FIELD: astronautics.
SUBSTANCE: invention relates to telemetry sensors of spacecraft mechanical devices, in particular to devices for actuating limit switch contacts, namely, to devices actuating in final or other preset position on path of any body, and can be used as element of mechanical device at operation of telemetering sensor of spacecraft. Pressure device comprises bracket (1), on which end sensor (2) is fixed. Pressure plate (3) is installed perpendicular to direction of button (5) of end sensor (2) with possibility of free rotation in its side around axis (4).
EFFECT: technical result is higher reliability of operation of telemetric sensors of spacecrafts, as well as provision of guaranteed operation of end sensor under conditions of high errors, mutual arrangement of pressure element and sensor when it is actuated and at critical angle of approach to each other.
1 cl, 2 dwg
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Authors
Dates
2020-10-01—Published
2019-12-20—Filed