NASA STTR 2018-I Solicitation

Proposal Summary


PROPOSAL NUMBER:
 18-1- T12.01-1662
SUBTOPIC TITLE:
 Thin-Ply Composite Technology and Applications
PROPOSAL TITLE:
 Automated Fiber Placement of Thin-Ply Composite Materials for Large Aerospace Structures
SMALL BUSINESS CONCERN (SBC):
RESEARCH INSTITUTION (RI):
Name:   NextGen Materials & Processing, LLC
Name:   University of Massachusetts Lowell
Street:  31 Wells Drive
Street:  600 Suffolk Street, Suite 212
City:   Tewksbury
City:   Lowell
State/Zip:  MA  01876-3637
State/Zip:   MA 01854 - 3643
Phone:  (978) 604-1660
Phone:   (978) 934-4170


Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Christopher Hansen
christopher_hansen@uml.edu
1 University Ave Lowell, MA 01854 - 3931
(978) 934-2932

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Konstantine Fetfatsidis
kfetfatsidis@nextgenmp.com
31 Wells Drive Tewksbury, MA 01876 - 3637
(978) 604-1660
Estimated Technology Readiness Level (TRL) :
Begin: 4
End: 5
Technical Abstract

Leveraging their prior experience working with automated fiber placement (AFP) of thin-ply composite materials, NextGen Materials & Processing LLC and the University of Massachusetts Lowell will utilize a Design of Experiments approach, combined with analytical modeling, to identify the critical material, slitting, spooling, and AFP parameters that influence the repeatable, high quality laydown of thin-ply composite materials to produce large aerospace structures. To date, long and costly certification processes have hindered the widespread adoption and exploitation of the benefits of thin-ply composites with AFP. Without critical end-user feedback, material manufacturers haven’t fully developed their thin-ply material systems with the same repeatability, consistency, and quality of standard-ply-thickness composites. Thus, further process development is necessary to optimize thin-ply unidirectional tapes for AFP. Working closely with Hexcel, the NextGen/UMass Lowell team will develop AFP-optimized conditions for a thin-ply version of the IM7 carbon fiber/8552-1 epoxy prepreg system, independent of different types of AFP machines. Using this material in conjunction with AFP, mechanical test coupons will be fabricated and tested to produce data for contribution to the development of the design and qualification database for thin-ply composite materials that will accelerate the adoption of these materials in structural applications.

Potential NASA Applications

This program will lead to more efficient AFP processing of thin-ply composite materials, enabling various manufacturing applications for NASA including aerostructures requiring high structural efficiency, and lightweight deep-space exploration structures such as pressurized habitation systems and tanks. Having the ability to manufacture cost-efficiently will also enable low-mass high stiffness deployable structures that can be packaged efficiently during launch (via folding/rolling).

Potential Non-NASA Applications

Non-NASA commercial applications of AFP of thin-ply materials include commercial rockets requiring advancements in materials and processing technologies to reduce cost, weight, and improve structural performance. Non-space applications include UAVs staying aloft for long durations to provide internet to remote global regions. Supersonic and hypersonic aircraft can be manufactured with reduced lifecycle costs due to the improved damage tolerance and reduction in repair and maintenance activity.


Form Generated on 05/25/2018 11:56:28