FIELD: space technology.
SUBSTANCE: invention relates to space technology and can be used to drive nanosatellites to specified trajectories and at specified speeds from the space station. Device for separating nanosatellites consists of an electromechanical trigger system of a magnetic induction type and an electronic control module. Device contains a high-current solenoid placed in the working gap of a system of permanent neodymium magnets consisting of a set of annular magnets and a coaxially installed neodymium cylindrical magnet enclosed in a casing made of a soft magnetic material. Solenoid is connected via a key device to the coil connected to the microprocessor. Control module plates are located in the vacuumized compartments, which allows long-term service in open space. Device contains an autonomous power supply system, consisting of batteries, solar panels and their charge controller, which is controlled by a microprocessor.
EFFECT: technical result is an increase in the kinetic energy at the start of the detachable apparatus.
3 cl, 2 dwg
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Authors
Dates
2018-05-11—Published
2016-08-23—Filed