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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. Volume Sensor for Flexible Fluid Reservoirs in Microgravity

    SBC: CREARE LLC            Topic: T6

    The Advanced Space Suit carries consumable cooling water maintained at ambient pressure within a soft-walled, flexible reservoir. To ensure uninterrupted thermal control it is critical to monitor the volume of water remaining, but no known sensor is suitable for this task. Existing measurement techniques are unacceptably sensitive to the motion and varying geometry of the reservoir in microgravity ...

    STTR Phase II 2018 National Aeronautics and Space Administration
  2. Low Cost Cryocooler Control Electronics for Small Space Platforms

    SBC: CREARE LLC            Topic: S1

    Many of NASA’s future space science missions will utilize small spacecraft, and many of these missions will require cryocoolers for cooling detectors, sensors, shields, and telescopes. For Class C and D missions, the cryocooler technical requirements for performance, size, and mass, coupled with the programmatic requirements for minimal cost and development time, are extremely challenging. Fli ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
  3. A Two-Phase Pumped Loop Evaporator with Adaptive Flow Distribution for Large Area Cooling

    SBC: CREARE LLC            Topic: S3

    NASA’s future remote sensing science missions require advanced thermal management technologies to maintain multiple instruments at very stable temperatures and utilize waste heat to keep other critical subsystems above minimum operational temperatures. Two-phase pumped loops are an ideal solution for these applications. A critical need for these pumped loops is a microgravity-compatible evaporat ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
  4. VLWIR Sensors for Detecting and Tracking Near-Earth Asteroids

    SBC: QMAGIQ LLC            Topic: S1

    An important NASA mission is to detect, count and track near-earth asteroids for a variety of reasons including the hazards of collisions with our planet. Such asteroids are mostly dark, small and cold (~ 200K); so they are best detected in the very longwave infrared (VLWIR) wavelengths greater than ~ 12 microns where they glow brightest. To accomplish this, we developed in Phase I a record-perfor ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
  5. Open-Source Pipeline for Large-Scale Data Processing, Analysis and Collaboration

    SBC: CREARE LLC            Topic: S5

    NASA's observational products generate petabytes of scientific data, which are highly underutilized due to computational requirements; disjoint data access protocols; and task-specific, non‑reusable code development. Our overall objective is to accelerate NASA science through development of an open-source, Python-based Pipeline for Observational Data Processing, Analysis, and Collaboration ( ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
  6. Multi-Spectral Infrared Focal Plane Array For Wildfire And Burning-Biomass Analysis

    SBC: QMAGIQ LLC            Topic: S1

    An important NASA mission is to remotely analyze fires, such as wildfires and burning biomasses, for their chemical content. The chemical species of most interest have infrared spectral signatures at wavelengths ranging from 1.5 microns to 12 microns. A broadband infrared focal plane array (FPA) with that spectral coverage and high quantum efficiency is a key technology to enable this mission. Qma ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  7. Optically Interrogated Thin Film Strain Gauge for Balloon

    SBC: CREARE LLC            Topic: S3

    To support development of atmospheric balloons and gossamer structures, NASA requires a capability for real-time, dynamic strain measurement in thin polymeric membranes during deployment and flight. This capability will provide quantitative test data to inform balloon design efforts, as well as enable real-time monitoring of material state during flight. Existing technologies include wired or wi ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  8. High Efficiency 4 K Cryocooler for Space Missions

    SBC: CREARE LLC            Topic: S1

    Future astrophysics missions require efficient, low-temperature cryocoolers to cool advanced instruments or serve as the upper stage cooler for sub-Kelvin refrigerators. Potential astrophysics missions include Lynx, the Origin Space Telescope, and the Superconducting Gravity Gradiometer. Cooling loads for these missions are up to 300 mW at temperatures of 4 to 10 K, with additional loads at higher ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  9. ASOMIS

    SBC: APPLIED GEOSOLUTIONS LLC            Topic: S5

    The innovation of the Agricultural SOil Moisture and Irrigation Status (A·SOM·IS) platform is the development of operational and moderate resolution mapping and assessment of soil moisture, irrigation status (irrigated vs not), and crop water stress metrics at field scale for agricultural decision support tools. The platform focuses on utilization of Synthetic Aperture Radar (SAR) and blends SAR ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
  10. A Compact, Lightweight Electrically Driven Propellant Pump with High Pressure Rise

    SBC: CREARE LLC            Topic: S4

    Reducing the inert mass of propulsion systems in sample return spacecraft will reduce their launch costs and increase opportunity for these missions. Compared to a pressure-fed system, a propellant pump-fed system can significantly reduce overall propulsion system mass, especially for a system with high propellant throughput. To address this need, we propose to develop a compact, lightweight elect ...

    SBIR Phase I 2018 National Aeronautics and Space Administration
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