FIELD: astronautics.
SUBSTANCE: invention relates to modular structures of spacecrafts, mainly, small spacecraft of various purpose. Platform is made on the basis of the load bearing structure of the housing (LBSH) in the form of posts. Inside the LBSH there is a propulsion unit with a tank (tanks) of the working body and a correction motor. Instrument compartment (IC), inside which service systems are installed, and outside – solar battery wings, is mounted at LBSH. IC consists of basic and modified modules. Earth remote sensing or communication earthing spacecraft can be created based on the above. All modules are made from honeycomb panels, which together form IC housing. Each module separately is a service system having its own set of on-board cable network, mechanical, electrical and other typical elements.
EFFECT: technical result is aimed at improving reliability, manufacturability and universality of spacecraft.
12 cl, 8 dwg
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Authors
Dates
2019-04-15—Published
2018-05-25—Filed