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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.

Displaying 172691 - 172700 of 207728 results
  1. N/A

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    N/A

    SBIR Phase I 2000 National Aeronautics and Space Administration
  2. N/A

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    N/A

    SBIR Phase I 2000 National Aeronautics and Space Administration
  3. N/A

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    N/A

    SBIR Phase II 2000 National Aeronautics and Space Administration
  4. Methane to Aromatics on Mars

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The Methane to Aromatics on Mars (METAMARS) project will design and build a machine for converting methane produced by the Sabatier reaction into a low hydrogen content, low vapor pressure, high density, aromatic fuel. Its primary advantage is a factor of four reduction of hydrogen feedstock importation requirements for production of rocket fuel compared to the standard S/E process for an equivale ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  5. Carbon dioxide Oxidizer Rocket

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The Carbon dioxide Oxidizer Rocket (COR) is a novel propulsion system concept that can enable global mobility for Mars exploration. In this concept a fuel, such as B2H6, B5H9, SiH4, LiBH4, Al(BH4)3, H2, Mg, NH3 or N2H4 is transported to Mars and burned in the COR engine using native Martian CO2 as the oxidizer. Specific impulses for these propellant combinations range from 200 to 320 s. Because th ...

    SBIR Phase I 2001 National Aeronautics and Space Administration
  6. Methane to Aromatics on Mars

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The Methane to Aromatics on Mars (METAMARS) project will design and build a machine for converting methane produced by the Sabatier reaction into a low hydrogen content, low vapor pressure, high density, aromatic fuel. Its primary advantage is a factor of four reduction of hydrogen feedstock importation requirements for production of rocket fuel compared to the standard S/E process for an equivale ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  7. Lightweight Auto-Inflating Self-Rigidizing Booms

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    Lightweight Auto-Inflating Self-Rigidizing Booms (LAISRB) is a key technology to enable large space ?gossamer? structures such as radiometer or radar antennas or solar sails. In Pioneer Astronautics LAISRB concept, inflatable tubes containing a small amount of methanol and a UV-curing self-hardening resin are deployed in a canister attached to the gossamer structure. Upon reaching deployment orbit ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  8. Methane to Aromatics on Mars

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The Methane to Aromatics on Mars (METAMARS) project will design and build a machine for converting methane produced by the Sabatier reaction into a low hydrogen content, low vapor pressure, high density, aromatic fuel. Its primary advantage is a factor of four reduction of hydrogen feedstock importation requirements for production of rocket fuel compared to the standard S/E process for an equivale ...

    SBIR Phase II 2002 National Aeronautics and Space Administration
  9. Nitrous Oxide Monopropellant rocket

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The Nitrous Oxide Monopropellant Rocket (NOMR) is a new Extravehicular Mobility Unit (EMU) thruster concept using nitrous oxide as a monopropellant. Liquid monopropellants are often used in propulsion systems where simplicity of design, restartable/control on demand, and repeatability is desired. Unfortunately, many monopropellants are toxic and dangerous, ruling them out for EMU thruster applicat ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
  10. Carbon Monoxide Metal Oxide Reduction System

    SBC: PIONEER ASTRONAUTICS            Topic: N/A

    The Carbon Monoxide Metal Oxide Reduction System (COMORS) is a method of producing useful oxygen by reducing oxides found in Lunar and Martian surface material. The COMORS heats the oxides to temperatures where the oxygen atoms combine with carbon monoxide gas acting as a reducing agent, producing carbon dioxide. The CO2 is reduced with hydrogen in a reverse water gas shift (RWGS) reactor, and the ...

    SBIR Phase I 2002 National Aeronautics and Space Administration
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