Abstract: An initiation fitting (10) includes a sleeve member (12) having a first end to which a fuse (18) or other initiator is connected and a second end to which an initiating charge (38) is connected for initiating a connected device such as a rocket motor and to hinder the venting of gases from the device through the fitting (10). The sleeve member (10) includes an internal passage (14) extending therethrough and a malleable internal flange (48) which protrudes into the internal passage (14). The internal flange (48) is dimensioned and configured so that when the initiating charge (38) detonates, the internal flange (48) collapses into the internal passage (14) to hinder the flow therethrough of explosive gases from the second end of the fitting.

Abstract: An igniter (18) provides rapid longitudinal and radial propagation of the ignition reaction. The igniter may comprise a pyrotechnic material and an inorganic binder, such as silica, carried on a carrier web (10) which may be fiber-glass. One or more layers of coated web (10) are disposed to provide an igniter (18) of cylindrical configuration and having a hollow core. The coated layers are permeable to the ignition reaction to facilitate radial propagation of ignition. The hollow core and the continuous nature of the pyrotechnic layers promotes longitudinal propagation of ignition. The igniter may consist mostly or entirely of inorganic materials to reduce or eliminate the formation of carbon monoxide upon ignition, and may be contained within a radially perforated sheath (20) to form a radial ignition device (25).