A window assembly and method for its installation is provided. The window assembly may include multiple transparent panels covering an opening of an aircraft fuselage. One or more retainer members and a flexible clip member may be utilized to secure the window assembly over the opening of the fuselage.

 
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< System and method for internal passive cooling of composite structures

> Integral frame member for an aircraft

> Method of controlling the attitude of satellites, particularly agile satellites with a reduced number of gyrodynes

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