FIELD: space equipment.
SUBSTANCE: invention relates to space engineering, and more specifically to means of protecting space objects. Proposed device comprises n pressure sensors installed inside m of object hardware, onboard computing machine (OBDC) and standard telemetry system. Device further comprises in-series connected first switch, narrow-band amplifier, demodulator and threshold unit. Each housing of object equipment includes controlled source of gas. Control inputs of the first, second and third switches, power supply, narrow-band amplifier and threshold unit and output of threshold unit are connected to OBDC. Narrow-band amplifier has control over amplification. Power supply is made with control over connection and voltage level. Threshold unit is controlled by threshold.
EFFECT: higher durability of space objects.
1 cl, 2 dwg
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Authors
Dates
2020-10-28—Published
2020-03-25—Filed