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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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Antistatic Thermal Control Coatings
SBC: Adherent Technologies, Inc. Topic: N/AElectrostatic discharge control is vital for the health of any spacecraft. Exposure to charged particles in a space enviroment can lead to large charge differences across the craft, that, if no mechanism for controlled discharge is present, can destroy mission critical equipment. The preferred way of ESD control is to use conducting thermal control coatings. These coatings combine the ability to r ...
SBIR Phase II 2002 National Aeronautics and Space Administration -
Antistatic Thermal Control Coatings
SBC: Adherent Technologies, Inc. Topic: N/AElectrostatic discharge control is vital for the health of any spacecraft. Exposure to charged particles in a space enviroment can lead to large charge differences across the craft, that, if no mechanism for controlled discharge is present, can destroy mission critical equipment. The preferred way of ESD control is to use conducting thermal control coatings. These coatings combine the ability to r ...
SBIR Phase I 2002 National Aeronautics and Space Administration -
Self-Deploying Foam Antenna Structures
SBC: Adherent Technologies, Inc. Topic: N/AInflatable or self-deployable systems offer the only practical way to achieve space deployed antennas with low mass at large aperture. In this Phase I program, open-celled rigid polyurethane foams were developed for use in self-deploying antenna structures. Advantages of such a system relative to current systems include high volumetric efficiency of packing, inherent restoring force, low (or no) o ...
STTR Phase I 2002 National Aeronautics and Space Administration -
Self-Deploying Foam Antenna Structures
SBC: Adherent Technologies, Inc. Topic: N/AInflatable or self-deployable systems offer the only practical way to achieve space deployed antennas with low mass at large aperture. In this Phase I program, open-celled rigid polyurethane foams were developed for use in self-deploying antenna structures. Advantages of such a system relative to current systems include high volumetric efficiency of packing, inherent restoring force, low (or no) o ...
STTR Phase II 2002 National Aeronautics and Space Administration -
Spacesuit Monitor
SBC: Adherent Technologies, Inc. Topic: N/AThe concentration of carbon dioxide in exhaled breath is 3.8%; a concentration of 2% causes deepened breathing, and 4% causes a marked increase in respiration. These higher concentrations of CO2 also cause drowsiness and can be unsafe. Therefore, it is desirable to monitor the concentration of CO2 in exhaled breath to guarantee the safety of an astronaut in the dangerous extravehicular environment ...
SBIR Phase I 2002 National Aeronautics and Space Administration -
SBIR/STTR Phase I: Low-bandwidth Long-distance Learning
SBC: Aics Inc Topic: N/AThis Small Business Innovation Research Phase I project investigates the opportunities inherent in long-distance learning alternatives fashioned around the telnet internet protocol. To date, virtually all long-distance learning trials have been designed to operate using the procedures of the world-wide web (HTTP, CGI, Java, etc.), but these web-based solutions have a number of obvious intrinsic p ...
SBIR Phase I 2002 National Science Foundation -
Low Cost Engine Test Stand for 500 lb Thrust Class Engines
SBC: AJT and Associates, Inc Topic: N/AAJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard test-stand interface, greatly reducing the time required to install and remove various engines. Thi ...
SBIR Phase I 2002 National Aeronautics and Space Administration -
Low Cost Engine Test Stand for 500 lb Thrust Class Engines
SBC: AJT and Associates, Inc Topic: N/AAJT proposes to develop a low-cost, engine test-stand system for small (500 pound) thrust engines using gaseous, liquid or cryogenic propellants. This test stand would incorporate automated propellant transfer and automated propellant line purge systems. The engines would be configured to a standard test-stand interface, greatly reducing the time required to install and remove various engines. Thi ...
SBIR Phase II 2002 National Aeronautics and Space Administration -
Magnetohydrodynamic Stable Reference (MSTAR)
SBC: A-TECH CORPORATION Topic: N/APlatforms for scientific instruments increasingly require attitude knowledge and optical instrument pointing at sub-arcsecond accuracy. No low-cost commercial system exists to provide this level of accuracy for guidance, navigation, and control (GNC) and precision instrument pointing. ATA proposes to introduce a small inexpensive inertial attitude reference system based upon magnetohydrodynamic (M ...
SBIR Phase I 2002 National Aeronautics and Space Administration -
Magnetohydrodynamic Stable Reference (MSTAR)
SBC: A-TECH CORPORATION Topic: N/APlatforms for scientific instruments increasingly require attitude knowledge and optical instrument pointing at sub-arcsecond accuracy. No low-cost commercial system exists to provide this level of accuracy for guidance, navigation, and control (GNC) and precision instrument pointing. ATA proposes to introduce a small inexpensive inertial attitude reference system based upon magnetohydrodynamic (M ...
SBIR Phase II 2002 National Aeronautics and Space Administration