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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

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.

  1. Efficient cFS-based On-board Lamberts Solution for DSMs

    SBC: Advanced Space LLC            Topic: T11

    Distributed Spacecraft Missions (DSM) architectures provide unique scientific and programmatic benefits including multipoint in-situ measurements, multi-angle viewpoints, and improved understanding of the connections between separately measured phenomena and their time variations. However, these missions impose significant operational demands on ground tracking resources and mission operators alik ...

    STTR Phase II 2019 National Aeronautics and Space Administration
  2. 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
  3. 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
  4. Testing of COTS Systems in Space

    SBC: Streamline Automation, LLC            Topic: T6

    For long duration space missions beyond LEO, the complexity of the missions and the latency of communications with Earth will require HPC systems that would be prohibitively expensive if qualified under traditional guidelines for high reliability space systems. There is a wealth COTS hardware that could potentially be used for HPC systems for non-critical tasks within heavily shielded spacecraft c ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  5. 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
  6. Next Generation Distributed Electric Propulsion Urban Air Mobility Aircraft Analysis/Design Tools

    SBC: Continuum Dynamics Inc            Topic: T15

    Urban Air Mobility (UAM) aircraft development, enabled by Distributed Electric Propulsion (DEP), is transforming the aerospace industry by providing on-demand, affordable, quiet, and fast passenger-carrying operations in metropolitan areas. Designing and producing safe reliable UAM aircraft is particularly challenging given the relative infancy of electric propulsion for aeronautical applications, ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  7. Dual Mode Green Monopropellant Propulsion System for Interplanetary Missions

    SBC: Plasma Processes, LLC            Topic: T2

    Today many spacecraft carry two propulsion options: high thrust required for high acceleration maneuvers such as orbit insertion and rapid response; and low thrust required for station keeping and less critical maneuvers. A new class of non-toxic monopropellants, such as AF-M315E and LMP-103S, perform well in both high and low thrust regimes. Significant investments are maturing both monopropellan ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  8. Air Vehicle Gust Response analysis for Conceptual Design

    SBC: Research In Flight, LLC            Topic: T15

    Research in Flight (RIF) and Auburn University are offering the development of an advanced, robust tool and methodology that allows the simulation and modeling of gust and wake vortex encounters for Distributed Electric Propulsion (DEP) enabled Urban Air Mobility (UAM) vehicle concepts. DEP enabled UAM concepts offer the potential for large performance improvements by exploiting favorable synergie ...

    STTR Phase I 2019 National Aeronautics and Space Administration
  9. 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
  10. DEP Aircraft Terminal Area Ride Quality/Safety of Operations Assessment Tool

    SBC: Continuum Dynamics Inc            Topic: T15

    Dynamic gust encounters due to urban terrain and/or neighboring aircraft presents a significant safety hazard for Distributed Electric Propulsion (DEP) aircraft operating in Urban Air Mobility (UAM) environments.nbsp; DEP aircraft differ significantly from conventional single main rotor helicopters as they use multiple small rotors distributed over the airframe.nbsp; If a subset of these rotors ex ...

    STTR Phase I 2019 National Aeronautics and Space Administration
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