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Award Data

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The Award database is continually updated throughout the year. As a result, data for FY20 is not expected to be complete until September, 2021.

  1. Warm Gas Generator Resistojet Micropropulsion System

    SBC: Benchmark Space Systems, Inc.            Topic: Z8

    Benchmark Space Systems proposes a resistojet micropropulsion system that leverages a solid gas generator to offer high-performance, low-cost propulsion with key safety features. This system is designed to offer 1600 Nbull;s in a 2U frame.The design calls for one central thruster that will provide 0.2 N of thrust. The resistojet thruster uses a patent-pending exothermic Warm Gas Generator (WGG) th ...

    SBIR Phase I 2019 National Aeronautics and Space Administration
  2. Advanced Display Interface Technology

    SBC: CREATIVE MICROSYSTEMS CORPORATION            Topic: H1202

    CMC proposes, along with our collaborator, Dr. Mica Endlsey of SA Technologies, to produce a framework from which an Adaptive User Interface (AUI) can be modeled and ultimately developed that utilizes Augmented Reality (AR) to improve Situational Awareness (SA) for spaceflight users in a high-workload scenario. This effort includes a thorough literature review related to the effects of modality an ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  3. Ultra-Narrow Bandpass Filters for Long Range Optical Telecommunications at 1064nm and 1550nm

    SBC: Omega Optical, Inc.            Topic: H901

    Ultra-narrow bandpass filters with high off-band rejection are needed to maximize signal to noise for free space communications. Omega Optical is developing NIR filters with less than 1 nm bandwidths, which are thermally stable, and provide high rejection of adjacent communication channels. This program will address advancing these filters from a technology readiness level (TRL) of 3 to TRL 5. Dev ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  4. In-Suit Waste Management Technologies

    SBC: Omni Measurement Systems, Inc.            Topic: H401

    There is no acceptable urine or fecal containment waste management system for long duration missions for use by crew members confined to pressurized space suits available. Omni's proposed solution is to integrate its new patent pending urine collection and containment system technology, ProRen FLO (Prosthetic Renal Flow System), combined with Omni fecal collection and containment options into a I ...

    SBIR Phase II 2016 National Aeronautics and Space Administration
  5. In-Suit Waste Management Technologies

    SBC: Omni Measurement Systems, Inc.            Topic: H401

    There is no acceptable urine or fecal containment waste management system for long duration missions for use by crew members confined to pressurized space suits available. Omni's proposed solution is to integrate its new patent pending urine collection and containment system technology, ProRen FLO (Prosthetic Renal Flow System), combined with Omni fecal collection and containment options into a In ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  6. Inlet Cover Treatment to Enhance Zero NPSH Inducer Operation

    SBC: Concepts NREC, LLC            Topic: H203

    Zero net positive suction head (NPSH)-capable hydrogen pump inducers are a critical component needed to lower the cost and increase the effectiveness of Nuclear Thermal Propulsion (NTP) engines. Zero NPSH pumps need to be able to pump up to 55% vapor fraction by volume without significant head fall-off. Current technology inducers can pump liquid hydrogen up to a limit of about 25% vapor fractio ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  7. Extremely High Suction Performance Inducers for Space Propulsion

    SBC: Concepts NREC, LLC            Topic: T901

    The proposed innovation provides a way to design low flow coefficient inducers that have higher cavitation breakdown margin, larger blade angles, thicker more structurally robust blades, and better off-design flow stability than the current state-of-the-art designs. The technology will increase the structural, stability, and suction margin of inducers designed in the currently acceptable flow coe ...

    STTR Phase II 2011 National Aeronautics and Space Administration
  8. Extremely High Suction Performance Inducers for Space Propulsion

    SBC: Concepts NREC, LLC            Topic: T901

    Advanced pump inducer design technology that uses high inlet diffusion blades, operates at a very low flow coefficient, and employs a cavitation control and stability device. A preliminary scoping inducer test with this technology indicated a doubling of the suction specific speed capability over current inducers. A three to four fold increase over current technology is the goal of this research ...

    STTR Phase I 2010 National Aeronautics and Space Administration
  9. Application of a Fused Carbon Nanomaterial Filter for Lunar Dust Abatement

    SBC: Seldon Technologies, Inc.            Topic: X301

    Seldon Technologies will further test and develop its patented carbon nanotube filtration technology to NASA's Lunar Exploration challenges. This project focuses on the problem of efficient removal of nanoscale (10-100nm) and larger lunar dust particulates from air using a nanostructured fiber media containing carbon nanotubes. Lunar dust presents an important challenge to Lunar exploration and ha ...

    SBIR Phase II 2009 National Aeronautics and Space Administration
  10. Application of a Fused Carbon Nanomaterial Filter for Lunar Dust Abatement

    SBC: Seldon Technologies, Inc.            Topic: X301

    Seldon Laboratories, LLC, will apply its patented carbon nanotube filtration technology for air and nanoscale particulate engine exhaust filtration to NASA's Lunar Exploration challenges. This project focuses on the problem of efficient removal of nanoscale (10-100nm) and larger lunar dust particulates from air using a nanostructured fiber media containing carbon nanotubes. Lunar dust presents an ...

    SBIR Phase I 2008 National Aeronautics and Space Administration
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