FIELD: monitoring of radar and infra-red homing heads of rockets.
SUBSTANCE: the device has a target simulator, an indexing mechanism with a rotary platform and a transducer of the angle of its turn are installed on the table of the sine stand, the axis of rotation of the platform and the axis of oscillation of the table are aligned.
EFFECT: provided measurement of synchronous errors depending on the bearing.
1 dwg
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Authors
Dates
2006-06-27—Published
1970-11-20—Filed