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- Article name
- METHOD FOR SELECTING COMPONENTS FOR SPACECRAFT SYSTEMS
- Authors
- Shovkaluk A. P., , shovalex@yandex.ru, Moscow Aviation Institute (National Research University), Moscow, Russia
- Keywords
- spacecraft / consistency / set / rocket engine / relative comparison indicator / ranking
- Year
- 2020 Issue 4 Pages 37 - 41
- Code EDN
- Code DOI
- Abstract
- In this work, the process of designing a spacecraft (SC) is presented in the form of a multistage integration of elements and their properties into the system. The basis for achieving design solutions is the hierarchy of parameters of the component parts of the technical system. It has been determined that the final characteristics of the spacecraft being designed can be of two types: additive and partially additive. To select the components of the subsystems, complex indicators are used, calculated by summing the relative comparison indicators (OPS) of the parameters. The weight of the parameters is determined by ranking in accordance with the satellite optimization criteria.
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