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Award Data
The Award database is continually updated throughout the year. As a result, data for FY22 is not expected to be complete until September, 2023.
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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Non-Polluting Solvent And System For Surface Cleaning
SBC: ENVIRONMENTAL TECHNOLOGY & EDUCATION CTR Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
High-Performance Environmentally Safe Refrigerant
SBC: ENVIRONMENTAL TECHNOLOGY & EDUCATION CTR Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
Micromachined Fiber Optic Accelerometers
SBC: Luna Innovations Incorporated Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
High Performance Sputtered Shape Memory Alloy Thin Film Actuators In Hybrid Multi Layers For Adaptive Space Structures
SBC: Luna Innovations Incorporated Topic: N/AN/A
SBIR Phase I 1997 National Aeronautics and Space Administration -
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 -
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 -
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 -
LAMINAR-TURBULENT TRANSITION PREDICTION OF REACTING FLOWS IN HYPERSONIC VEHICLES APPLICATION
SBC: High Technology Corporation Topic: N/AN/A
SBIR Phase I 1996 National Aeronautics and Space Administration