APPLIED POLERAMIC INCORPORATED

As the size of composite parts exceed that of even the largest autoclaves, new out-of-autoclave processes and materials are necessary to achieve the same level of performance as autoclave cured compos ...

As an alternative material to aluminum-lithium, cryotanks developed from fiber reinforced composites can offer significant weight savings in applications for fuel containment of liquid oxygen and hydr ...

As an alternative material to aluminum-lithium, cryotanks developed from fiber reinforced composites can offer significant weight savings in applications for fuel containment of liquid oxygen and hydr ...

Polymeric composite materials that are currently utilized in aircraft structures are susceptible to significant damage from lightning strikes. Enhanced electrical and thermal conductivity in these po ...

Composite parts on aircraft can be field repaired if the damage is small, using only vacuum and heat blankets or portable ovens. As alternative to using wet laminating resins and prepreg systems for ...

Composite aircraft structures can be damaged and require field repair to make operable and safe for flight. Field repairs have typically been accomplished using two-part liquid resin systems or prepr ...

In Phase I, a filament winding resin was developed that had a glass transition temperature of 274 C and could be processed at ambient temperature. This resin was characterized using existing filament ...

The Army desires to have a high temperature matrix for use in filament winding composites that can be easily processed at room temperature and has a minimum glass transition temperature of 260C (500F) ...

Future composite applications for Navy submarines and surface ships requires advanced polymeric matrices that have improved fire, smoke, and toxicity (FST) as compared to the present state of the art ...

N/A