FIELD: machine building.
SUBSTANCE: invention relates to machine building, particularly, to space platforms. Space platform (SP) comprises structural frame of housing (SFH) composed of mesh structure made of composite materials, on which instrument compartment is arranged. Note here that SFH ends protrude beyond plane of instrument compartment panels. On ends of SFH there are assembling units with separation system and payload, and inside SFH there are tanks for working body storage for engines of correction, orientation and stabilization systems. Instrument compartment is made of interconnected panels, and some of them are radiator panels. Instruments and equipment of onboard service systems are arranged inside and outside the instrument compartment. Outside on instrument compartment there are: engines of orientation and stabilization system, assemblies with payload, rotary wings of solar battery (SB), folded in start-up state, fixed symmetrically on two opposite sides of instrument compartment by means of rods to devices of rotation of wings of SB, at that wings of SB are made in the form of flat panels attached to each other. Besides, SP comprises engines providing completion of geostationary orbit arranged outside the instrument compartment and capable of changing its position.
EFFECT: higher platform power.
7 cl, 4 dwg
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Authors
Dates
2019-05-21—Published
2016-10-11—Filed