List

For best search results, use the search terms first and then apply the filters
Reset

The Award database is continually updated throughout the year. As a result, data for the given year is not complete until April of the following year. Annual Reports data is a snapshot of agency reported information for that year and hence might look different from the live data in the Awards Information charts.

  1. Go Write

    SBC: Attainment Co., Inc.            Topic: 91990018R0006

    In this project, the team will develop a prototype of GoWrite, a platform designed for students with moderate to severe disabilities to guide instruction in writing. The cross-curricular intervention will have four modes including instruction, writing about academic content, journaling, and social media. At the end of Phase I, in a pilot study with 30 students (10 each in grade school, middle scho ...

    SBIR Phase I 2018 Department of EducationInstitute of Education Sciences
  2. Polymer Coating-Based Contaminant Control/Elimination for Exo-S Starshade Probe

    SBC: Photonic Cleaning Technologies LLC            Topic: S2

    Our First Contact Polymer (FCP) is an easy-to-apply, residue-less, peelable strip coat that protects and cleans optics, detectors, and other sensitive surfaces, restoring them to a pristine condition. Using FCP is as simple as spraying or brushing it on a surface of interest, allowing it to dry for 15 minutes, and stripping off the rugged coating when desired. Multiple measurements, including at N ...

    SBIR Phase II 2018 National Aeronautics and Space Administration
  3. Polymer Coating-Based Contaminant Control/Elimination for Exo-S Starshade Probe

    SBC: Photonic Cleaning Technologies LLC            Topic: S201

    Our past success in developing what has proven to be a revolution in contamination control ? that of residue free, strippable polymer coatings for surface protection and cleaning has, so far, been limited use on substrates such as glass, fused silica and aluminum. These are the types of surfaces found on flagship projects such as the LIGO Gravitational Wave Observatory, the 10 meter class WM Keck ...

    SBIR Phase I 2017 National Aeronautics and Space Administration
  4. High Capacity, High Efficiency 10 to 20 K Pulse Tube Cryocooler

    SBC: Madison CryoGroup LLC            Topic: S109

    Closed-cycle cryocooler alternatives currently available for space applications in the temperature range of 10 to 20 K are not well suited to the requirements of such applications. In many cases reliability is low and vibration high. In other cases, coolers are too massive and inefficient. However, such coolers are often important components in enabling many of the advanced sensor and detector tec ...

    SBIR Phase I 2016 National Aeronautics and Space Administration
  5. Pulsating Heat Pipe for Cryogenic Fluid Management

    SBC: Madison CryoGroup LLC            Topic: H204

    A passive Pulsating Heat Pipe (PHP) system is proposed to distribute cooling over broad areas with low additional system mass. The PHP technology takes advantage of the large latent heat associated with phase change of a working fluid that is confined to small capillaries to carry heat efficiently from evaporator regions to a condenser that is attached to the cold head of the cryocooler. This sy ...

    SBIR Phase I 2015 National Aeronautics and Space Administration
  6. Zero G Mass Measurement Device (ZGMMD)

    SBC: Orbital Technologies Corporation            Topic: E103

    The Zero Gravity Mass Measurement Device (ZGMMD) provides the ability to measure the mass of samples in a microgravity environment, like that found on the International Space Station (ISS). One of the primary measurements often taken during science experiments is mass. This is even more relevant in biology, where mass is often one of the key measurements taken for analysis. During the Phase I effo ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  7. Miniature Nontoxic Nitrous Oxide-Propane (MINNOP) Propulsion

    SBC: Orbital Technologies Corporation            Topic: S302

    ORBITEC proposes to develop the Miniature Nontoxic Nitrous Oxide-Propane (MINNOP) propulsion system, a small bipropellant propulsion system which we offer as an alternative to miniature hydrazine monopropellant thrusters for CubeSat-class spacecraft. As compared to state-of-the-art hydrazine systems, MINNOP propulsion will provide significant increases in specific impulse (in bipropellant mode) a ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  8. Cryocooler With Cold Compressor for Deep Space Applications

    SBC: Madison CryoGroup LLC            Topic: S106

    The innovation is a high-frequency single-stage pulse tube cryocooler (PTC) that operates at a heat rejection temperature of 150 K. It employs a flexure-bearing cold compressor operating at that same heat rejection temperature. High frequency, low temperature pulse-tube cryocoolers are a promising technology for future NASA missions. Such missions will require cryocoolers providing cooling capacit ...

    SBIR Phase II 2014 National Aeronautics and Space Administration
  9. Plastic Melt Waste Compactor Flight Demonstrator Payload (PFDP)

    SBC: Orbital Technologies Corporation            Topic: H2002

    The PMWC Flight Demonstrator Payload is a trash dewatering and volume reduction system that uses heat melt compaction to remove nearly 100% of water from trash while significantly reducing the volume. Recent advances have proven that ORBITEC's HEHO-PMWC is a viable technology for producing 16" square tiles for radiation protection. ORBITEC proposes to enhance the current SOA by repackaging all the ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  10. VTX HyHeat

    SBC: Orbital Technologies Corporation            Topic: H204

    In this project Orbital Technologies Corporation (ORBITEC) will utilize its unique vortex propulsion technology to develop a high-capacity heating system to heat hydrogen to extremely high temperature levels. The heated hydrogen is to be used for test purposes for nuclear rocket propulsion simulations and total exhaust recovery applications. Our vortex rocket propulsion system is able to reliabl ...

    SBIR Phase I 2014 National Aeronautics and Space Administration

Agency Micro-sites

SBA logo
Department of Agriculture logo
Department of Commerce logo
Department of Defense logo
Department of Education logo
Department of Energy logo
Department of Health and Human Services logo
Department of Homeland Security logo
Department of Transportation logo
Environmental Protection Agency logo
National Aeronautics and Space Administration logo
National Science Foundation logo
US Flag An Official Website of the United States Government