METHOD TO LAUNCH MICRO-AND NANO-SATELLITES AND DEVICE BASED ON MICROPROCESSOR INDUCTIVE SYSTEM FOR LAUNCHING Russian patent published in 2016 - IPC B64G1/00 

FIELD: space.

SUBSTANCE: group of inventions relates to space engineering. Method to launch micro-and nano-satellites consists in the fact that after installation of launched satellite with single-axle gyro on a base and after selection by means of electromechanical system of specified direction orientation gyro run-up and launching of a device is carried out. Electromechanical part of microprocessor inductive launching system contains mechanisms of rotation of launching baseplate in azimuthal and zenith directions, driven by step motors controlled by commands of the microprocessor. For generation of mechanical launching pulse there is a solenoid placed in the working gap of the magnetic system. Electromechanical system also comprises electromagnet, fixing satellite with single-axle gyro installed on its lower base. Microprocessor of launching system disconnects electromagnet in the moment of separation.

EFFECT: technical result of group of inventions is providing controlled launching and micro-satellites with preservation of orientation in space relative to the main axis of separated apparatus.

4 cl, 2 dwg