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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-Function Fluid Measurement System using High-Definition Fiber Optic Sensing

    SBC: LUNA INNOVATIONS INCORPORATED            Topic: T13

    Propulsion systems require rigorous and highly instrumented testing to enable a comprehensive analysis of performance and to minimize risks associated with space flight. Current testing instrumentation methods can be replaced with embedded sensor systems that are used for monitoring remote, hazardous, or inaccessible locations, while reducing cabling and power consumption. The additional informati ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  2. Automated Fiber Placement of Thin-Ply Composite Materials for Large Aerospace Structures

    SBC: NEXTGEN MATERIALS & PROCESSING LLC            Topic: T12

    Leveraging their prior experience working with automated fiber placement (AFP) of thin-ply composite materials, NextGen Materials & Processing LLC and the University of Massachusetts Lowell will utilize a Design of Experiments approach, combined with analytical modeling, to identify the critical material, slitting, spooling, and AFP parameters that influence the repeatable, high quality laydown of ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  3. Efficient CO2 and H2O Removal with Novel Adsorbentsfor Life Support Applications on Mars

    SBC: MOSAIC MATERIALS, INC.            Topic: T6

    Very low CO2 concentrations that accumulate quickly from human respiration can have dramatic health effects, and thus in NASA’s history many technical removal strategies for CO2 from a confined atmosphere have been suggested and explored. A CO2 removal system that functions in a is a new area of research, as the primary CO2 removal component in the state-of-the-art system doesn’t have the adso ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  4. Integrated Photonic Filters for RF Signal Processing

    SBC: OEWAVES, INC            Topic: T8

    In this Project, OEwaves Inc. and Georgia Tech team propose to research and develop a unique RF photonic receiver front-end enabling microwave signal processing at a heterogeneously integrated photonic platform. In particular, we propose to develop a new technology for photonic microwave filters based on the new advances in Si-based integrated photonics. We will exploit the expertise of the team m ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  5. Multiscale Design Tool and Process Development of Thin-Ply Composites

    SBC: TECHNICAL DATA ANALYSIS, INC.            Topic: T12

    Use of thin ply composites offers good potential for significant mass savings for aerospace structures besides its improved resistance to micro-cracking, fatigue, and delamination. However, mass savings due to thin-ply technology depends on material and fabrication technology, vehicle configuration, structural design, loads etc. Structural integrity of components made from thin plies need to be c ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  6. Regeneratively Cooled Ceramic Matrix Composite Nozzle Assembly for Reduced Weight

    SBC: PHYSICAL SCIENCES INC.            Topic: T9

    All rocket missions benefit from having lower structural mass and higher specific impulse, both of which contribute to larger payload fractions and therefore lower mission cost. High temperature materials such as ceramic matrix composites (CMCs) are an avenue to lower engine mass because of the low density and high specific strength of the material. They also have a high maximum temperature and so ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  7. Nanosat Maneuvering and Orbital Transfer Stage

    SBC: PARABILIS SPACE TECHNOLOGIES INC            Topic: T1

    The proposed innovation is a modular, high-performance orbital transfer stage (OTS) vehicle for Nanosats and Microsats launched as secondary payloads and require maneuvering to their desired orbits. The OTS has a modular design, and can accommodate payloads ranging from 5kg 3U size Nanosats to >50kg Microsat size vehicles. The propulsion system uses hydroxyl-terminated polybutadiene (HTPB) fuel wi ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  8. Refractory Additively Manufactured Affordable Launch Vehicle RCS

    SBC: VALLEY TECH SYSTEMS INC            Topic: T1

    Due to the rapid maturity of small satellite technologies to meet near term commercial, science and military space applications there is a driving need for development of increased affordable space launch system capability. To address this need, Valley Tech Systems and the University of Texas El Paso (UTEP) is proposing evolving our innovative Affordable Launch Vehicle Reaction Control System (AL ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  9. Chip-scale THz Spectrometer

    SBC: NEXUS PHOTONICS INC            Topic: T8

    We propose to revolutionize the field of frequency-domain terahertz (THz) spectrometers by developing ~2 cm3 wide-band spectrometer with improved frequency accuracy, resolution and stability. Integration will also provide significant SWaP-C advantage compared to present solution allowing deployment in small spacecraft platforms and other applications where low SWaP is crucial.Compared to presently ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  10. Properties Investigation of High-MON Oxidizers for Use in Deep Space Exploration

    SBC: Frontier Aerospace Corporation            Topic: T9

    Rocket propulsion for deep space applications typically use liquid propellants for axial stage and attitude control systems. The most common propellants are hydrazine (N2H4) and monomethylhydrazine (MMH) (CH3N2H3) for the fuels, and nitrogen tetroxide (NTO) (N2O4) for the oxidizer. The freezing points of both hydrazine and NTO approach room temperature and require on-board electrical heaters for t ...

    STTR Phase I 2018 National Aeronautics and Space Administration
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