You are here

Award Data

For best search results, use the search terms first and then apply the filters
Reset

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. Synthesis of HAN and HEHN in a Continuous Mix Process

    SBC: Digital Solid State Propulsion, Inc            Topic: AF171061

    Production of hydroxylamine nitrate (HAN) and hydroxyethyl hydrazine nitrate (HEHN) is of great concern for the manufacture of AF-315E. Current stockpiles of heritage ingredients held by AFRL are being depleted and those manufacturers are no longer in exi

    SBIR Phase I 2017 Department of DefenseAir Force
  2. High Voltage (HV) Fireset Systems and Subsystem Component Level Designs

    SBC: HYPERION TECHNOLOGY GROUP INC            Topic: AF171089

    Current and future explosive munition weapon systems development relies heavily on explosives detonation performance characterization and computational hydro-code simulation research conducted by DoD and DoE research communities. This work in turn relies

    SBIR Phase I 2017 Department of DefenseAir Force
  3. Prediction and Measurement of the Soot Build-Up in Film-Cooled Rocket Engines

    SBC: SIERRA ENGINEERING, INC.            Topic: AF15AT21

    This Phase II STTR effort is focused on generating the data necessary to identify the phenomenology that produces carbon deposition within kerosene film cooled rocket engines.This data is essential to guide the model development and validation process.Program outputs will be both data and a physics-based model for carbon deposition.

    STTR Phase II 2017 Department of DefenseAir Force
  4. Precision ACS (PACS) for DACS Low Level ACS

    SBC: Digital Solid State Propulsion, Inc            Topic: MDA11025

    Our Precision Attitude Control System (PACS) delivers high precision attitude control for Kinetic Weapon (KW) long range target discrimination and acquisition. The PACS utilizes electrically-controlled solid propellant (ESP), an innovative propulsion technology that enables fast burn rate control, throttling, and extinguishment of thrusters, simply by controlling applied electrical current. This ...

    SBIR Phase II 2013 Department of DefenseMissile Defense Agency
  5. Computational Modeling of Coupled Acoustic and Combustion Phenomena Inherent to Gas Turbine Engines

    SBC: Flow Modeling and Simulation            Topic: AF131181

    ABSTRACT: Flow Modeling and Simulation, LLC (FMS), proposes to develop a computational software tool, herein designated AUG3D, that is intended to provide physics-based, multi-level, validated computational simulations of turbine engine component flow fields, particularly those associated with thrust augmentors, i.e., afterburners. This tool will be ideally suited for closely integrating physica ...

    SBIR Phase I 2013 Department of DefenseAir Force
  6. Safe Solid Rocket Motor Ignition Systems for Mil. Std. 1901A Compliance Using Electric Solid Propellants and Pyrogens

    SBC: Digital Solid State Propulsion, Inc            Topic: MDA08045

    In process for public release

    SBIR Phase II 2013 Department of DefenseMissile Defense Agency
  7. Precision ACS

    SBC: Digital Solid State Propulsion, Inc            Topic: MDA08045

    In process for public release

    SBIR Phase II 2013 Department of DefenseMissile Defense Agency
  8. Improved Thrust Termination Modeling for Solid Rocket Motors

    SBC: SIERRA ENGINEERING, INC.            Topic: MDA10022

    This effort addresses the need for a predictive model which characterizes the motor ejecta from thrust terminated and burn-to-depletion solid rocket motors. Two models will be developed: an engineering model that provides near term predictive capability and a high fidelity model which will provide guidance to improve the engineering models. The engineering model, developed under Phase I, will be ...

    SBIR Phase II 2013 Department of DefenseMissile Defense Agency
  9. Advanced Analysis and Design Tool for Scramjet Air-frame Propulsion Integration

    SBC: Flow Modeling and Simulation            Topic: AF112004

    ABSTRACT: The SCRAMSIM computer code will be able to perform analysis for engineering design, stemming from a low order Reynolds Average Navier-Stokes (RANS) to high order (4th or higher) LES using accurate subgrid scale models (SGS). It will also solve thermal non-equilibrium mechanisms, conjugated heat transfer, general finite-rate chemistry using several databases for hydrocarbon/hydrogen-air ...

    SBIR Phase II 2013 Department of DefenseAir Force
  10. Advanced Combustion Stability Analysis Tools for Ox-rich Preburners

    SBC: SIERRA ENGINEERING, INC.            Topic: AF083112

    The goal of this SBIR is the enhancement of the current state-of-the-art combustion instability analysis tools.  The planned enhancement is focused on capturing the effects of injection element distribution and the inclusion of substantial film cooling and diluent injection.  These characteristics are extremely important in the design of high-pressure oxygen rich staged combustion (ORSC) engines ...

    SBIR Phase I 2009 Department of DefenseAir Force
US Flag An Official Website of the United States Government