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Title: Photovoltaic module start-up for the International Space Station

Conference ·
OSTI ID:474442
;  [1]
  1. Rockwell International, Canoga Park, CA (United States). Rocketdyne Div.

The International Space Station (ISS) US On-Orbit Segment Electric Power System (EPS) uses four photovoltaic modules (PVMs). Each PVM consists of solar array wings (SAW) for converting solar flux to electric power, nickel-hydrogen batteries for electric energy storage, electronic boxes for electric voltage control and power switching, and a thermal control system (TCS) for maintaining selected PVM components within their normal operating temperature ranges. Each PVM consists of two independent power channels, which are started sequentially. The start-up consists of deploying the SAW and photovoltaic radiator (PVR), initialization and check out of all hardware, thermally conditioning batteries, and charging batteries. After start-up, each PVM power channel is able to generate, store, and distribute electric power to ISS loads. Electric power to support start-up of the first PVM is provided by the NSTS via two auxiliary power converter units (APCUs), one per channel. During sunlit periods, the SAW provides power for the battery heaters (for thermal conditioning, as needed) and battery charging. During eclipse periods, the APCU maintains the channel in a standby mode. After start-up is complete, the APCU is disconnected and the PVM operates independently. The process used to start-up the first PVM on the ISS is described in this paper. Procedures used to bring dormant batteries to their normal operating temperature range and then to charge them to 100% state of charge (SOC) are also described. Total time required to complete start-up and the APCU power required during start-up are computed and compared to the requirements.

OSTI ID:
474442
Report Number(s):
CONF-960805-; TRN: IM9723%%335
Resource Relation:
Conference: 31. intersociety energy conversion engineering conference, Washington, DC (United States), 9-14 Aug 1996; Other Information: PBD: 1996; Related Information: Is Part Of Proceedings of the 31. intersociety energy conversion engineering conference. Volume 1: Aerospace power systems, aerospace technologies; Chetty, P.R.K.; Jackson, W.D.; Dicks, E.B. [eds.]; PB: 681 p.
Country of Publication:
United States
Language:
English