The SCS design is the core of overall spacecraft system design. It includes the design of distribution manager, EED and cable harness, grounding system, and interfaces between satellite (spacecraft) and rocket and between satellite (spacecraft) and ground. The SCS design is based on power and information topology of spacecraft load distribution, EED initiation, secondary power conversion, signal rate power, and information topology, as well as the interfaces with launch vehicle, ground test system, and other space subsystems.
Design of System Circuit Subsystem (SCS)
sp.
2020-08-15
42 pages
Article/Chapter (Book)
Electronic Resource
English
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