You are here
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.
-
SMART MATERIAL PRODUCTS FOR COMMUNICATION, SENSING AND ACTUATION
SBC: LUNA INNOVATIONS INCORPORATED Topic: N/AN/A
SBIR Phase I 1996 National Aeronautics and Space Administration -
Lidar Systems For Atmospheric Measurements
SBC: FIBERTEK, INC. Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
TUNABLE SOLID-STATE UV FREQUENCY CONVERTER FOR OZONE DIAL INSTRUMENTATION
SBC: FIBERTEK, INC. Topic: N/AN/A
SBIR Phase I 1996 National Aeronautics and Space Administration -
NUMERICAL MODELING OF FULLY VISCOUS ROCKET PLUME FLOWS
SBC: Gt-devices Inc Topic: N/ATHE PLUME PRODUCED BY THE GAS FLOW THROUGH THE NOZZLE OF A ROCKET ENGINE OR SYSTEM VENT ON A SPACECRAFT CAN CONTAMINATETHE SPACECRAFT, ITS SENSORS AND OTHER NEARBY APPARATUS. ANALYTIC METHODS FAIL FOR DENSE OR COOL EXHAUST GAS, WHICH EXHIBITS VISCOUS BOUNDARY LAYER FLOW, AND NUMERIC SOLUTIONS FOR THE NOZZLE CORE FLOW ARE THEN PATCHED TO THOSE FOR THE BOUNDARY LAYER FLOW. THE RESULTING CONTINUUM SO ...
SBIR Phase I 1988 National Aeronautics and Space Administration -
Transistion Control in Corner Flow of a Supersonic Square Nozzle
SBC: High Technology Corporation Topic: N/A"Quiet" (low-disturbance) wind tunnels, needed for transitionresearch, require cleverly designed nozzle contours forstabilization or delay of dominant instabilities in supersonicnozzle wall boundary layers. However, if a nozzle of squarecross-section
SBIR Phase I 1994 National Aeronautics and Space Administration -
Drag-Prediction Algorithms for Navier-Stokes Solutions over Single- and Multi-Element Airfoils
SBC: High Technology Corporation Topic: N/AAccurate prediction of the aerodynamic lift and drag is acritical requirement in the development process of an aircraft.Presently, computational methods based on numerical solution ofthe Reynolds-averaged Navier-Stokes (N-S) equations are beingapplie
SBIR Phase I 1994 National Aeronautics and Space Administration -
A Novel Computational Tool For Hypersonic Transition Prediction
SBC: High Technology Corporation Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
HYBRID LAMINAR FLOW CONTROL TECHNIQUE FOR ENGINE NACELLES
SBC: High Technology Corporation Topic: N/AN/A
SBIR Phase I 1996 National Aeronautics and Space Administration -
A PROGRAMMING ENVIRONMENT FOR THE DEVELOPMENT OF LARGE SCIENTIFIC SYSTEMS ON A DISTRIBUTED COMPUTING NETWORK
SBC: High Technology Corporation Topic: N/AN/A
SBIR Phase I 1996 National Aeronautics and Space Administration -
Active Suppression of Resonance Interactions between Shear-Layers and Cavities
SBC: High Technology Corporation Topic: N/AN/A
SBIR Phase I 1994 National Aeronautics and Space Administration