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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-Band Software Defined Radio Sensor System

    SBC: Pegasense, LLC            Topic: T13

    This Multiband Software Defined Radio (SDR) sensor system proposal will demonstrate the ability to operate within multiple frequency bands and across multiple technology platforms in a single transceiver. The center frequencies and bandwidths chosen are representative of current demonstrated commercial or research devices and bands used: 400 MHz, 900 MHz, and 2.4 GHz ISM bands, with bandwidths of ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  2. 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
  3. Wireless Passive Nanoparticle based Intelligent Sensor System for Extreme Environments

    SBC: SENSATEK PROPULSION TECHNOLOGY, INC            Topic: T13

    Sensatek Propulsion Technology, Inc. proposes to demonstrate the feasibility of a wireless, passive, nanoparticle-based sensor system. The sensor in its current form can be used to measure real time temperatures and pressures wirelessly without the need of an external energy source. It should be noted that the same sensing principle can be used for strain monitoring as well. It comprises of a micr ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  4. A Supported Liquid Membrane System for Steady State CO2 Control in a Spacecraft Cabin

    SBC: REACTION SYSTEMS, INC.            Topic: T6

    Reducing the allowable concentration of carbon dioxide (CO2) in spacecraft is a critical need for NASA. The system now used on the International Space Station (ISS) is the carbon dioxide removal assembly (CDRA). While it has performed well on the ISS, managers have concluded that using the device to reach the new ppCO2 limit of 2.0 mm Hg is not practical and a new method is needed.In this projec ...

    STTR Phase I 2018 National Aeronautics and Space Administration
  5. 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
  6. 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
  7. Extensible Modeling to Create Knowledgebase for AM Processing of Alloy GrCop-84

    SBC: APPLIED OPTIMIZATION, INC.            Topic: T12

    The research objective of the proposed work is to demonstrate feasibility of utilizing extensible modeling to create an AM knowledgebase for copper alloy, GrCop-84, and utilize it to design an AM process for GrCop-84. The work plan has three tasks: (1) Utilize process modeling to demonstrate feasibility of predicting AM process parameters for alloy GrCop-84 for the powder bed and blown powder proc ...

    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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