Woven fiberglass fluted-core simulated aircraft interior panels were flame tested and structurally evaluated against the Boeing 747 present baseline interior panels. The NASA-defined panels, though inferior on a strength-to-weight basis, showed better structural integrity after flame testing, due to the woven fiberglass structure.
Evaluation of Materials and Concepts for Aircraft Fire Protection
1976-04-01
Report
No indication
English
Airport and aircraft fire protection
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