BOEING COMPANY, THE
Task Order completed 12/16/2010. This effort is aimed at developing next-generation composite damage-arrest design principles that would be applicable to either a conventional tube-and-wing or a hybrid wing body aircraft, using the PRSEUS structural concept. The Contarctor shall design, analyze, and fabricate a curved panel with a 90 inch radius. The panel fabricated under this task order will be tested to failure at the FAA FASTER (Full-scale Aircraft Structure Test Evaluation and Research) facility after the expiration of this task order.