HyPerComp Engineering, Inc.

Basic Information

1080 North Main, Suite #2
Brigham City, UT, 84302 0505

Company Profile

n/a

Additional Details

Field Value
DUNS: 956327308
Hubzone Owned: Y
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 12


  1. The Cryogenic Impact Resistant Evaluation of Composite Materials for Use in Composite Pressure Vessels with an Additional Cryogenic Bonding Scope

    Amount: $599,754.00

    The intent of the proposed effort is to investigate the detailed composite material performance characteristics after being subjected to cryogenic temperatures and impact damage. HyPerComp Engineerin ...

    STTR Phase II 2007 National Aeronautics and Space Administration
  2. Defining the coupled effects of cryogenic, space-radiation, and hypervelocity impact damamge on COPV's

    Amount: $588,156.00

    The intent of the proposed effort is to investigate the detailed composite overwrapped pressure vessel (COPV) performance characteristics after being subject to irradiation, hypervelocity micro-meteor ...

    SBIR Phase II 2007 National Aeronautics and Space Administration
  3. Defining the coupled effects of cryogenic, space-radiation, and hypervelocity impact damamge on COPV's

    Amount: $69,956.00

    The objective of the research proposed herein is to define the coupled (combined) effect of critical environments on the structural performance of composite overwrap pressure vessels (COPV). The thre ...

    SBIR Phase I 2006 National Aeronautics and Space Administration
  4. The Cryogenic Impact Resistant Evaluation of Filament Wound Materials for Use in Composite Pressure Vessels

    Amount: $99,000.00

    HyPerComp Engineering Inc. (HEI) and Utah State University (USU) propose to develop technology for lightweight composite materials for use in composite structures suitable for both cryogenic and damag ...

    STTR Phase I 2006 National Aeronautics and Space Administration
  5. The Cyogenic Evaluation of Irradiated Composite Materials for Use in Composite Pressure Vessels

    Amount: $599,955.00

    HyPerComp Engineering, Inc. (HEI) proposes to continue the characterization of the cryogenic evaluation of irradiated composite materials for use in composite overwrap pressure vessels COPVs. The int ...

    STTR Phase II 2006 National Aeronautics and Space Administration
  6. To Ensure the Integrity of the Cryogenic Propellant Depot Tank Within the Expected Radiation and Space Debris Environment

    Amount: $50,000.00

    HyPerComp Engineering, Inc. (HEI) proposes to develop well characterized, structurally reliable filament wound composite pressure vessels for use in both cryogenic and radiation environment applicatio ...

    SBIR Phase II 2006 National Aeronautics and Space Administration
  7. To Ensure the Integrity of the Cryogenic Propellant Depot Tank Within the Expected Radiation and Space Debris Environment

    Amount: $69,396.00

    We intend to develop the technology for lightweight composite structure suitable for both cryogenic fuel depot storage as well as human in-space habitat. These will incorporate improved impact techno ...

    SBIR Phase I 2005 National Aeronautics and Space Administration
  8. The Cyogenic Evaluation of Irradiated Composite Materials for Use in Composite Pressure Vessels

    Amount: $99,584.00

    The intent of this proposal is to develop key building block technology for lightweight composite structures suitable for cryogenic fuel depot storage as well as human in-space habitat. The effort ...

    STTR Phase I 2005 National Aeronautics and Space Administration
  9. The cryogenic evaluation of typical and experimental filament winding materials

    Amount: $598,810.00

    HyPerComp Engineering, Inc. (HEI) proposes to develop well characterized, reliable filament wound composite pressure vessels for cryogenic and other low temperature applications. The proposed effort a ...

    SBIR Phase II 2004 National Aeronautics and Space Administration
  10. The cryogenic evaluation of typical and experimental filament winding materials

    Amount: $69,927.00

    HyPerComp Engineering proposes to conduct a series of material tests to evaluate the performance of standard and experimental filament winding materials in cryogenic pressure vessel applications. The ...

    SBIR Phase I 2003 National Aeronautics and Space Administration

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