You are here

Manufacturing and Strength Improvement for Thick Carbon-Carbon Laminates

Award Information
Agency: Department of Defense
Branch: Defense Advanced Research Projects Agency
Contract: W911NF-15-C-0012
Agency Tracking Number: D2-1381
Amount: $1,498,915.00
Phase: Phase II
Program: SBIR
Solicitation Topic Code: SB133-005
Solicitation Number: 2013.3
Timeline
Solicitation Year: 2014
Award Year: 2015
Award Start Date (Proposal Award Date): 2015-01-06
Award End Date (Contract End Date): 2017-01-08
Small Business Information
209 Puente Ave.
City of Industry, CA 91746
United States
DUNS: 026249487
HUBZone Owned: No
Woman Owned: No
Socially and Economically Disadvantaged: No
Principal Investigator
 Wei Shih
 (626) 369-1273
 wei.shih@allcomp.net
Business Contact
 Mr. Wei Shih
Phone: (626) 369-1273
Email: weishih@aol.com
Research Institution
N/A
Abstract

The aerospace community has recently been successful in making complex large scale, hot structure carbon-carbon (C-C) assemblies for high speed aerospace vehicles. However, lessons learned from these programs revealed many issues that need to be overcome in order to further improve the design margins and to reduce performance risks for future applications.The overall objective of the program is to improve the strength and consistency of thick C-C laminates used on large scale, load bearing airframe structures. With strength properties as the focus of improvements, improved properties will give more analytical confidence during the design phase of programs.In this program, we propose to leverage our past experiences and to develop new class of C-C composites that meet the overall objective of the program. Test panels and demonstration article, aiming to achieve improved properties, will be designed, fabricated and then tested to check property improvement, property consistency and materials affordability in cost and lead time.

* Information listed above is at the time of submission. *

US Flag An Official Website of the United States Government