Stratos Flap Test

Stratos Aircraft have successfully completed the flap structural test to prove safety of flight for the prototype. The flap, while attached to the back of the wing, was taken to 1.2 times limit load and the wing box, attachments, flap and vane carried the load with no adverse effects and no noise from the aircraft structure. The lightweight flap and vane are damage tolerance carbon fiber laminate structure developed by Abbott Aerospace Inc., integrated with the flap system developed in house by Stratos.

Congratulations to the Stratos Team on the successful completion of another important program milestone.

http://www.stratosaircraft.com/


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Stratos Flap Test

Stratos Aircraft have successfully completed the flap structural test to prove safety of flight for the prototype. The flap, while attached to the back of the wing, was taken to 1.2 times limit load and the wing box, attachments, flap and vane carried the load with no adverse effects and no noise from the aircraft structure. The lightweight flap and vane are damage tolerance carbon fiber laminate structure developed by Abbott Aerospace Inc., integrated with the flap system developed in house by Stratos.

Congratulations to the Stratos Team on the successful completion of another important program milestone.

http://www.stratosaircraft.com/


AA SEZC Banner #6

To try our free Stress Analysis Engineering Spreadsheets click below

FREE ANALYSIS SPREADSHEETS 3

To try our Add-in for Microsoft Excel for Windows click below

XL-Viking 2

Comment On This Post

Your email address will not be published. Required fields are marked *