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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. Advanced Composites for Ammunition Protection and Crew Survivability

    SBC: Fiber Materials, Inc.            Topic: A03032

    Battlefield vehicles such as the Interim Armored Vehicle (IAV) and Future Combat Systems (FCS) carry high energy, large caliber munitions into combat. The munitions are stowed in a rack within the vehicle and are susceptible to burning, detonation, and explosion when impacted by spall fragments occurring when the vehicle wall is penetrated by small arms and medium caliber projectiles. A need exist ...

    SBIR Phase I 2004 Department of DefenseArmy
  2. Advanced Divert and Attitude Control Materials, Attitude Control System (ACS) Thruster Body Application

    SBC: Fiber Materials, Inc.            Topic: MDA03087

    Fiber Materials, Inc. (FMI), teamed with Aerojet, proposes to demonstrate a low cost material concept applicable to the SM-3 ACS. The material, a 4-dimensionally reinforced carbon-carbon containing silicon carbide to eliminate oxidation and erosion, will offer significant benefits in comparison to the refractory metals now in use such as rhenium, columbium, and molybdenum. Refractory and other m ...

    SBIR Phase II 2004 Department of DefenseMissile Defense Agency
  3. Advanced Divert and Attitude Control System Materials for Liquid/Gel DACS Systems

    SBC: Fiber Materials, Inc.            Topic: MDA03087

    Fiber Materials, Inc., teamed with Aerojet and Plasma Processes, Inc., will complete the design and development leading to fabrication and demonstration of a ceramic matrix composite thrust chamber and requisite joining technologies for an advanced liquid/gel divert and attitude control (LDACS) application. The proposed Phase II development program will utilize a non-eroding material based on carb ...

    SBIR Phase II 2004 Department of DefenseMissile Defense Agency
  4. Advanced High Mass Fraction Tactical Rocket Motor Case

    SBC: FMW COMPOSITE SYSTEMS, INC.            Topic: AF04199

    The 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
  5. Advanced Rocket Propulsion Technologies

    SBC: FMW COMPOSITE SYSTEMS, INC.            Topic: AF04199

    The future propulsion requirements of the USAF will require substantial performance improvements, especially stage mass fraction as defined by the Phase III IHPRPT goals. The development and transition to production of titanium matrix composites (TMC) offer the potential of significant mass fraction gains for liquid engines. This program proposes the substitution of TMC into the impeller, which ...

    SBIR Phase I 2004 Department of DefenseAir Force
  6. Airdroppable High Speed, Low Signature Craft

    SBC: OREGON IRON WORKS, INC.            Topic: N04044

    The Oregon Iron Works, Inc. Phase 1 proposal for N04-044 Air droppable High Speed, Low Signature Craft consists of two distinct parts, and includes the development of a Phase II proposal. Part 1 is a progressive application research plan to investigate implementation of the current state of the art critical technologies required for development of an air droppable, high speed, low signature, un ...

    SBIR Phase I 2004 Department of DefenseNavy
  7. Aspect-Oriented Secure Fuselet Runtime Environment

    SBC: ORIELLE, LLC            Topic: MDA04044

    We propose to develop a secure runtime environment for fuselet-based missile targeting and threat analysis built on a foundation of aspect-oriented secure web services. Aspect-oriented techniques enable the modularization of crosscutting concerns such as remote access, security, transactions, and monitoring. We will compose aspect-oriented instrumentation with distributed object technologies in a ...

    SBIR Phase I 2004 Department of DefenseMissile Defense Agency
  8. Bore Insulator Materials for a Naval Electromagnetic Launcher

    SBC: Fiber Materials, Inc.            Topic: N04045

    Electromagnetic rail launchers are being designed for future long range naval surface fire support. These projectile launchers operate due to the interaction between the magnetic field and current flow between parallel conductive rails. An electric current accelerates a projectile down the barrel at hypersonic velocities. A high strength insulator is required to separate the energized launcher rai ...

    SBIR Phase I 2004 Department of DefenseNavy
  9. Breatheable Ablator Concept for Extended Flight/Maneuvering Navy Strategic Reentry Bodies

    SBC: INTERMAT            Topic: N04151

    The proposed program will develop a breathable ablator concept for application to Navy extended flight or maneuverable reentry vehicles. The breathable ablator concept will consist of a high-density, carbon-carbon outer shell over a charring ablator. This material configuration provides a greater resistance to ablation over longer flight times, where conventional materials would typically burn t ...

    SBIR Phase I 2004 Department of DefenseNavy
  10. Carbon Foam Composite Tooling

    SBC: TOUCHSTONE RESEARCH LABORATORY, LTD.            Topic: MDA03049

    Touchstone Research Laboratory has developed a novel material, CFOAMr. The primary enabling carbon foam characteristic is that the Coefficient of Thermal Expansion (CTE) values are comparable to carbon fiber polymer matrix systems in manufacturing advanced composites. Other advantages of carbon foam-based tools are low mass, reduced energy, easy modifications, unmatched repair capabilities, and r ...

    SBIR Phase II 2004 Department of DefenseMissile Defense Agency
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