FIELD: spacecraft power supply systems on base of solar batteries.
SUBSTANCE: proposed spacecraft has form of right-angle prism with cross-section in form of equilateral tetragon (rhomb). Mounted on side faces of prism are solar battery panels. Spacecraft is provided with passive or combined system of gravitational stabilization in orbit. Acute angle of tetragon ranges from 50 to 90° to ensure required power supply for spacecraft equipment. Main central axes of symmetry of spacecraft in transversal plane are parallel to tetragon diagonal. Lesser axis is parallel to larger diagonal, thus enhancing stable gravitational orientation of spacecraft by larger diagonal perpendicularly to orbit axis.
EFFECT: enhanced efficiency.
3 dwg
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