Large Scale Composite Manufacturing for Heavy Lift Launch VehiclesRisk reduction for the large scale composite manufacturing is an important goal to produce light weight components for heavy lift launch vehicles. NASA and an industry team successfully employed a building block approach using low-cost Automated Tape Layup (ATL) of autoclave and Out-of-Autoclave (OoA) prepregs. Several large, curved sandwich panels were fabricated at HITCO Carbon Composites. The aluminum honeycomb core sandwich panels are segments of a 1/16th arc from a 10 meter cylindrical barrel. Lessons learned highlight the manufacturing challenges required to produce light weight composite structures such as fairings for heavy lift launch vehicles.
Document ID
20150007663
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Stavana, Jacob (HITCO Carbon Composites, Inc. Gardena, CA, United States)
Cohen, Leslie J. (HITCO Carbon Composites, Inc. Gardena, CA, United States)
Houseal, Keth (HITCO Carbon Composites, Inc. Gardena, CA, United States)
Pelham, Larry (NASA Marshall Space Flight Center Huntsville, AL, United States)
Lort, Richard (Smith (B. G.) and Associates, Inc. Huntsville, AL, United States)
Zimmerman, Thomas (Smith (B. G.) and Associates, Inc. Huntsville, AL, United States)
Sutter, James (NASA Glenn Research Center Cleveland, OH, United States)
Western, Mike (Janicki Industries Secro Wooley, CA, United States)
Harper, Robert (Mag-IAS, LLC Hebron, KY, United States)
Stuart, Michael (Cytec Industries, Inc. Anaheim, CA, )
Date Acquired
May 7, 2015
Publication Date
May 21, 2012
Subject Category
Composite MaterialsMechanical Engineering
Report/Patent Number
E-664015Report Number: E-664015
Meeting Information
Meeting: SAMPE 2012 Conference and Exhibition
Location: Baltimore, MD
Country: United States
Start Date: May 21, 2012
End Date: May 24, 2012
Sponsors: Society for the Advancement of Materials and Process Engineering