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NASA NTRS · 19770053838

Fabrication of PDA/HTS prototype components

Abstract

A process was developed for autoclave molding structural poly-(Diels-Alder) polyimide (PDA) resin/HTS graphite composites for short-term 600 F service. The autoclave molding process used to fabricate these composites required a maximum cure temperature of 427 K (400 F) and a maximum molding pressure of 0.7 MN/sq m (100 psig). This process then was adapted to the fabrication of co-cured polyimide sandwich panels consisting of PDA/HTS skins, PDA syntactic foam and polyimide/glass honeycomb core. Fabrication ease was demonstrated by manufacturing five three-quarter scale YF-12 wing panels using the PDA resin. It was concluded from successful evaluation of these prototype units that the PDA resin is suitable for fabrication of components using commercial equipment.

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BibTeXRIS

Sheppard, C. H., Orell, M. K., Vaughan, R. W., Jones, R. J.. 1976-01-01. Fabrication of PDA/HTS prototype components. https://ntrs.nasa.gov/citations/19770053838

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