Title :
Battery reinitialization on the photovoltaic module of the international space station
Author :
Hajela, G. ; Cohen, Fernand
Author_Institution :
Rocketdyne Power & Propulsion, Boeing Co., Canoga Park, CA, USA
Abstract :
The photovoltaic (PV) module on the International Space Station (ISS) has been operating since November 2000 and supporting electric power demands of the ISS and its crew of three. The PV module contains photovoltaic arrays that convert solar energy to electrical power, and an integrated equipment assembly (IEA) that houses electrical hardware and batteries for electric power regulation and storage. Each PV module contains two independent power channels for fault tolerance. Each power channel contains three batteries in parallel to meet its performance requirements and for fault tolerance. Each battery consists of 76 Ni-Hydrogen (Ni-H2) cells in series. These 76 cells are contained in two orbital replaceable units (ORU) that are connected in series. On-orbit data are monitored and trended to ensure that all hardware is operating normally. Review of on-orbit data showed that while five batteries are operating very well, one is showing signs of mismatched ORUs. The cell pressure in the two ORUs differs by an amount that exceeds the recommended range. The reason for this abnormal behavior may be that the two ORUs have different use history. An assessment was performed and it was determined that capacity of this battery would be limited by the lower pressure ORU. Steps are being taken to reduce this pressure differential before battery capacity drops to the point of affecting its ability to meet performance requirements. As a first step, a battery reinitialization procedure was developed to reduce this pressure differential. The procedure was successfully carried out on-orbit and the pressure differential was reduced to the recommended range. This paper describes the battery performance and the consequences of mismatched ORUs that make a battery. The paper also describes the reinitialization procedure, how it was performed on orbit and battery performance after the reinitialization. On-orbit data monitoring and trending is an ongoing activity and it will continue as ISS assembly progresses.
Keywords :
fault tolerance; hydrogen compounds; nickel compounds; photovoltaic power systems; secondary cells; solar cell arrays; space vehicle power plants; Ni-H2; battery performance; battery reinitialization; electric power demand; electric power regulation; electrical hardware; fault tolerance; integrated equipment; international space station; on-orbit data monitoring; orbital replaceable units; photovoltaic arrays; photovoltaic module; power channels; solar energy; Assembly; Batteries; Energy storage; Fault tolerance; Hardware; International Space Station; Monitoring; Photovoltaic systems; Solar energy; Solar power generation;
Conference_Titel :
Energy Conversion Engineering Conference, 2002. IECEC '02. 2002 37th Intersociety
Print_ISBN :
0-7803-7296-4
DOI :
10.1109/IECEC.2002.1391986