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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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Missile/UAV Dispense Interference Modeling
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: A07029The innovation is that of using blast-based concepts for the hypersonic/endo dispense of an array of small hardened projectiles (SHAPs) from an interceptor missile. Hit-to-kill successes using this SHAP concept will be significantly enhanced from that of conventional, single warhead concepts, akin to the improved probability of hitting a fast moving object with buckshot in comparison to a single ...
SBIR Phase I 2008 Department of DefenseArmy -
IM Modeling/Simulation Tool for KEI Dynamic/Thermal Loads Associated with Stage Separation
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: MDA06041Intense dynamic and thermal loads will occur during stage-separation events that are of major concern from both operational and safety viewpoints. The insensitive-munitions (IM) stimuli and thermal/dynamic response associated with such events has received very little attention, yet this is of major concern for the KEI vehicle undergoing Stage 1 to Stage 2 separation. The KEI event is at lower alti ...
SBIR Phase II 2008 Department of DefenseMissile Defense Agency -
Transpiration Cooling Computational Fluid Dynamics Submodel
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: A08033This proposal entails the development of specialized CFD models which can analyze transpiration cooling processes in complex high-speed environments. This is of significant importance to the Army since “well-designed” transpiration concepts are needed on missile systems that can provide reductions in both heat transfer and skin friction, resulting in improvements in overall performance. The ...
SBIR Phase I 2008 Department of DefenseArmy -
Advanced Scramjet Engine/Vehicle Design
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: A08032This program entails designing a Mach 10, scramjet propelled missile system using advanced CFD and design-optimization tools. The CFD codes were validated using full-scale data sets obtained from tests performed in the LENS shock tunnel facility. They contain advanced turbulence and thermochemical models. A preliminary rocket boosted and scramjet propelled concept vehicle will be designed meeting ...
SBIR Phase I 2008 Department of DefenseArmy -
Maneuvering Target Phenomenology
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: MDA07021Propulsion systems may perform a variety of maneuvers during the ascent phase of flight that can impact the performance of an interceptor or other parts of an MDA system designed to perform threat detection, discrimination, and tracking. Our Phase I effort focuses on building on extending existing plume signature software. A main technical objective is to establish the various components and app ...
SBIR Phase I 2008 Department of DefenseMissile Defense Agency -
Computational Fluid Dynamics Modeling for Electrically Conducting Flows
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: A06018A unified comprehensive framework that incorporates Maxwell’s equations coupled with the 3D unsteady Navier-Stokes equations of fluid mechanics, is being developed utilizing an innovative Multi-Physics Simulation (MPS) Architecture, for conducting multi-disciplinary simulations. The MPS Architecture can be used for analysis of problems where the dominant physical mechanisms are strongly influenc ...
SBIR Phase II 2008 Department of DefenseArmy -
Missile/UAV Dispense Interference Modeling
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: A07029The innovation proposed is the development of a high-fidelity software tool to be used for the design of hypersonic UAV dispense and subsequent dispense and dispersion of small hardened projectiles (SHAPs) from the UAVs using blast-based concepts. Such dispersed kinetic energy concepts can be effective against maneuverable and depressed trajectory threats for which conventional interceptors would ...
SBIR Phase II 2008 Department of DefenseArmy -
Energetic Secondary Fuel Injection for Propulsion System Performance Improvement
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: N07082A joint analytical/experimental program to develop technologies to improve thermal output from combustors in propulsion systems while ensuring their stable operation is proposed. The program will exploit the use of energetic materials as secondary fuels to be injected suitably into the combustors to both increase their thermal output and ensure the mitigation of any instability that may arise in t ...
SBIR Phase II 2008 Department of DefenseNavy -
Improving Weapons Bay Acoustical Environments
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: AF071256The F-22A main weapons bay experiences severe acoustic loading when exposed to the freestream. The severity and attenuation of this loading is exacerbated by the flight envelope of the F-22A aircraft, as well as the requirement to carry and release “smart” weapons throughout this envelope. This extremely harsh environment can also impact components that are mounted within the bay itself, inclu ...
SBIR Phase II 2008 Department of DefenseAir Force -
Turbopump Cavitation Tools
SBC: COMBUSTION RESEARCH & FLOW TECHNOLOGY INC Topic: AF071204Next generation liquid rocket systems envision novel designs for turbopumps that can operate at high suction speeds (i.e. low inlet pressures), and can be throttled over a wide range of low, off-design flow conditions. This is an extremely demanding flow regime where performance loss and damage from cavitation instabilities can be catastrophic since they can generate large amplitude pressure fluc ...
SBIR Phase II 2008 Department of DefenseAir Force