Long Out-time, Out-of-Autoclave Cure Composites

Award Information
Agency:
National Aeronautics and Space Administration
Amount:
$99,248.00
Program:
SBIR
Contract:
NNX10CF32P
Solitcitation Year:
2009
Solicitation Number:
N/A
Branch:
N/A
Award Year:
2010
Phase:
Phase I
Agency Tracking Number:
094612
Solicitation Topic Code:
X5.03
Small Business Information
Applied Poleramic, Inc.
6166 Egret Court, Benicia, CA, 94510-1269
Hubzone Owned:
N
Woman Owned:
N
Socially and Economically Disadvantaged:
N
Duns:
787223460
Principal Investigator
 Brian Hayes
 Principal Investigator
 (707) 747-6738
 hayesb1@sbcglobal.net
Business Contact
 Doyle Dixon
Title: Vice President
Phone: (707) 747-6738
Email: poleramic@aol.com
Research Institution
N/A
Abstract
As the size of composite parts exceed that of even the largest autoclaves, new out-of-autoclave processes and materials are necessary to achieve the same level of performance as autoclave cured composites. Unfortunately, the quality of composites manufactured with current out-of-autoclave prepreg systems is limited by their short shelf-life at ambient conditions. The resin advancement, due to long lay-up times, commonly causes variations in fiber volume and higher void content in the cured structures. Also, current out-of-autoclave prepreg systems do not provide the same level of performance, especially damage tolerance, as many current autoclave cured prepreg systems. It is the objective of this work to develop a matrix and prepreg system for out-of-autoclave processing that has a year out-time at ambient conditions while also providing an excellent balance of mechanical properties and damage tolerance. As an additional functionality, the out-of-autoclave prepreg system will be developed to have inherent skin-core self-adhesive properties so that film adhesives are not required for designs with honeycomb cores. It is expected that the TRL will be 4 at the end of this Phase I program.

* information listed above is at the time of submission.

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