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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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ADIABATIC WANKEL TYPE ROTARY ENGINES
SBC: ADIABATICS INC Topic: N/AN/A
SBIR Phase I 1984 National Aeronautics and Space Administration -
LOW THERMAL EXPANSION METAL COMPOSITE JOINTS FOR SPACE STRUCTURES
SBC: Material Concepts Inc Topic: N/AGRAPHITE/MAGNESIUM COMPOSITES ARE IDEAL FRO SPACE STRUCTURESBECAUSE OF THEIR LOW CTE, HIGH STIFFNESS AND STRENGTH, LOW DENSITY, AND LACK OF OUTGASSING OR MOISTURE ASORPTION. ALTHOUGH THESE MATERIALS ARE BEING FABRICATED INTO LONG STRAIGHT SECTIONS, NO METHOD HAS BEEN AVAILABLE TO JOIN THESE SECTIONS USING A SIMILAR MATERIAL TO FORM A COMPLETE STRUCTURE. RECENTLY DEVELOPED IS A NEW TECHNOLOGY WHICH ...
SBIR Phase II 1984 National Aeronautics and Space Administration -
ADVANCED ROTARY ENGINE
SBC: Material Concepts Inc Topic: N/ATHE ADVANCED ROTARY ENGINE HAS THE POTENTIAL FOR HIGH EFFICIENCY AND DURABILITY DUE TO ITS LOW NUMBER OF MOVABLE PARTS, COMPACTNESS, AND EXTREMELY HIGH HORSEPOWER-TO- WEIGHT RATIO. THIS PROJECT CAN ASSUME THAT AN AUTOMOTIVE VERSION OF THE ROTARY ENGINE CAN BE MODIFIED AND DEVELOPED FOR USE IN BUSINESS AIRCRAFT APPLICATIONS. THE APPROACH IS TO MODIFY AN ENGINE BY REPLACING ENGINE HOUSING MATERIALS ...
SBIR Phase II 1984 National Aeronautics and Space Administration -
LOW CTE FITTINGS
SBC: Material Concepts Inc Topic: N/ASATELLITES AND SPACE STRUCTURES UTILIZING GRAPHITE/METAL MATRIX COMPOSITES WILL REQUIRE HIGH MODULUS, LOW DENSITY THERMALLY STABLE JOINTS. ONE CANDIDATE MATERIAL IS CHOPPED (DISCONTINUOUS) GR/A1. THIS PROGRAM WILL INVESTIGATE THE FABRICATION CHARACTERISTICS AND MEASURE THE THERMAL AND MECHANICAL PROPERTIES OF CHOPPED GR/A1. CONSOLIDATION AND FORMING METHODS WILL BE EVALUATED.
SBIR Phase I 1984 National Aeronautics and Space Administration -
METALLIZED KEVLAR SPACE TETHER SYSTEM
SBC: Material Concepts Inc Topic: N/AN/A
SBIR Phase I 1984 National Aeronautics and Space Administration -
RAPID SOLIDIFICATION OF LOW DENSITY ALLOYS BY MELT OVERFLOW
SBC: Ribbon Technology Corpon Topic: N/AN/A
SBIR Phase I 1984 National Aeronautics and Space Administration -
AN ANIMAL DEVELOPMENT HABITAT FOR SPACE BIOLOGY
SBC: STAR ENTERPRISES, INC. Topic: N/AN/A
SBIR Phase I 1984 National Aeronautics and Space Administration -
MEASUREMENT OF REVERSING FLOW PRESSURE DROPS IN STIRLING ENGINE HEAT EXCHANGERS
SBC: Sunpower, Inc. Topic: N/AN/A
SBIR Phase I 1984 National Aeronautics and Space Administration