Total Capability Contracting for a Flight Critical Structure

Abstract

COMPONENTS using aluminium skins, ribs and honeycomb or graphite/epoxy and Nomex honeycomb bonded into an assembly, have been manufactured for some years. Major aircraft companies queried the use of honeycombs and expressed the need for other techniques to be developed.

Citation

Wardrop, D.J. and Allanson, R.M. (1990), "Total Capability Contracting for a Flight Critical Structure", Aircraft Engineering and Aerospace Technology, Vol. 62 No. 9, pp. 10-12. https://doi.org/10.1108/eb036990