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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY23 is not expected to be complete until September, 2024.

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.

Displaying 196121 - 196130 of 204455 results
  1. Monolithic Q-switched waveguide laser fabricated by ultrafast laser inscription for pulsed lidar source

    SBC: AKTIWAVE LLC            Topic: S11

    We plan to develop a monolithic Q-switched Waveguide Laser, using ultrafast laser inscription (ULI) technology. The proposed prototype is enabled by a Q-switched operation of waveguide realized by ULI inside diffusion-bonded laser media. Owing to its flexibility, ease for integration, and three-dimension nature, ULI of waveguides in laser materials and dielectric media enables transformative lidar ...

    SBIR Phase I 2022 National Aeronautics and Space Administration
  2. Single Fluid Tuned Winding Induction Motors

    SBC: CGC Ultramarin Ltd            Topic: A1

    This proposal focusses on the development of two high power density and high reliability asynchronous lift motors for Electric Vertical Takeoff and Landing (eVTOL) being relevant to the NASA Revolutionary Vertical Lift Technology (RVLT) Project. These motors are proposed in response to NASArsquo;s A1.06 Vertical Lift Technology for Urban Air Mobility -Electric Motor Fault Mitigation Technology req ...

    SBIR Phase I 2022 National Aeronautics and Space Administration
  3. Motorless Expandable Solar Array (MESA)

    SBC: DYNOVAS INC            Topic: H5

    Dynovasrsquo; Motorless Expandable Solar Array (MESA) system provides a novel solution that specifically addresses NASArsquo;s call for technologies enabling structural and mechanical innovations for a 50-kW-class solar array that can be relocated and deployed at least 5 times.nbsp; This solution was developed based on previous technologies that have proven track record such as inflatables and bis ...

    SBIR Phase I 2022 National Aeronautics and Space Administration
  4. Improved Thermo-Mechanical Design of the VASIMR RF Coupler

    SBC: AD ASTRA ROCKET CO            Topic: Z10

    Ad Astra Rocket Company proposes a novel method of manufacturing a VASIMRreg; coupler.nbsp; This method intends to increase the surface area in contact between the actively cooled coupler and the plasma facing GCT resulting in a lower heat flux between the components, lower temperature on the GCT, higher operational temperature margin, and ultimately a higher steady-state operational power limit o ...

    SBIR Phase I 2022 National Aeronautics and Space Administration
  5. LIGHTWEIGHT MICROTUBE PHASE CHANGE MATERIAL HEAT EXCHANGERS

    SBC: International Mezzo Technologies, Inc.            Topic: Z2

    The primary goal of this program is to develop the significant weight-saving potential of phase change material (PCM) microtube heat exchangers for NASA spacecraft thermal management. Mezzo will utilize microtube heat exchanger technology along with topography optimization and 3D printing to allow for cutting-edge performance and weight savings.

    SBIR Phase I 2022 National Aeronautics and Space Administration
  6. Optimized miniature spectrometer for improved trace gas monitoring and satellite validation

    SBC: SCIGLOB INSTRUMENTS & SERVICES LLC            Topic: S11

    SciGlob proposesnbsp;the development of an optimized miniature spectrometer for improved trace gas monitoring and satellite validation. The new spectrometer will be substantially superior to the ones currently used giving higher signal-to-noise ratio, having less stray light and better temperature stabilization, and also a more repeatable manufacturing and alignment process. Thisnbsp;will signific ...

    SBIR Phase I 2022 National Aeronautics and Space Administration
  7. High-Purity, Defined-Envelope Pressure Bladder

    SBC: Rapa Technologies LLC            Topic: H4

    The NASA Portable Life Support System (PLSS) for the Exploration Extravehicular Mobility Unit (xEMU) incorporates a Feedwater Supply Assembly (FSA) to store consumable cooling water. The FSA must accept a total of 12 lbs. of pure water prior to each Extra-Vehicular Activity (EVA), then supply this water to the cooling loop at ambient suit pressure during the EVA, functioning reliably for 700 cycle ...

    SBIR Phase II 2022 National Aeronautics and Space Administration
  8. Lightweight and Low Stow Volume Solar Concentrator for Lunar Based In-Situ Resource Utilization

    SBC: L'GARDE, INC.            Topic: Z12

    The objective of the proposed Phase II effort is to further develop a lightweight and low stow volume solar concentrator for use in lunarnbsp;in-situ resource utilization (ISRU) applications, specifically for oxygen extraction from lunar regolith. In the Phase I effort, anbsp;design of a full scale solar concentrator was created, and analysis showed the solar concentrator meeting NASA performance ...

    SBIR Phase II 2022 National Aeronautics and Space Administration
  9. Improved Abrasion Resistance of High Temperature Seals

    SBC: Jackson Bond Enterprises LLC            Topic: A1

    In Phase I, JBE proved that two coatings improved the abrasion resistance of materials typically used in high temperature seals.nbsp; Phase I testing was done at ambient temperature.nbsp; In Phase II, JBE will determine the optimal seal material and coating combinations, work to optimize the coating processes, and validate the improved abrasion resistance at representative and relevant temperature ...

    SBIR Phase II 2022 National Aeronautics and Space Administration
  10. Materials for Structural and Thermal Preservation of Sample Return Payload During Earth Entry and Landing

    SBC: ULTRAMET            Topic: S13

    To maximize reliability, Earth entry/landing vehicles for robotic sample return missions will comprise an aeroshell, a crushable layer that will absorb the energy of the ballistic impact landing, and a sample container inside the crushable layer; parachutes will not be used. Lightweight carbon foams are being considered for the crushable layer, but many other foams with different strengths and ene ...

    SBIR Phase I 2022 National Aeronautics and Space Administration
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