Control and digital telemetry arrangement for an aerial missile

Details Control and digital telemetry arrangement for an aerial missile Control and digital telemetry arrangement for an aerial missile

1990-04-04

1994-02-01

Gregory, Bernarr E.

Communications: electrical

Continuously variable indicating

Combined

375 25, 102374, 244 314, 244 319, H04Q 900

Patent

active

H00012882

ABSTRACT:
A control and digital telemetry arrangement for an aerial missile includes digital telemetry system, a firing circuit, a battery and a latching relay. The digital telemetry system receives an analog input telemetry signal and produces and transmits to a ground station a digital output telemetry signal representing the current status of missile functions. The firing circuit is connected to the telemetry system to indicate that a firing command signal for firing the missile rocket motor has been received. The battery is capable of being switched back and forth between non-conducting and conducting states. The latching relay is connected between the telemetry system and battery and the system and external ground power and capable of switching the battery from its non-conductive to conductive state for latching power from the battery to said telemetry system. The digital telemetry system, firing circuit, battery and latching relay are packaged in a cannister housing which, in turn, is mountable in the missile.

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