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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. Vortex Control for Low-Noise DEP Urban Aircraft

    SBC: Surfplasma, Inc.            Topic: T15

    Suppression of noise from aircraft is a vital NASA goal, especially important for the vision of Urban Air Mobility. Small urban aircraft may utilize Distributed Electric Propulsion along with advanced structural and electric motor/storage technologies to achieve the necessary flight capability. However, these aircraft utilize propellers or fans to achieve the necessary thrust, with attendant commu ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  2. 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
  3. Demonstration of Dual Mode Ionic Liquid Propulsion

    SBC: STREAMLINE AUTOMATION LLC            Topic: T2

    This program will design, fabricate, and test a dual mode propulsion system in a non-flight-weight configuration using a novel energetic, low-toxicity ionic liquid for both high thrust (conventional catalyst-based monopropulsion system) and low thrust (electrospray) engines. Non-Stoichiometric HydroxyEthyl Hydrazinium Nitrate (NSHEHN), developed under Army and NASA SBIR programs, will be used for ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  4. POC Blood Coagulopathy Monitor

    SBC: CFD RESEARCH CORPORATION            Topic: DHA19A001

    Traumatic injuries account for 30% of all life years lost in the US and is the leading cause of death for people under 46 years of age. Uncontrolled bleeding or hemorrhage constitute 30-40% of trauma related deaths and are considered to be a major cause o

    STTR Phase I 2019 Department of DefenseDefense Health Agency
  5. Multi-Band Software Defined Radio Sensor System

    SBC: Pegasense, LLC            Topic: T13

    This Multiband Software Defined Radio (SDR) sensor system proposal will demonstrate the ability to operate within multiple frequency bands and across multiple technology platforms in a single transceiver. The center frequencies and bandwidths chosen are representative of current demonstrated commercial or research devices and bands used: 400 MHz, 900 MHz, and 2.4 GHz ISM bands, with bandwidths of ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  6. Wireless Passive Nanoparticle based Intelligent Sensor System for Extreme Environments

    SBC: SENSATEK PROPULSION TECHNOLOGY, INC            Topic: T13

    Sensatek Propulsion Technology, Inc. proposes to demonstrate the feasibility of a wireless, passive, nanoparticle-based sensor system. The sensor in its current form can be used to measure real time temperatures and pressures wirelessly without the need of an external energy source. It should be noted that the same sensing principle can be used for strain monitoring as well. It comprises of a micr ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  7. 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
  8. Extensible Modeling to Create Knowledgebase for AM Processing of Alloy GrCop-84

    SBC: APPLIED OPTIMIZATION, INC.            Topic: T12

    The research objective of the proposed work is to demonstrate feasibility of utilizing extensible modeling to create an AM knowledgebase for copper alloy, GrCop-84, and utilize it to design an AM process for GrCop-84. The work plan has three tasks: (1) Utilize process modeling to demonstrate feasibility of predicting AM process parameters for alloy GrCop-84 for the powder bed and blown powder proc ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  9. Additive Manufacture of Refractory Metal Propulsion Components

    SBC: GEOPLASMA LLC            Topic: T9

    Niobium alloy (C-103) reaction control system (RCS) chambers have been used on numerous NASA programs. However at elevated temperatures, the strength of C-103 decreases significantly. Higher strength niobium alloys have been developed, but these alloys lack the formability of C-103. Recently, Additive Manufacture (AM) of niobium and C-103 has been demonstrated using powder bed electron beam me ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  10. Validated Engineering Tools for Thin-Ply Composites

    SBC: OPTERUS RESEARCH AND DEVELOPMENT, INC            Topic: T12

    Opterus Research and Development, Inc. proposes to develop and validate multi-scale thin-ply High Strain Composites (HSCs) constitutive modeling tools for incorporation into commercial finite element analysis codes. The constitutive models will capture the time-temperature-load-deformation viscoelastic characteristics common to HSCs as well as the yielding or permanent deformation associated with ...

    STTR Phase I 2018 National Aeronautics and Space Administration
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