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ACCUDYNE SYSTEMS, INC.
UEI: QLJLWGE4MHD4
# of Employees: 30
HUBZone Owned: No
Socially and Economically Disadvantaged: No
Woman Owned: No
Award Charts
Award Listing
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Automation of Material Placement for Aircraft Radomes
Amount: $142,883.00ABSTRACT: 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 ...
SBIRPhase I2012Department of Defense Air Force -
Innovative Approaches to the Fabrication of Composite Rotary Wing Main Rotor Blade Spars with Option
Amount: $1,087,160.00Sponsored 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 ...
SBIRPhase II2010Department of Defense Navy -
Generating Autoclave-Level Mechanical Properties with Out-of-Autoclave Thermoplastic Placement of Large Composite Aerospace Structures
Amount: $599,487.00While 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 ...
STTRPhase II2009National Aeronautics and Space Administration -
Innovative Low-cost, In-situ Consolidation Head for Complex Geometry Thermoplastic Fiber Placement
Amount: $79,924.00Accudyne 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 ...
SBIRPhase I2008Department of Defense Navy -
Innovative Approaches to the Fabrication of Composite Rotary Wing Main Rotor Blade Spars
Amount: $67,823.00This 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 ...
SBIRPhase I2008Department of Defense Navy -
Generating Autoclave-Level Mechanical Properties with Out-of-Autoclave Thermoplastic Placement of Large Composite Aerospace Structures
Amount: $99,935.00Out-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 ...
STTRPhase I2008National Aeronautics and Space Administration -
Heated Thermoplastic Fiber Placement Head for NASA Langley Research Center
Amount: $600,000.00Reduced-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 ...
SBIRPhase II2005National Aeronautics and Space Administration -
Optimal Composite Materials using NASA Resins or POSS Nanoparticle Modifications for Low Cost Fabrication of Large Composite Aerospace Structures
Amount: $68,204.00Reduced 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 ...
SBIRPhase I2005National Aeronautics and Space Administration -
Heated Thermoplastic Fiber Placement Head for NASA Langley Research Center
Amount: $69,714.00Reduced 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 ...
SBIRPhase I2004National Aeronautics and Space Administration -
Cost Effective Processing Equipment for Large Composite Parts
Amount: $598,755.00Reduced 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 ...
SBIRPhase II2001National Aeronautics and Space Administration
