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Award Data

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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. Novel Focal Plane Array Photodetector Technology for use in Eye Safe Imaging LADAR Receivers

    SBC: SOLID STATE SCIENTIFIC CORPORATION            Topic: N/A

    Imaging LADAR systems are critical to autonomous guided munitions. The objective of this program is to demonstrate a solid-state, eye-safe, 3-D staring imaging LADAR receiver. This state-of-the-art focal plan array LADAR receiver will combine a 1.55micron photodetector and an internal gain photodetector with a 3-D imaging readout circuit using an innovative manufacturing process. The resulting ...

    SBIR Phase II 2001 Department of DefenseAir Force
  2. Space Qualified, Low Cost Compact Disk Data Storage/Retrieval System

    SBC: AIREX CORP.            Topic: N/A

    Recent advances in electromagnetic technology clearly lend themselves to application in space-based data storage/retrieval systems. Commercial data storage systems provide low cost, long-life operation and strong logic/control systems, but employmechanical bearings that limit their resistance to shock and life expectancy. A similar system ruggedized for space via integrated magnetic motor-bearing ...

    SBIR Phase II 2001 Department of DefenseAir Force
  3. A High-Capacity Turboalternator for Turbo-Brayton Cryocoolers

    SBC: CREARE LLC            Topic: N/A

    Future DoD cryogenic cooling applications include space missions with relatively large cooling demands. These include space-based lasers, orbital transfer vehicles requiring cooling of stored fuels, and space-based platforms using large arrays of infrareddetectors. Loads for these applications will range from several watts to tens of watts. Temperatures of interest are between 10 and 100 K. Cu ...

    SBIR Phase II 2001 Department of DefenseAir Force
  4. An Innovative Cargo Securement Mesh with Integral Lightweight, Low-Cost Tensioning Devices and Adaptable Control Systems

    SBC: CREARE LLC            Topic: N/A

    The goal of this project is development of an acoustic system for imaging buried objects and underground geological features like bedrock layers, underground stream channels, and fracture zones. Current technology for imaging these features relies on theuse of electromagnetic radiation and suffers from limited spatial resolution and limited penetration depth in areas of high soil conductivity. Dur ...

    SBIR Phase II 2001 Department of DefenseArmy
  5. Mitigation of Single Event Upset (SEU) by Virtual Redundancy in Design

    SBC: ALTERNATIVE SYSTEM CONCEPTS, INC.            Topic: N/A

    Mitigation of Single Event Upset (SEU) to electronic devices and components has traditionally been and expensive problem to overcome. Dramatic improvements in electronics technology have rendered many prior SEU solutions ineffective and have created theneed for more advanced and innovative design tools. One of the more promising SEU solutions has been triple modular redundancy (TMR), where each ...

    SBIR Phase II 2001 Department of DefenseMissile Defense Agency
  6. Fiber Optic Grating Depth Sensor for Towed Array Applications

    SBC: CREARE LLC            Topic: N/A

    This project is directed towards the refinement and demonstrationof a robust high-temperature nonskid coating that can withstandrepeated flight operations associated with the AV-8B Harrieraircraft on the decks of Wasp-class Amphibious Assault Ships(LHDs). The Fleet has filed a series of Quality DeficiencyReports, Hazardous Material Reports, and Casualty Reports, whichdocument nonskid failures rel ...

    SBIR Phase II 2001 Department of DefenseNavy
  7. Ultra-Compact Heat Exchangers for Space-Borne Cryocoolers

    SBC: CREARE LLC            Topic: N/A

    Low-temperature cryocooler systems need recuperative heat exchangers with extremely high-thermal effectiveness (0.997 or greater) to achieve cooling in the 10 K range. For space-borne cryocoolers for sensor cooling, these recuperators must also be compact, lightweight, and cause minimal pressure losses in the gas stream. To meet these challenging requirements, we propose to develop a radial flow h ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
  8. Aerospace Model Maker System

    SBC: SANDERS DESIGN INTERNATIONAL            Topic: N/A

    The proposed Sanders Aerospace ModelMaker (AMM) system provides an innovative rapid prototyping method of fabricating aerospace wind tunnel test models that dramatically increases instrumentation effectiveness with reduced complexity, cost and construction time. The AMM uses an in-situ layered deposition process to build ceramic test models that withstand high temperatures and have fully integrate ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
  9. Reliable, Efficient, Lightweight Cryocooler for ISRU

    SBC: CREARE LLC            Topic: N/A

    Future planetary exploration missions will require technology for In-Situ Resource Utilization (ISRU) to minimize launch mass, risk, and cost. We propose an innovative cryocooler for in-situ separation of gases and production of cryogens. Key applications will be production and storage of liquid oxygen needed as propellant oxidizer, liquid oxygen supply for EVA suits for Mars exploration, and cond ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
  10. A Fault-Tolerant Heat Exchanger for Manned Spacecraft

    SBC: CREARE LLC            Topic: N/A

    The specific proposed innovation is a compact, fluid-to-fluid heat exchanger that is fault tolerant because the working fluids cannot come into contact even if there are large internal leaks. Manned spacecraft typically use water-based, secondary coolant loops to isolate the crew from toxic or asphyxiating fluids (such as ammonia or freon) in the central thermal bus. The innovation is a fabricatio ...

    SBIR Phase II 2001 National Aeronautics and Space Administration
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