257545-5

Guided missile rate sensing unit

257545-5 Description

AGM-65A maverick end item identification, used to sense the accelerations in the various axes of the missile during flight functional description.

Properties of 257545-5

End Application:
Agm-65a maverick
Functional Description:
Used to sense the accelerations in the various axes of the missile during flight
General Description:
Length 2.400 in. Max; outside diameter, min 1.182 in., max 1.186 in.; inside diameter, 0.939 in. Max
NSN:
1430-01-180-2070
Description:
Sensing Unit,rate,guided Missile
Cage Code:
82577

Definition Guided Missile Rate Sensing Unit

An item specifically designed to provide azimuth and elevation deviation rate information obtained by tracking a moving target. The electrical error voltages are used to provide corrective command signals to a guided missile in flight. Excludes accelerometer (as modified); gyroscope, rate; and moving target indicator group.

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Last modified 04/29/2024