Title :
Life cycle testing of spaceflight qualified nickel-hydrogen battery cells
Author :
Francisco, Jennifer M. ; Fox, Christopher L. ; Cook, William D.
Author_Institution :
Technol. Div., Eagle-Picher Ind. Inc., Joplin, MO, USA
fDate :
27 Jul-1 Aug 1997
Abstract :
The nickel-hydrogen (Ni-H2) aerospace battery has become the advanced power storage system of choice for military and commercial satellite programs requiring high reliability, long-life and rugged, abuse-tolerant operation. This system is providing dependable eclipse and peak power to hundreds of Earth orbiting satellites as well as planetary spacecraft. These batteries have provided in excess of two hundred million successful operational cell-hours on-orbit. Due to the nature of the application, battery failure is not an option, therefore quality performance is of the utmost importance. In addition to the system´s extensive flight proven heritage, Ni-H2 batteries and battery cells have been subjected to many and varied life cycle tests. Both real-time (RT) and accelerated (ACC) tests in Low Earth Orbit (LEO) as well as Geosynchronous Orbit (GEO) test regimes have been performed and are represented. In some cases, these tests attempt to duplicate the on-orbit charge/discharge profile of the application as closely as possible, as well as testing extreme situations. This test database was originated in support of early Ni-H2 flight programs and has been consistently expanded over 15 years. In addition to the testing performed in-house, many life cycle tests are performed by our customer base as well as independent test laboratories. Several different Ni-H2 cell and battery designs are on test including Individual Pressure Vessel, Common Pressure Vessel, Single Pressure Vessel and Dependent Pressure Vessel
Keywords :
hydrogen; life testing; nickel; pressure vessels; secondary cells; space vehicle power plants; Common Pressure Vessel; Dependent Pressure Vessel; Earth orbiting satellites; Geosynchronous Orbit tests; Individual Pressure Vessel; Low Earth Orbit tests; Ni-H2; Ni-H2 aerospace battery; Single Pressure Vessel; accelerated tests; battery failure; commercial satellite programs; high reliability; life cycle testing; life cycle tests; long-life; military satellite programs; on-orbit charge/discharge profile; planetary spacecraft; power storage system; real-time tests; rugged abuse-tolerant operation; spaceflight qualified nickel-hydrogen battery cells; test database; varied life cycle tests; Aerospace testing; Batteries; Life testing; Low earth orbit satellites; Military satellites; Performance evaluation; Planetary orbits; Power system reliability; Space vehicles; System testing;
Conference_Titel :
Energy Conversion Engineering Conference, 1997. IECEC-97., Proceedings of the 32nd Intersociety
Conference_Location :
Honolulu, HI
Print_ISBN :
0-7803-4515-0
DOI :
10.1109/IECEC.1997.659176