Pioneer Astronautics

Basic Information

CO
Lakewood, CO, 80215-5516

http://www.pioneerastro.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 120561456
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 8


  1. Advanced Wastewater Photo-oxidation System

    Amount: $124,946.00

    Pioneer Astronautics proposes an advanced photocatalytic oxidation reactor for enhancing the reliability and performance of Water Recovery Post Processing systems aboard crewed spacecraft. This novel ...

    SBIR Phase I 2014 National Aeronautics and Space Administration
  2. Nitrous Oxide Ethane Ethylene Engine

    Amount: $124,660.00

    The Nitrous Oxide Ethane-Ethylene (NEE) engine is a proposed technology designed to provide spacecraft with non-toxic non-cryogenic high-performance propulsion. With the NEE engine, nitrous oxide is ...

    SBIR Phase I 2013 National Aeronautics and Space Administration
  3. High Performance Photocatalytic Oxidation Reactor System

    Amount: $124,880.00

    Pioneer Astronautics proposes a technology program for the development of an innovative photocatalytic oxidation reactor for the removal and mineralization of Volatile Organic Compounds to extend crew ...

    SBIR Phase I 2013 National Aeronautics and Space Administration
  4. Lunar Organic Waste Reformer

    Amount: $599,931.00

    The Lunar Organic Waste Reformer (LOWR) utilizes high temperature steam reformation to convert all plastic, paper, and human waste materials into useful gases. In the LOWR, solar thermal concentrators ...

    SBIR Phase II 2011 National Aeronautics and Space Administration
  5. Nitrous Oxide Micro Engines

    Amount: $99,999.00

    Nitrous Oxide Micro Engines (NOME) are a new type of nitrous oxide dissociation thruster designed to generate low levels of thrust that can be used for RCS control in large satellites or as main propu ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  6. Mars Regolith Water Extractor

    Amount: $99,999.00

    The Mars Regolith Water Extractor (MRWE) is a system for acquiring water from the Martian soil. In the MRWE, a stream of CO2 is heated by solar energy or waste heat from a nuclear reactor and then pas ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  7. Regenerable Contaminant Removal System

    Amount: $99,984.00

    The Regenerable Contaminant Removal System (RCRS) is an innovative method to remove sulfur and halide compounds from contaminated gas streams to part-per-billion levels in support of lunar oxygen prod ...

    SBIR Phase I 2011 National Aeronautics and Space Administration
  8. Lunar Organic Waste Reformer

    Amount: $99,964.00

    The Lunar Organic Waste Reformer (LOWR) utilizes high temperature steam reformation to convert all plastic, paper, and human waste materials into useful gases. In the LOWR, solar thermal concentrators ...

    SBIR Phase I 2010 National Aeronautics and Space Administration
  9. Multi-Cell Thermal Battery

    Amount: $599,990.00

    The multi-cell thermal battery (MCTB) is a device that can recover a large fraction of the thermal energy from heated regolith and subsequently apply this energy to heat up cool regolith. The individu ...

    SBIR Phase II 2010 National Aeronautics and Space Administration
  10. Lunar Soil Particle Separator

    Amount: $599,827.00

    The Lunar Soil Particle Separator (LSPS) is an innovative method to beneficiate soil prior to in-situ resource utilization (ISRU). The LSPS can improve ISRU oxygen yield by boosting the concentration ...

    SBIR Phase II 2010 National Aeronautics and Space Administration

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