FIELD: space.
SUBSTANCE: invention relates to space instrument-making and may be used for collection of data on parameters of movement of space objects such as particles of space garbage and micrometeoroids. Small spacecraft for detection of space garbage particles and micrometeoroids consists of metal-dielectric-metal film structure, electromagnets arranged in three mutually orthogonal axes, ion receiver, solar battery, at that each axis holds one electromagnet connected to control unit electromagnets, that is connected to the system control unit, additional components include the recording unit connected to the metal-dielectric-metal film structure of overhead-hood version and system control unit, power forming unit connected to solar battery and system control unit, receiving-transmitting module connected with command antenna, telemetric system control unit and antenna, a film sensor sweep unit connected to system control unit whereto connected are six solar sensors located on each of the faces of the small spacecraft.
EFFECT: technical result is reduction of target dimensions in unopened state.
1 cl, 4 dwg
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