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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. Power Balance Solver Enhanced by an Experimental Absorption Cross-Section Database

    SBC: Electro Magnetic Applications, Inc.            Topic: T5

    We propose the development of a user-friendly software tool for estimating the electric field distributions within spacecraft enclosures based on the Power Balance (PwB) method and enhanced by a database of experimentally determined Absorption Cross-Sections (ACS) of common equipment, components and cables.The software will be built around an already developed PwB solver that determines the statis ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  2. Energy and Velocity Analyzer for Distributions of Electric Rockets

    SBC: PLASMA CONTROLS, LLC            Topic: T2

    Plasma Controls, LLC (SBC) and Colorado State University (RI) will mature an energy and species plasma diagnostic for use with plasma thrusters. The combined Energy and Velocity Analyzer for Distributions of Electric Rockets, or the lsquo;E-VADERrsquo;, is needed especially for characterizing the plasma plume of Hall thrusters, where researchers desire to know ion energies and charged species frac ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  3. Hybrid Anode for Electrified Aircraft Propulsion

    SBC: CORNERSTONE RESEARCH GROUP INC            Topic: T15

    Electrified Aircraft Propulsion (EAP) research is part of NASA effort to improve aircraft fuel efficiency, emissions, and noise levels. New secondary battery chemistries are required to meet the 500 ndash; 700 Wh/kg cell level specific energy needs of UAM, all-electric helicopters and regional passenger aircraft. The cycle life, currently at asymp; 1500 ndash; 3000 cycles, also needs substantial i ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  4. Braided Thin-Ply Tapes

    SBC: OPTERUS RESEARCH AND DEVELOPMENT, INC            Topic: T12

    Opterus proposes to develop braided thin ply composite tapes. The tapes will be braided from ultra-thin spread-tow unidirectional carbon and glass ribbons and will enable a new source and form factor for thin-ply textiles. The resulting tapes will be especially useful for thin high strain composite space deployable structures where they will allow bias plies in long parts without requiring seams. ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  5. Concurrent High-Fidelity Measurements and Simulations for Advancing the Design of Rotating Detonation Engines

    SBC: SPECTRAL ENERGIES LLC            Topic: T2

    Rotating Detonation Engine (RDE) design is challenging due to the lack of in-depth understanding of many key mixing and combustion processes. The RDE flow field is a nonuniform mixture of fuel and oxidizer concentrations with strong injector effects, large turbulence effects, multiple shockwaves, and shear layers. These inhomogeneities can lead to significant combustion inefficiencies which have a ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  6. In-Situ Application of Multi-Layer Thermal Protection System

    SBC: CORNERSTONE RESEARCH GROUP INC            Topic: T12

    Cornerstone Research Group Inc. (CRG) proposes to advance the state-of-the-art in space vehicle Thermal Protection Systems (TPS) through in-situ application and curing of a proprietary new resin technology called MG Resin, a family of thermoset formulations. The resins are being explored with DARPA, MDA, NASA, and the Army for a range of applications including C/C hot structures, TPS, syntactic in ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  7. Provably Convergent Game-Theoretic Coordination for Space Vehicle Swarms

    SBC: ASTER LABS, INC.            Topic: T4

    This program will develop a communication-less solution to decentralized control and task coordination for multi-agent systems (MAS). Reducing the operational burden of MAS swarms on human operators will greatly improve the capability of spacecraft constellations and distant planetary explorations. The proposed solution would guide the MAS towards a cost minimized set of actions by performing grad ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  8. Cervical Spine Health Improvement Products

    SBC: SWITCHBOX INC            Topic: DHA18B001

    Most standard-of-care tools and techniques for evaluating neck disorders are subjective, unreliable, and do not provide actionable information for providers, payers, and organizations to deliver efficient and effective care. This lack of objective neck he

    STTR Phase I 2019 Department of DefenseDefense Health Agency
  9. Oxygen Production and Delivery on Demand

    SBC: GLOBAL RESEARCH & DEVELOPMENT INC            Topic: DHA17B005

    This proposal is in response to the Defense Health Agency 2017 Phase I SBIR topic 17B-005.The approach is the use of a membrane oxygen pump using newly developed nano-thickness membranes with all the layers less than 1 micron total.Nanometer thickness membranes enable more oxygen output per surface area at temperatures of 300-600 C than current state-of-the -art 600-800 C membranes that are 50-300 ...

    STTR Phase I 2018 Department of DefenseDefense Health Agency
  10. A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin

    SBC: REACTION SYSTEMS, INC.            Topic: T6

    Reducing the allowable concentration of carbon dioxide (CO2) in spacecraft is a critical need for NASA. The system now used on the International Space Station (ISS) is the carbon dioxide removal assembly (CDRA). While it has performed well on the ISS, managers have concluded that using the device to reach the new ppCO2 limit of 2.0 mm Hg is not practical and a new method is needed.In this projec ...

    STTR Phase I 2018 National Aeronautics and Space Administration
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