Development of a low-cost, modified resin transfer molding process using elastomeric tooling and automated preform fabricationThis paper describes the design and process development of low-cost structural parts made by a modified resin transfer molding process. Innovative application of elastomeric tooling to increase laminate fiber volume and automated forming of fiber preforms are discussed, as applied to fabrication of a representative section of a cruise missile fuselage.
Document ID
19950021847
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Doane, William J. (General Dynamics/Convair San Diego, CA, United States)
Hall, Ronald G. (General Dynamics/Convair San Diego, CA, United States)
Date Acquired
September 6, 2013
Publication Date
September 1, 1992
Publication Information
Publication: FAA, Ninth DOD(NASA)FAA Conference on Fibrous Composites in Structural Design, Volume 3