Company Information
Address 6325 W 55TH AVE
ARVADA, CO, 80002-2707


DUNS: 074072554

# of Employees: 66

Ownership Information

HUBZone Owned: N

Socially and Economically Disadvantaged: N

Woman Owned: N

Award Charts

Award Listing

  1. Enabling Pump Technologies for Deep Throttle Ascent/Descent Engine Operation

    Amount: $124,882.00

    Methane fueled ascent / descent space engines in the 10,000 to 25,000 lbf thrust class require deep throttle capability, placing unique challenges on the turbopumps. Previous engine throttle-ability ...

    SBIRPhase I2015National Aeronautics and Space Administration
  2. High Speed Compressor for Subcooling Propellants

    Amount: $749,881.00

    The most promising propellant subcooling systems for LH2 require compression systems that involve development of significant head. The inlet pressure for these systems is typically on the order of 1 ...

    SBIRPhase II2014National Aeronautics and Space Administration
  3. High Speed Compressor for Subcooling Propellants

    Amount: $124,974.00

    Propellant densification systems for LH2 require compression systems that develop significant head. In the past this has required multiple stages of compressors running at high speed on grease-packed ...

    SBIRPhase I2013National Aeronautics and Space Administration
  4. High Seed Compressor for Propellant Densification

    Amount: $99,814.00

    Propellant densification systems particularly for H2 require compression systems developing very large amounts of head. Development of this head requires multiple stages of compressors running at hig ...

    SBIRPhase I2011National Aeronautics and Space Administration
  5. Turbine Component Rapid Manufacturing via Electron Beam Melting/Electrochemical Machining

    Amount: $149,366.00

    Development of new, more efficient gas turbine engines is a lengthy process of engine test iterations to maximize performance. This engine development cycle time is driven to a large extent by the man ...

    SBIRPhase I2011Department of Energy
  6. Thermal Conversion Device for Hydrothermal Vents

    Amount: $79,962.00

    The objective of this proposal is to develop technology which will enable electricity to be produced and stored by utilizing geothermal energy emanating from the fissures in the bottom of the ocean. G ...

    SBIRPhase I2011Department of Defense Navy
  7. Parallel Operation of Compact, Efficient Turbogenerators for Robust Tactical Energy Independence

    Amount: $99,956.00

    The intent of this project is to explore the feasibility of using a parallel connection strategy similar to a utility solution for the operation of multiple high speed turbo-generators in the 10 to 50 ...

    SBIRPhase I2010Department of Defense Air Force
  8. Development of Advanced Compact Energy Recovery Pumping System for Shipboard Seawater Reverse Osmosis Desalination

    Amount: $69,445.00

    The proposed advanced, compact, lightweight turbine-pump (ACLTP) assembly takes advantage of the available pressure in the overboard RO seawater stream via hydraulic Turbine expansion which provides a ...

    SBIRPhase I2010Navy Department of Defense
  9. Turbopump Design for Deep Throttling Capability

    Amount: $599,989.00

    This project will demonstrate the benefits of a partial emission pump coupled with a zero net positive suction pressure inducer design to achieve robust, deep throttling capability. This pump applica ...

    STTRPhase II2009National Aeronautics and Space Administration
  10. High Speed Compact Vaneaxial Fans

    Amount: $99,032.00

    Barber-Nichols will be using state-of-the art aerodynamic and acoustic design and optimization tools to improve the efficiency and acoustic signature of a current cooling fan design. The efficiency a ...

    SBIRPhase I2009Department of Defense Navy

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