Fuze data quantizing system

Measuring and testing – Instrument proving or calibrating – Volume of flow – speed of flow – volume rate of flow – or mass...

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Details

73167, 73489, G01M 1900

Patent

active

042803551

ABSTRACT:
The present invention discloses an in-flight testing of projectile and mor fuzes. A microminiature electronic circuitry in a cartridge form is designed to attach to any of the large caliber shell or mortar fuzes. The test-cartridge is a recoverable, reusable, high-g hardened device. The system for sampling and recording projectile fuzes during a period of target impact comprises: a power supply; a timing and control logic unit; an accelerometer; an amplitude encoder; a shift register; and an interface connector to transform stored information of the fuze functioning characteristics to a ground station readout unit.

REFERENCES:
patent: 2834293 (1958-05-01), Beach et al.
patent: 3761917 (1973-09-01), Brown et al.
patent: 4114450 (1978-09-01), Shulman et al.

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