Patent ID: 7284487

Claim:
An igniter for igniting a missile, the missile having a nozzle and a motor, said igniter being ejectably securable within the nozzle and comprising: a unitary, single-piece body having a first end and a second end, said ends being opposite from each other; a chamber within said body for holding therein pyrotechnic material; at least one initiator port on said first end and at least one output port on said second end, said ports communicating with said chamber; an initiator coupled to said initiator port, said initiator responding to electric current applied thereto to ignite said pyrotechnic material and producing pyrotechnic output, said output port passing therethrough said pyrotechnic output to ignite the motor; a plurality of flexible retaining fingers extending from said unitary body; and a plurality of cavities located on said body to allow said retaining fingers to recede thereinto while said igniter is being ejectably installed in said missile, said retaining fingers snapping out of said cavities to secure said igniter in place upon completion of installation.