NASA STTR 2017-II Solicitation

Proposal Summary


PROPOSAL NUMBER:
 17-2- T12.02-9846
PHASE 1 CONTRACT NUMBER:
 NNX17CK09P
SUBTOPIC TITLE:
 Technologies to Enable Novel Composite Repair Methods
PROPOSAL TITLE:
 Efficient Composite Repair Methods for Launch Vehicles
SMALL BUSINESS CONCERN (SBC):
RESEARCH INSTITUTION (RI):
Name:   Luna Innovations, Inc.
Name:   Aerospace Federally Funded Research and Development Center
Street:  301 1st Street Southwest, Suite 200
Street:  2310 East El Segundo
City:   Roanoke
City:   El Segundo
State/Zip:  VA  24011-1921
State/Zip:   CA 90245 - 4609
Phone:  (540) 769-8400
Phone:   (310) 336-5233


Principal Investigator (Name, E-mail, Mail Address, City/State/Zip, Phone)
Dr. Daniel Metrey PhD
metreyd@lunainc.com
3155 State Street Blacksburg, VA 24060 - 6604
(540) 961-4509

Business Official (Name, E-mail, Mail Address, City/State/Zip, Phone)
Michael Pruzan
pruzanm@lunainc.com
301 1st Street Southwest, Suite 200 Roanoke, VA 24011 - 1921
(540) 769-8430
Estimated Technology Readiness Level (TRL) :
Begin: 4
End: 6
Technical Abstract

Polymer matrix composites are increasingly replacing traditional metallic materials in NASA launch vehicles due to high strength to weight ratio, manipulative properties, and corrosion resistance.  However, the inspection and repair methods for these materials are considerably more complicated.  For aerospace platform repairs, a composite laminate patch must be manually fabricated on-site and then bonded to the damaged structure.  Prior to the bonding or co-curing, a vacuum debulk process is performed on the lay-up, requiring a separate piece of support equipment. The ideal method would allow for a rapid structural repair to be performed in locations with minimal access without the need for extensive tooling, surface prep, cure times and complicated techniques. In Phase I, engineers at Luna demonstrated a comprehensive system that included facile surface preparation, single-bag out of autoclave processing and Luna’s unique fiber optic measurement capability for monitoring repair state. This Phase II program will focus on optimizing these methods for launch vehicle composite damage that can be performed during ground processing of the launch vehicle without the need for full replacement. It is expected that the technology will meet NASA launch vehicle requirements and demonstrate potential for in-situ repairs to spacecraft on long missions.

Potential NASA Applications

Luna’s composite repair system will be directly applicable to launch pad damage mitigation activities for current and future launch vehicles. Ground processing operators will be able to identify the damage that will require patching and Luna’s technology will enable rapid surface preparation, patch bonding, vacuum debulking and consolidation without the need for complicated tooling or equipment. This should dramatically reduce time and energy costs while maintaining high probabilities of mission success.

Potential Non-NASA Applications

Luna’s technology is applicable to a wide range of composite material systems, manufacturing methods, and applications. The barrier and curative approaches can be adapted to prepreg systems that would have prolonged room temperature storage capability with the ability to be quickly cured, out of autoclave and on-demand. The impact of these systems on the broad composite commercial market could be enormous.


Form Generated on 08/02/2018 17:10:53