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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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A BIOLOGICAL APPROACH TO THE SYNTHESIS OF META-HYDROXY PHENYLACETYLENE FROM PHENYLACETYLENE
SBC: Bio-technical Resources, L.p. Topic: N/AACETYLENE-TERMINATED RESINS ARE ONE OF SEVERAL CANDIDATE POLYMERIC MATERIALS BEING DEVELOPED FOR POTENTIAL AEROSPACE APPLICATIONS. THE ACETYLENE-TERMINATED RESINS POSSESS PROPERTIES REQUIRED FOR THE PROPOSED APPLICATIONS SUCH AS TEMPERATURE, MOISTURE, AND SHEAR INSENSITIVITY. THE LIMITING FACTOR FOR THE COMMERCIAL MANUFACTURE OF THESE RESINS IN A COST-EFFECTIVE METHOD FOR THE SYNTHESIS OF AN ESSEN ...
SBIR Phase I 1987 Department of DefenseAir Force -
Accelerated Development of High-Performance Mo-Si-B-X Alloys via an Approach of Integrating Thermodynamic Modeling with Experimental Study
SBC: Computherm, LLC Topic: AF07T003The proposed study aims at accelerated development of Mo-Si-B-X (X=Ti, Zr, Hf, Re, Mn) alloys with an optimized balance of properties, via an approach of integrating thermodynamic modeling with experimental study. On the basis of the Mo-Si-B-X (X=Ti, Zr, Hf) database developed in Phase I, a thermodynamic database of the Mo-Si-B-O-X (X=Ti, Zr, Hf, Re, Mn) system will be developed using the Calp ...
STTR Phase II 2009 Department of DefenseAir Force -
Advanced Diagnostic for Performance and Combustion Characterization in Rotational Detonation Rocket Engine (RDRE)
SBC: Exo-Atmospheric Technologies LLC Topic: AF19AT011Rotating Detonation Rocket Engines (RDRE)are being developed to take advantage of the near instantaneous heat release potential of detonation waves versus conventional deflagration-based chemical reactions in combustion applications. However, the detonation product environment is extreme and current instrumentation to measure wall / surface conditions within the detonation chamber are lacking. The ...
STTR Phase I 2019 Department of DefenseAir Force -
Advanced Friction Stir Processing for Ultra-refined Microstructure Development of Aluminum 7XXX Series Alloys
SBC: FRICTION STIR LINK, INC. Topic: AF07T038Friction Stir Processing (FSP) has been demonstrated to generate refined microstructures, resulting in improved material properties. This has several areas of application. First, FSP can enhance the formability of the particular alloy of interest. This is especially important for the superplastic forming process, where the use of FSP can be used to create superplastic behavior at high strain r ...
STTR Phase I 2008 Department of DefenseAir Force -
Advanced High Mass Fraction Tactical Rocket Motor Case
SBC: FMW COMPOSITE SYSTEMS, INC. Topic: AF04199The maturation of Titanium Matrix Composite into an affordable material system with production experience on the F-16 opens up a wide series of opportunities for improved propulsion performance. This SBIR builds on the baseline TMC demonstrations being conducted by FMW and ATK and extends them to advanced systems. The use of configured residual stress states and enhanced Titanium matrix systems ...
SBIR Phase I 2004 Department of DefenseAir Force -
Advanced High Mass Fraction Tactical Rocket Motor Case
SBC: FMW COMPOSITE SYSTEMS, INC. Topic: AF04199The higher Mach number flight capability required in future missile systems has necessitated the development of advanced materials capable of surviving the increased thermal loads expected in these systems. Although previous research has indicated that titanium matrix composites (TMCs) are a potential solution to this problem, the high cost of these materials has severely hindered their considerat ...
SBIR Phase II 2005 Department of DefenseAir Force -
Advanced Instrumentation for Carbon-Carbon Structures in Hypersonic Environments
SBC: Exo-Atmospheric Technologies LLC Topic: AF171020An integrated measurement sensor for carbon-carbon (C-C) structures is needed for testing in arc-jet facilities to meet testing needs for future hypersonic flight systems. This work continues development on a measurement suite capable of surviving the long duration glide phase characteristic of hypersonic vehicles. A fast-response pressure sensor, an instrumented temperature measurement plug, and ...
SBIR Phase II 2019 Department of DefenseAir Force -
Advanced Microwave Electrothermal Thruster for Dual-Mode Water Rocket Propulsion (AMET-DMWRP)
SBC: Orbital Technologies Corporation Topic: AF081065ORBITEC proposes to develop the Advanced Microwave Electrothermal Thruster (AMET) for use as one of the primary thrusters in the Dual-Mode Water Rocket Propulsion system. The AMET uses an electrodeless microwave discharge to produce thrust from water vapor propellant, delivering specific impulse in excess of 800 seconds with a highly efficient process. Microwave energy is introduced to a reson ...
SBIR Phase I 2009 Department of DefenseAir Force -
Advanced Monopropellant Management Device
SBC: Exo-Atmospheric Technologies LLC Topic: AF181036Exo-Atmospheric Technologies, LLC (Exo-AT) will undertake the design and development of a propellant management device PMD) designed for the unique fluid property characteristics of AF-M315E monopropellant.Along with its experimental testing partner, Purdue University, Exo-AT will conduct a series of tests to measure fluid properties for AF-M315E.Exo-AT will use these fluid properties (surface ten ...
SBIR Phase I 2018 Department of DefenseAir Force -
Advanced Near-Net Shape Metallurgy of Liquid Rocket Engine Components
SBC: Orbital Technologies Corporation Topic: AF103215ABSTRACT: ORBITEC proposes to develop and demonstrate a family of Low-Cost Thrust Chambers (LCTC) for use in future NASA exploration systems. Substantial cost savings will be realized in the production of the LCTCs with ORBITEC"s innovative hybrid fabrication technique. Hybrid fabrication (HF) allows for the rapid casting of near-net shape metallic thruster components, including regeneratively- ...
SBIR Phase I 2011 Department of DefenseAir Force