The design and evaluation of built-up attachments and bonded joint concepts for use at elevated temperatures is documented. Joint concept screening, verification of GR/PI material, fabrication of design allowables panels, definition of test matrices, and analysis of bonded and bolted joints are among the tasks completed. The results provide data for the design and fabrication of lightly loaded components for advanced space transportation systems and high speed aircraft.
Design, fabrication and test of graphite/polyimide composite joints and attachments for advanced aerospace vehicles
1979-10-01
Report
No indication
English
Bonded and Bolted Graphite/Polyimide Composite Joints
NTRS | 1985
|High temperature polyimide foams for aerospace vehicles
Tema Archive | 1999
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