Abstract: A system and method for automatically configuring a component, such as an MCC cell), of the system includes the component, which further includes a module having storage, and a data concentrator device that is in communication with the component. The data concentrator device is in communication with a database, which may be a local ID database or a master ID database. The module stores a unique configuration code that is provided to the data concentrator device. The data concentrator device determines whether the database stores configuration information for the module that corresponds to the unique configuration code. The data concentrator device accesses the configuration information and uses it to automatically configure the component.

Abstract: A system includes a number of components; and a processor comprising a display, a program and a text file. The processor is structured to cause the display to display an initial overview display page operatively associated with the number of components. The processor is further structured to execute the program and cause the display to display a subsequent overview display page operatively associated with the number of components based upon the text file.

Abstract: A system automatically configures a component of the system from a database operatively associated with the system. The system includes a number of components, each having a module with a unique configuration code and a first communication interface, and a processor. The processor includes a second communication interface structured to communicate with the first communication interface, an interface to the database, and a routine structured to input the unique configuration code from the module, determine if the unique configuration code is in the database, and responsively input configuration information from the database and automatically configure a corresponding one of the number of components with the configuration information.

Abstract: A motor control centre is provided having an analyst system which is capable of recording data from the monitoring equipment provided therein, and providing a predictive analysis of the data received. The predictive analysis allows the operator to have the ability to schedule routine maintenance to correct a predicted failure of a device to continue operation within a pre-determined set of parameters. Improved operation and maintenance of a controlled system is achieved.

Abstract: A material which has two reactive groups, one of which is reactive with the irst of two dissimilar polymeric materials but not the second and the other of which is reactive with the second but not the first, is utilized to bind layers of the two polymeric materials together. The groups that are reactive with the first polymeric material are reacted with it as a layer of that material cures. Then a layer of the uncured second polymeric material is placed on the first and the groups that are reactive with it are reacted with it as it cures.

Abstract: An elastomeric or rigid polymeric material, such as a propellant, is strongly bonded to an incompatible material, such as a silicon rubber liner, when a long chain polymer which is insoluble in and unreactive with the liner but has groups reactive with the propellant is added to the liquid or uncured liner. As the liner cures, the polymer chain migrates to the surface. Upon laying the propellant on the surface and curing the propellant, the propellant is cross-linked to the long chain polymer, which is entangled in the rubber liner.

Abstract: A barrier layer made up of a suitable powder interspersed within either a trix of cured propellant binder or a matrix of silicone rubber is interposed between a silicone rubber insulator and a solid propellant grain in a rocket motor to prevent curatives from migrating from the propellant into the silicone rubber layer when the propellant is cast.

Abstract: Compositions consisting essentially of about 1 weight percent carbon black, rom about 20 to about 35 weight percent polytetrafluoroethylene and from about 79 to about 64 weight percent of a material selected from the group consisting of isobutylene-isoprene copolymer and ethylene-propylene rubber are disclosed as being useful as protective fillers in situations where the protective filler is subjected to high temperatures and pressures.

Abstract: A rocket motor is described in which a thin layer of metallic foil or the ke is used between a silicone rubber insulator and an isocyanate cured, hydroxy terminated polybutadiene bound propellant grain to prevent migration of isocyanate into the silicone rubber liner.

Abstract: An inhibitor for double-base propellant consisting essentially of a layer Saran or polystyrene bonded to the propellant grain by means of a block copolymer containing vinyl chloride-vinylidene chloride blocks or polystyrene blocks and polyurethane blocks.