Distributed electrical power system for modular spacecraft

Electrical transmission or interconnection systems – Vehicle mounted systems

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244173, 307 18, H02J 400

Patent

active

057985740

ABSTRACT:
A spacecraft avionics module having a selected degree of electrical power independence from a core spacecraft structure to which the module is attached. The module of the invention includes at least a power regulator and converter function. Other embodiments of the invention also include an energy storage device and a power generator on the module itself, for complete decentralization of electrical power management for the spacecraft.

REFERENCES:
patent: 4494063 (1985-01-01), Callen et al.
patent: 4654846 (1987-03-01), Goodwin et al.
patent: 4659942 (1987-04-01), Volp
patent: 4794272 (1988-12-01), Bavaro

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