Space Power Volume 9 Numbers 2&3 1990

The validation items for this subsystem, which have also been put on hold because of funding shortfalls, are the high temperature electrical cable, the shunt power dissipator and the main bus load controller. Mechanical/Structural Subsystem This subsystem design was also completed for the system design review and the configuration, materials and components are shown in Fig. 28. The structural design is

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