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. (Author)
Evaluation of Materials and Concepts for Aircraft Fire Protection
1976
38 pages
Report
No indication
English
Airport and aircraft fire protection
Engineering Index Backfile | 1946
|Aircraft Fire Protection Technology Applications
SAE Technical Papers | 1972
|