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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. 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
  2. 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
  3. Light Weight Spherical Cryotank

    SBC: GLOYER-TAYLOR LABORATORIES INC            Topic: H204

    BHL? technology offers the means to reduce the mass of cryogenic propellant tanks by 75% relative to state-of-the-art metal tanks. Since propellant tanks are generally the largest individual mass item on a launch vehicle or spacecraft, this mass savings of this magnitude can have profound effect on vehicle performance. A conceptual design of a spherical BHL cryotank for the NASA Morpheus Lander ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  4. 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
  5. 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
  6. 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
  7. Micropump for MON-25/MMH Propulsion and Attitude Control

    SBC: Flight Works, Inc.            Topic: S302

    Flight Works is proposing to expand its work in micro-gear-pumps for hypergolic and ?green? propellants in order to develop and demonstrate a micropump for MON-25 and mono methyl hydrazine (MMH) bipropellant thrusters. MON-25, with 25% of nitric oxide (NO) and 75% nitrogen tetroxide (NTO, N2O4), allows lowering the oxidizer freezing point to -55 C, which is a close match to that of the fuel, MMH ( ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  8. Precision Guided Parafoil System For Sounding Rocket Recovery

    SBC: STARA Technologies, Inc.            Topic: S304

    The primary goal of the proposed STARA innovation is to develop and demonstrate a high altitude precision guided parafoil system that will enable NASA to control the final landing point of the sounding rocket payload, thus reducing system offset, recovery time, and recovery cost. Current recovery methods utilize unguided parachutes, which are susceptible to large uncertainties in recovery location ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  9. Industrial Electrostatic-Gecko Gripper

    SBC: Somatis Sensor Solutions LLC            Topic: S402

    Perception Robotics is developing an innovative product, the Electrostatic Gecko Gripper? (ESG Gripper), for the industrial automation market. This unique gripping solution overcomes the shortcomings of vacuum grippers by eliminating the need for a compressed air system and offering more rapid actuation, thus achieving significant cost savings and throughput improvements in customers? manufacturi ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  10. Continued Development of Environmentally Conscious "ECO" Transport Aircraft Concepts as Hybrid Electric Distributed Propulsion Research Platforms

    SBC: EMPIRICAL SYSTEMS AEROSPACE INC            Topic: A103

    ESAero's vast TeDP and HEDP-specific experience, Helden Aerospace's distributed propulsion airframe integration effects & CFD analysis experience, and Rolls-Royce's propulsion and power, thermal management, and fault tolerant microgrid systems design experience will be leveraged to develop the ECO-150 and ECO-80 concepts as Vision Vehicles which can become research platforms to investigate the pot ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
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