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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. Vertical Lift by Series Hybrid Power

    SBC: AURORA FLIGHT SCIENCES CORPORATION            Topic: A106

    A major market for vertical lift aircraft is in urban operations, primarily for police and electronic news gathering (typically a Bell 206 or a Eurocopter AS350). Manned systems are more costly to operate and have a much larger operational footprint than their unmanned counterparts. But the unmanned multirotor does not have the range and endurance to compete with the manned systems. Aurora Fligh ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  2. An Optimality Metrics Reporting Toolkit for SMART NAS

    SBC: RESILIENT OPS, INC.            Topic: A301

    This SBIR project aims to develop a software module for the SMART NAS Test Bed (or another similar simulation environment) that allows an apples-to-apples comparison of system performance across scenarios and a comparison to a 'best possible' case. The module, named TOMO (Toolkit for Optimality Metrics Overlay), is a metrics toolkit for comparing SMART NAS simulation runs to the optimal decision ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  3. A Distributed Resilient Autonomous Framework for Manned/Unmanned Trajectory-Based Operations

    SBC: RESILIENT OPS, INC.            Topic: A302

    Resilient Ops, working in collaboration with Metron Aviation, Inc., proposes to develop a prototype system for planning Unmanned Aircraft Systems (UAS) trajectories based on user intent and preference information. The system, called DRIFT-UAS (Distributed Resilient Framework for Trajectory Management of Unmanned Aircraft Systems), is intended to support autonomous Air Traffic Flow Management (ATFM ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  4. Multi-Species Chemical Microsensor For Real Time Cryogenic Purge Line Monitoring

    SBC: MAKEL ENGINEERING, INC.            Topic: H1001

    Makel Engineering, Inc. proposes to develop a miniaturized Multi-Species Chemical Microsensor Instrument suitable for real-time, in situ measurements of hydrogen, oxygen, water vapor and mixture thermal conductivity for monitoring purge effectiveness in cryogenic propellant lines. Helium is a scarce, strategic and non-renewable natural resource. NASA is a major user of helium and significant fut ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  5. High Pressure Electrochemical Oxygen Generation for ISS

    SBC: GINER INC            Topic: H1402

    Giner, Inc. has developed an advanced high pressure electrochemical oxygen concentrator (EOC) that offers a simple alternative to the use of pressure swing adsorption (PSA) systems to generate high pressure oxygen for the International Space Station (ISS) and future human space flight applications. The high pressure EOC is based on proven electrolyzer technology demonstrated at Giner and delivers ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  6. Additively Manufactured Monolithic LOx/Methane Vortex RCS Thruster

    SBC: PARABILIS SPACE TECHNOLOGIES INC            Topic: H201

    Parabilis Space Technologies proposes to advance development of an additively manufactured liquid oxygen (LOx) and liquid methane Reaction Control System (RCS) thruster in response to solicitation H2.01, In-Space Chemical Propulsion. This RCS-class thruster will provide a simple, robust, and low-cost solution for vehicle attitude control on upcoming NASA projects. The thruster is additively manuf ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  7. Passive Technology to Improve Criticality Control of NTP Reactors

    SBC: Ultra Safe Nuclear Corporation            Topic: H202

    This SBIR will develop passive reactor criticality control technology for Nuclear Thermal Propulsion (NTP) identified by Ultra Safe Nuclear Corporation (USNC) in Phase 1. This technology will allow NTP systems to start up by rotating the control drums to a single predetermined location and remain there for the duration of operation for the majority of the burns associated with a Mars mission. Pas ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  8. An Airborne Particulate Monitor for Spacecraft

    SBC: AEROSOL DYNAMICS INC            Topic: H301

    A compact instrument will be develop to provide long-term monitoring of the number concentration and approximate size of airborne particles in microgravity environments such as found aboard spacecraft cabins. Particles as small as 10 nm will be detected by a self-sustaining, tippable, water-based condensation particle counter. This will be coupled to an optical sizing instrument to provide particl ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  9. Microchip Capillary Electrophoresis for In-Situ Water Analysis

    SBC: LEIDEN MEASUREMENT TECHNOLOGY LLC            Topic: H301

    In this Small Business Innovation Research (SBIR) project, Leiden Measurement Technology, LLC (LMT) will develop a portable microfludic analysis instrument for measurement of inorganic ions present in potable water supplies, thermal control system cooling water, and human waste water. A primary goal of the Phase I effort was to identify and demonstrate the most viable development path to advance c ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  10. Pulsating Heat Pipes

    SBC: Peregrine Falcon Corporation            Topic: H801

    Large radiator panels, based upon state of the art conventional heat pipes with attached fins for thermal load distribution and dissipation is the current baseline design for NASA?s Fission Power System. The initial 1 kWe FPS requires a total radiating surface of 2.5 m2. Higher power designs will require corresponding larger radiating surfaces. In order to achieve optimum radiator performance, the ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
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