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

Award Information
Agency:
National Aeronautics and Space Administration
Branch
n/a
Amount:
$598,247.00
Award Year:
2011
Program:
SBIR
Phase:
Phase II
Contract:
NNX11CA77C
Agency Tracking Number:
094612
Solicitation Year:
2009
Solicitation Topic Code:
X5.03
Solicitation Number:
n/a
Small Business Information
Applied Poleramic, Inc.
CA, Benicia, CA, 94510-1269
Hubzone Owned:
N
Socially and Economically Disadvantaged:
N
Woman Owned:
N
Duns:
787223460
Principal Investigator:
Brian Hayes
Principal Investigator
(707) 707-6738
hayesb1@sbcglobal.net
Business Contact:
Brian Hayes
Business Official
(707) 707-6738
hayesb1@sbcglobal.net
Research Institution:
Stub




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. Many of the new out-of-autoclave prepreg systems can be used to manufacture high quality composites initially but the lay-up time for producing quality parts is limited by the 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 possesses a year plus shelf-life while also providing an excellent balance of composite properties and damage tolerance. As an additional functionality, the out-of-autoclave prepreg system will be developed to have inherent skin-core self adhesive characteristics so that film adhesives may not be required for designs with honeycomb structures. It is expected that the TRL will be 6 at the end of this Phase 2 program.

* information listed above is at the time of submission.

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