000 Department of DefenseAir Force -
N/A
SBC: ALAMEDA APPLIED SCIENCES CORPORATION Topic: N/AN/A
SBIR Phase I 2000 Department of DefenseAir Force -
N/A
SBC: ALAMEDA APPLIED SCIENCES CORPORATION Topic: N/AN/A
SBIR Phase II 2000 Department of DefenseAir Force -
N/A
SBC: ACELLENT TECHNOLOGIES INC Topic: N/AN/A
SBIR Phase I 2000 Department of DefenseAir Force -
N/A
SBC: ACTA, LLC Topic: N/AN/A
SBIR Phase I 2000 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 -
N/A
SBC: Advanced Projects Research, Incorporated Topic: N/ANot Available As microelectronic circuits used in space applications become more and more complex with greater capabilities, they require more chips, more memory, and more room. This means increased size and weight which means increased launch costs. One technique tha
SBIR Phase I 2000 Department of DefenseAir Force -
N/A
SBC: Advanced Projects Research, Incorporated Topic: N/AN/A
SBIR Phase II 2000 Department of DefenseAir Force -
N/A
SBC: Advanced Projects Research, Incorporated Topic: N/AN/A
SBIR Phase I 2000 Department of DefenseAir Force