NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Improved compression molding technology for continuous fiber reinforced composite laminates. Part 2: AS-4/Polyimidesulfone prepreg systemAS-4/polyimidesulfone (PISO2) composite prepreg was utilized for the improved compression molding technology investigation. This improved technique employed molding stops which advantageously facilitate the escape of volatile by-products during the B-stage curing step, and effectively minimize the neutralization of the consolidating pressure by intimate interply fiber-fiber contact within the laminate in the subsequent molding cycle. Without the modifying the resin matrix properties, composite panels with both unidirectional and angled plies with outstanding C-scans and mechanical properties were successfully molded using moderate molding conditions, i.e., 660 F and 500 psi, using this technique. The size of the panels molded were up to 6.00 x 6.00 x 0.07 in. A consolidation theory was proposed for the understanding and advancement of the processing science. Processing parameters such as vacuum, pressure cycle design, prepreg quality, etc. were explored.
Document ID
19920001989
Acquisition Source
Legacy CDMS
Document Type
Technical Memorandum (TM)
Authors
Baucom, Robert M.
(NASA Langley Research Center Hampton, VA, United States)
Hou, Tan-Hung
(NASA Langley Research Center Hampton, VA, United States)
Kidder, Paul W.
(NASA Langley Research Center Hampton, VA, United States)
Reddy, Rakasi M.
(Old Dominion Univ. Norfolk, VA., United States)
Date Acquired
September 6, 2013
Publication Date
October 1, 1991
Subject Category
Nonmetallic Materials
Report/Patent Number
NAS 1.15:104133
NASA-TM-104133
Report Number: NAS 1.15:104133
Report Number: NASA-TM-104133
Accession Number
92N11207
Funding Number(s)
CONTRACT_GRANT: NAG1-569
PROJECT: RTOP 510-02-11
CONTRACT_GRANT: NAS1-19000
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available