Abstract: A temporary control fin stop system employs a housing coupled to a vehicle. At least one tang is coupled to the housing and positioned to engage a trailing edge of a fin. The tang is ablatively erodible at a predetermined temperature induced by a flight profile of the vehicle to allow unconstrained motion of the fin.

Abstract: A temporary control fin stop system employs a housing coupled to a vehicle. At least one tang is coupled to the housing and positioned to engage a trailing edge of a fin. The tang is ablatively erodible at a predetermined temperature induced by a flight profile of the vehicle to allow unconstrained motion of the fin.

Abstract: A method for embedding piezoelectric ceramic transducers in thermoplastic composites. The piezoelectric ceramic transducer to be embedded in a graphite/PEEK composite is first bonded with two fine silver wires for electrical connection, one on each major surface. The bonding agent is a high temperature conductive adhesive compound, such as a silver/glass frit. The fusing of the frit bonding agent is done in an over at a high temperature (i.e. 600.degree. F. or higher) for 5 to 10 minutes. Bonds are applied at several discrete spots on the zig zag wire which relieves thermal stresses induced during cooling due to a mismatch of the coefficient of thermal expansion between the ceramic material and the wire. After the connecting wires are attached, the wires and transducer are wrapped with several plies of insulating glass/PEEK cloth to prevent electrical shorting between the two silver wires through the graphite/PEEK host.

Abstract: This invention consists of a method for embedding piezoelectric ceramic transducers in thermoplastic composites. The piezoelectric ceramic transducer to be embedded in a graphite/PEEK composite is first bonded with two fine silver wires for electrical connection, one on each major surface. The bonding agent is a high temperature conductive adhesive compound, such as a silver/glass frit. The fusing of the frit bonding agent is done in an over at, a high temperature (i.e. 600.degree. F. or higher) for 5 to 10 minutes. Bonds are applied at several discrete spots on the zig zag wire which relieves thermal stresses induced during cooling due to a mismatch of the coefficient of thermal expansion between the ceramic material and the wire. After the connecting wires are attached, the wires and transducer are wrapped with several plies of insulating glass/PEEK cloth to prevent electrical shorting between the two silver wires through the graphite/PEEK host.

Abstract: Viscoelastic constrained layer vibration damping composition having a shear storage modulus of 500.+-.100 psi consisting essentially of about 100 parts by weight of a butyl rubber having a glass transitional point temperature of -50 degrees F..+-.15 degrees, 100 parts by weight of a nitrile rubber having a glass transitional point temperature of 60 degrees F..+-.15 degrees, 50 parts by weight of a thermoplastic polymer having a glass transitional point temperature of 130 degrees F..+-.15 degrees, 45 parts by weight of a plasticizer, and 50 parts by weight of a powdered filler.