FIELD: instrument industry.
SUBSTANCE: device comprises two spheres mounted with a spaced relation one to the other. The outer sphere is made of a superconducting material, and the inner sphere is made of a magnetic material. The outer sphere is secured to the spacecraft, and the inner sphere is shifted with respect to the center of gravity and has the radiation source. The output of the radiation receiving unit is connected with the information input of the recording unit whose control input is connected with the output of the board control unit.
EFFECT: simplified structure.
5 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| EXPERIMENTAL INFORMATION SPACE SYSTEM AND METHOD OF ITS OPERATION | 2000 |
|
RU2180642C1 |
| SPACE ACCELEROMETER | 2019 |
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| GRAVIMETER | 0 |
|
SU881643A1 |
| SPACECRAFT FOR CALIBRATING RADAR STATIONS | 2015 |
|
RU2596194C1 |
| METHOD OF CONTROLLING MOVEMENT OF SPACECRAFT WITH CONTROLLED ORIENTATION | 2020 |
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| FACILITY TO SHIELD MAGNETOMETERS FROM MAGNETIC FIELDS OF SPACECRAFT AND OTHER OBJECTS | 2001 |
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RU2204151C2 |
| SPACESCRAFT POWER SUPPLY CONTROL METHOD AND SYSTEM TO THIS END | 2009 |
|
RU2411163C1 |
| METHOD OF CONTROL OF SPACECRAFT POWER SUPPLY SYSTEM | 2005 |
|
RU2291819C2 |
| SUPERCONDUCTIVE RECEIVER OF HEAT RADIATION | 0 |
|
SU807938A1 |
