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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.

  1. Practical CFD Models for Predicting Lean Blowout and Ignition in Gas Turbine Combustors

    SBC: CFD RESEARCH CORPORATION            Topic: N/A

    Current steady-state CFD combustion codes cannot predict transient combustion phenomena such as lean blowout (LBO) and ignition in gas turbine combustors. In this SBIR, we propose to develop an innovative analytical capability so that the combustordesigner can address operability issues. The key to predicting LBO/ignition is the use of time-accurate Unsteady Reynolds Averaged Navier Stokes (URAN ...

    SBIR Phase I 2003 Department of DefenseAir Force
  2. Fluidic System Optimization For Active Core Exhaust Control in High Bypass Ratio Turbofan Engines

    SBC: CFD RESEARCH CORPORATION            Topic: N/A

    Elimination of diverter valve sensitivity to core exhaust backpressure fluctuations will be critical to the success of future fluidic exhaust nozzle control technology enhancement programs. During Phase I extensive analysis of the pilot valve size,injection configuration and feed losses, as well as pulse format (frequency, pulse width, etc.) influences on main diverter valve operation, will be co ...

    SBIR Phase I 2003 Department of DefenseAir Force
  3. Axial Pintle Controlled Constant Volume Combustion Bipropellant Pulsed Rocket Motor

    SBC: CFD RESEARCH CORPORATION            Topic: N/A

    Idealized analysis has shown that, for the same propellant supply pressure, higher performance can be obtained in a constant-volume combustion device than the traditional constant pressure rocket. CFDRC proposes an effort consisting of multiple levels ofanalysis, followed by design and testing of a rocket engine prototype that will substantiate this claim. Recent relevant experience in advanced ...

    STTR Phase I 2003 Department of DefenseAir Force
  4. Multi-Resolution Tool for Rapid Evaluation of New Propulsion and Vehicle Systems

    SBC: CFD RESEARCH CORPORATION            Topic: N/A

    The project objective is to develop an integrated, hierarchical, multi-resolution tool for comprehensive prototyping and evaluation of new propulsion systems together with the launch vehicle systems. The overall vehicle system and its adjuncts will betreated as a collection of interacting software components coupled by a computational environment. Full and reduced scale component modules will al ...

    SBIR Phase I 2003 Department of DefenseAir Force
  5. High Quality E-beam Generation by Advanced Multipurpose Pseudospark Switch

    SBC: CFD RESEARCH CORPORATION            Topic: N/A

    CFD Research Corp. proposes the development of an Advanced Multipurpose Pseudospark Switch (AMPS) e-beam source capable of efficiently generating high average/peak current, bright electron beams. The improvement in e-beam quality (over a classicalpseudospark) stems from the inductive preionization of the hollow cathode chamber, prior to main gap breakdown. The proposed device features similaritie ...

    SBIR Phase I 2003 Department of DefenseAir Force
  6. PC Based Dynamic Real-Time Infrared Image Generation Capability

    SBC: CG2, Inc.            Topic: N/A

    Infrared image generation for IR sensor development and testing are currently large workstations costing several hundreds of thousands of dollars. Performance and image resolution is the key limiting factors of using PC hardware for this task. Usingdistributed processing, and intelligent algorithms, along with the forthcoming advances in PC graphics hardware; the next generation of real-time image ...

    SBIR Phase I 2003 Department of DefenseAir Force
  7. Creative Robots to Defeat Deeply Buried Targets

    SBC: IMAGINATION ENGINES, INC.            Topic: N/A

    Recent developments in the area of artificial neural networks have led to a totally new brand of machine intelligence that is capable of autonomously improvising and implementing cunning concepts and strategies. This revolutionary neural networktechnology, called the

    SBIR Phase I 2003 Department of DefenseAir Force
  8. Adaptive Artificial Intelligence for Next-Generation Conflict Simulation

    SBC: John Tiller Software, Inc            Topic: N/A

    This proposal is for the design and development of a challenging, adaptable, and extendible A/I system for use in state-of-the-art computer-based wargames. The development will result in a 3rd generation computer wargame based on modern air power conflictand the ability to apply the technology developed for this project in other wargames ranging from tactical ground-based warfare to naval conflic ...

    STTR Phase I 2003 Department of DefenseAir Force
  9. Innovative Applications of Plasma Discharge for Power and Propulsion Technology

    SBC: MEMS OPTICAL, INC.            Topic: N/A

    Traditional stationkeeping thrusters for satellites are low-efficient, complex, monopropellant or bipropellant chemical thrusters. The complexity and stored propellant of the thrusters result in satellites with higher dry weights, decreased payloadcapabilities, and thus higher incurred costs.A significant opportunity exists in the area of satellite stationkeeping for innovative propulsion systems ...

    SBIR Phase I 2003 Department of DefenseAir Force
  10. Variable Pressure High Speed Test Track

    SBC: MILTEC CORP.            Topic: N/A

    Miltec Missiles & Space Company and their subcontractor Secotec, Inc. propose to develop an innovative low cost ejector / diffuser system for economically producing a high vacuum in a very large chamber for use at Holloman AFB High Speed Test Track. Theunique and challenging requirement here is that this pressure vessel total length will most likely be thousands of feet and must be removable. The ...

    SBIR Phase I 2003 Department of DefenseAir Force
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