Accudyne Systems Inc

Basic Information

210 Executive Dr
Newark, DE, -

http://accudyne.com

Company Profile

n/a

Additional Details

Field Value
DUNS: 960998474
Hubzone Owned: N
Socially and Economically Disadvantaged: N
Woman Owned: N
Number of Employees: 30


  1. Automation of Material Placement for Aircraft Radomes

    Amount: $142,883.00

    ABSTRACT: Accudyne proposes a SBIR program to develop an automated material placement process for aircraft radomes and demonstrate it by forming quartz cynate ester fabric over an existing radome too ...

    SBIR Phase I 2012 Department of Defense Air Force
  2. Innovative Approaches to the Fabrication of Composite Rotary Wing Main Rotor Blade Spars with Option

    Amount: $1,087,160.00

    Sponsored by NAVAIR, Accudyne Systems completed a Phase 1 SBIR program, developing an equipment and process concept for cost-effective fabrication of composite rotary wing main rotor blade spars. The ...

    SBIR Phase II 2010 Department of Defense Navy
  3. Generating Autoclave-Level Mechanical Properties with Out-of-Autoclave Thermoplastic Placement of Large Composite Aerospace Structures

    Amount: $599,487.00

    While in the 1970's and 1980's, composites were adopted for aerospace structure for increased performance and weight savings, the 1990's and 2000's witnessed the attention towards cost-effective fabri ...

    STTR Phase II 2009 National Aeronautics and Space Administration
  4. Innovative Low-cost, In-situ Consolidation Head for Complex Geometry Thermoplastic Fiber Placement

    Amount: $79,924.00

    Accudyne proposes a SBIR program, endorsed by Sikorsky, Cytec Engineered Materials, and NASA-LaRC, to develop a cost-effective thermoplastic automated tow placement (ATP) process and demonstrate it by ...

    SBIR Phase I 2008 Navy Department of Defense
  5. Innovative Approaches to the Fabrication of Composite Rotary Wing Main Rotor Blade Spars

    Amount: $67,823.00

    This proposal will supply to NAVAIR and to rotorcraft manufacturing companies the emerging solution to their fabrication needs as it relates to the production of Rotor Blade Spars. The process and mac ...

    SBIR Phase I 2008 Navy Department of Defense
  6. Generating Autoclave-Level Mechanical Properties with Out-of-Autoclave Thermoplastic Placement of Large Composite Aerospace Structures

    Amount: $99,935.00

    Out-of-autoclave thermoplastic tape/tow placement (TP-ATP) is nearing commercialization but suffers a moderate gap in mechanical properties compared with laminates fabricated via thermoset autoclave p ...

    STTR Phase I 2008 National Aeronautics and Space Administration
  7. Heated Thermoplastic Fiber Placement Head for NASA Langley Research Center

    Amount: $600,000.00

    Reduced-mass polymer composite materials are crucial to the success of aerospace systems for reducing vehicle weight. But, composite material adoption is inhibited because the autoclave consolidation ...

    SBIR Phase II 2005 National Aeronautics and Space Administration
  8. Optimal Composite Materials using NASA Resins or POSS Nanoparticle Modifications for Low Cost Fabrication of Large Composite Aerospace Structures

    Amount: $68,204.00

    Reduced mass composite materials are crucial to the success of aerospace systems, but their adoption is inhibited because they require autoclave consolidation, a process that is prohibitively expensiv ...

    SBIR Phase I 2005 National Aeronautics and Space Administration
  9. Heated Thermoplastic Fiber Placement Head for NASA Langley Research Center

    Amount: $69,714.00

    Reduced mass composite materials are crucial to the success of aerospace systems, but are inhibited by expensive autoclave consolidation, especially for large parts. To remedy this, NASA-LaRC has bee ...

    SBIR Phase I 2004 National Aeronautics and Space Administration
  10. Cost Effective Processing Equipment for Large Composite Parts

    Amount: $598,755.00

    Reduced mass materials are critical to the success of aerospace systems. Thus, large air and space structures can benefit from lightweight composite materials. However, their adoption is impaired by t ...

    SBIR Phase II 2001 National Aeronautics and Space Administration

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