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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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UNIVERSAL END-EFFECTOR WITH TORQUE FEEDBACK FOR HAND VALVES
SBC: ADC Acquisition Co. dba Automated Dynamics Topic: N/AN/A
SBIR Phase I 1987 National Aeronautics and Space Administration -
SMART ANGLE ATTACK AND ANGLE OF SIDESLIP SENSOR
SBC: Engineering Development Lab Topic: N/AVIRTUALLY ALL FLIGHT VEHICLES REQUIRE THE ACCURATE MEASUREMENT OF ANGLE OF ATTACK (ALPHA); THOSE UNDER-GOING FLIGHT TESTING AND SOME COMMERCIAL AND MILITARY AIRCRAFT ALSO MAKE USE OF INFORMATION ON ANGLE OF SIDESLIP (BETA). EXISTING ANGLE MEASUREMENT METHODS HAVE LIMITATIONS THAT MAKE THE MEASUREMENT OF ALPHA AND BETA IMPOSSIBLE UNDER CERTAIN FLIGHT CONDITIONS. SOME OF THESE SENSORS HAVE POOR DURA ...
SBIR Phase I 1988 National Aeronautics and Space Administration -
INVESTIGATION OF WEIS-FOGH PRINCIPLE OF HIGH LIFT AS APPLIEDTO TURBOMACHINERY FLOWS
SBC: VIGYAN INC Topic: N/ATHE PROPOSED RESEARCH IS DIRECTED TOWARDS A DETAILED ANALYTICAL AND NUMERICAL STUDY OF THE UNSTEADY VORTEX MOTIONIN THE CLAP-FLING MOTION, OBSERVED BY WEIS-FOGY, WHICH COULDYIELD LIFT COEFFICIENTS OF UP TO EIGHT. THE APPLICATION OF THE CLAP-FLING MOTION ANALOGY TO A COMPRESSOR STAGE COULD, UNDER CERTAIN CIRCUMSTANCES, PREDICT A STRONG ROTOR-STATOR INTERACTION WHICH COULD YIELD AN IMPROVED STAGE PE ...
SBIR Phase I 1987 National Aeronautics and Space Administration -
ANALYSIS OF FLOWFIELDS AROUND HYPERVELOCITY VEHICLES IN LOW-TO-HIGH DENSITY FLIGHT REGIME
SBC: VIGYAN INC Topic: N/ATHE HYPERSONIC VEHICLES FLYING AT HIGH ALTITUDES OPERATE IN A FLOW REGIME WHERE THE NONCONTINUUM EFFECTS NEAR THE SURFACE AND FINITE SHOCK THICKNESS DUE TO LOW DENSITY MAKE THE CONVENTIONAL CONTINUUM TECHNIQUES GROSSLY INADEQUATE. CHEMICAL NONEQUILIBRIUM IS ALSO IMPORTANT UNDER THE LOW-DENSITY FLOW CONDITIONS. UNTIL RECENTLY NOT MUCH WORK HAS BEEN DONE TO EVALUATE DEFICIENCIES OF THE EXISTING CONT ...
SBIR Phase I 1987 National Aeronautics and Space Administration -
ZERO GRAVITY PHASE SEPARATION VIA ULTRASONIC COALESCENCE
SBC: Taylor S R & Assocs Topic: N/AN/A
SBIR Phase I 1988 National Aeronautics and Space Administration -
HYPERSONIC PROPULSION INLETS FOR NASP APPLICATIONS
SBC: Vra Inc Topic: N/AN/A
SBIR Phase I 1987 National Aeronautics and Space Administration -
30 GHZ REFLECTION MODE FET SOLID STATE POWER AMPLIFIER
SBC: Lnr Communications Inc. Topic: N/AN/A
SBIR Phase I 1988 National Aeronautics and Space Administration -
A MESOSCALE NUMERICAL WEATHER FORECAST SYSTEM FOR USE IN SHUTTLE OPERATIONS
SBC: MESOSCALE ENVIRONMENTAL SIMULATIONS AND OPERATIONS, INC Topic: N/ATHE PROPOSED INNOVATION SYNTHESIZES THREE HIGH TECHNOLOGY TOOLS IN AN EFFORT TO DEVELOP A RELIABLE NUMERICAL MESOSCALEWEATHER FORECAST SYSTEM FOR USE AT THE KENNEDY SPACE CENTER FOR SHUTTLE LAUNCH AND LANDING OPERATIONS. THESE TOOLS ARE:(1) AN ADVANCED MESOSCALE NUMERICAL WEATHER PREDICTION MODEL, I.E., THE MESOSCALE ATMOSPHERIC SIMULATION SYSTEM (MASS), (2) THE CRAY-2 SUPERCOMPUTER SYSTEM, AND (3 ...
SBIR Phase I 1987 National Aeronautics and Space Administration -
DEVELOP AN INHALATION SCREENING DOSE MONITOR FOR WORKERS AT NUCLEAR POWER PLANTS
SBC: Mikayola International Topic: N/AAN "INHALATION SCREENING DOSE COLLAR-STANCHION MONITOR" WITHEMBEDDED MINIATURE THIN-WALL GEIGER-MUELLER RADIATION DETECTORS EVALUATES THE THYROID GLAND FOR NANOCURIE ACTIVITYINVENTORY. THE PRIMARY TECHNICAL OBJECTIVE IS TO ESTABLISH THAT THE "COLLAR-STANCHION MONITOR" WILL BE CAPABLE OF DETECTING WITHIN 15 SECONDS AND WITH 2 SIGMA CONFIDENCE AN ACTIVITY INVENTORY OF 0.7 NANOCURIES OF I-131 DOSE EQ ...
SBIR Phase I 1987 Nuclear Regulatory Commission -
THREE-DIMENSIONAL EULER SOLVER
SBC: G M A F Inc Topic: N/ATHE COMPUTATIONAL TECHNIQUE FOR TWO-DIMENSIONAL, UNSTEADY FLOWS WHICH WE DEVELOPED (A COMBINATION OF THE LAMBDA-SCHEMEAND SHOCK-FITTING) HAS PRODUCED EXCELLENT RESULTS AND REQUIRES SUBSTANTIALLY LESS COMPUTATIONAL TIME THAN SHOCK-CAPTURING TECHNIQUES. IT IS PROPOSED TO EXTEND THE TECHNIQUE TO THREE-DIMENSIONAL FLOWS AND TO PROVIDE SEVERAL FEASIBILITY TESTS, INCLUDING SOME COMPLICATED SHOCK PATTERN ...
SBIR Phase I 1988 National Aeronautics and Space Administration
