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X-33 Tank Failure During Autoclave FabricationThe composite liquid hydrogen tank (tank #1 of 2) for the X-33 flight vehicle is made up of four lobes that have a sandwich construction, bonded to a frame of longerons. Lobes 1 and 4 showed local disbonds to the longerons they were bonded to. The 'bad' areas were cut away and patched with new material. The new material was cured by placing the entire tank in a heated autoclave with no pressure. Upon removal from the autoclave, it was noted that lobe 1 had severe skin/core disbonds on the inner and outer skins. The skins on this lobe were cracked as well. The core was disbonded from the inner skin across the entire acreage, except for spots around the lobe perimeter. The outer skin was separated from the core in a region near the center of the lobe. Lobe 1 was removed from the tank on January 13, 1999. Bolts were placed through the lobe to hold it together and the cuts on the inner skin were not continuous, but 'tabs' were left for final cutting and removal. Upon closer inspection of the disbonded basesheet, it was noted that there was a lack of filleting into the honeycomb core. Good fillets are critical to bond strength.
Document ID
20020021989
Acquisition Source
Marshall Space Flight Center
Document Type
Preprint (Draft being sent to journal)
Authors
Nettles, Alan T.
(NASA Marshall Space Flight Center Huntsville, AL United States)
Munafo, Paul
Date Acquired
September 7, 2013
Publication Date
January 1, 2001
Subject Category
Aircraft Design, Testing And Performance
Meeting Information
Meeting: Joint NASA/AF Meeting on Honeycomb Panels
Location: El Segundo, CA
Country: United States
Start Date: October 2, 2001
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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