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Nickel-metal hydride secondary batteries  4/17
      Table 4.12  Summary of  LEO cycle life test results for IPV Ni-H2 battery cells

       Manufacturer   No.   Capacity   Cycle   DOD   T     Cycles     Status        Test
                     cells   (Ah)    reginze   (%)   ("C)                         laborator):
      Hughes           3      50     LEO      40     10    19000   No failures   GE Astro Space
                                                                   test continuing
      Yardney          5      50     LEO      40     10    18000   No failures   Martin Marietta
                                                                   test continuing
      GE (now Hawker   16     50     LEO      40     10    15968   No failures   Martin Marietta
      Energy Inc.)                                                 test continuing
      Eagle-Picher    16      50     LEO      40     10    16912   No failures   Martin Marietta
                                                                   test continuing


      which to some extent must be regarded as still under   cell  technology  to  new  chemistry  are  just  becom-
      development.  'These  include  the  Spacenet  and  Intel-   ing  available  for  product  applications  such  as  note-
      stet V cells available from Comsaflntelstat  (US) and   book computers.
      the  Superbird cell V  available from Airforce Hughes   In  general  the  nickel-metal  hydnde  cell  per-
      (US). Data is also given for 27 cell batteries made up   forms  in  a  similar  manner  to  conventional  nickel-
      from these individual cells.                cadmium cells.
        The capacity decreases, as expected, with increasing   The  cell  volumetric  energy  density  is  currently
      temperature. For the  superbird battery the capacity at   between  25  and  30% better  than  high-performance
      35°C is only about 57% of the capacity at WC, at 30°C   nickel-cadmium  cells  or  close  to  double the  energy
      about  6796,  at  20°C  about  81%,  and  at  10°C about   density  of  'standard'  nickel-cadmium  cells.  This
      94%. For the Spacenet cells, on average the capacity   translates to  a present capacity for a Cs cell of  2700
      at  20°C is  about  84% of  the  capacity at WC,  and  at   milliampere-hours (mA h) in nickel-metal  hydride vs
      lWC about 97'%/0.                           2000 mA h for nickel-cadmium  cells. Improved design
        Some information on life cycle tests carried out on a   and materials usage optimization is anticipated to result
      range of commercially available nickel-hydrogen  cells   in  about 30% increase in  capacity for metal-hydride
      is summarized in Table 4.12.                cells over the next 5 to 6 years. Although first devel-
        Cycle  tests  are  continuing  and  databases  being   opment and application of  the metal-hydride  cell has
      developed. Cycles of 6000- 19  0100 have been achieved   been for medium-rate applications, high-rate discharge
      with tests continuing in orbit and ground-based trials.   capability has proven to be acceptable as well.
      A  way  of  increasing  cycle life  at  80% depth  of  dis-   Behaviour  of  the  nickel-metal  hydride  cell  on
      charge  is  to  decrease  the  potassium  hydroxide  elec-   charge and  its  toIerance for  overcharge is  very  sim-
      trolyte concentration from 3 1% to, say, 26%. Approx-   ilar to that of the nickel-cadmium  cell. There are two
      imately 40 000 cycles to 80% depth of discharge have   areas where  differences between the  two  chemistries
      been achieved using a 26% potassium hydroxide elec-   should be recognized:
      trolyte compared to 3500 cycles at 80% depth of  dis-
      charge using 3 1 % potassium hydroxide.     1. The metal hydride charging reaction is exothermic
        The present state of development of individual pres-   while the nickel-cadmium  reaction is endothermic.
      sure vessel (PV) nickel-hydrogen  battery cells is that   This  means  the  metal  hydride  cell  will  warm  as
      they are acceptable where not many cycles are required   it  charges whereas the  nickel-cadmium  cell  tem-
      over  life,  Le.  1000 cycles  over  10 years  of  geosyn-   perature  remains  relatively  constant  and  the  cell
      chronous orbit applications, but  are not acceptable in   moves into overcharge. However, the metal hydride
      applications wlhere many cycles are required, typically   cell still retains the marked increase in temperature
      30 000 over five years. In low earth orbit applications   on  overcharge  which  makes  temperature-sensing
      only 6000 to 10000 cycles at 80% depth of  discharge   charge termination schemes  feasible. The cells can
      can be achieved.                              be discharged at the 2-4T  rate and charged at the
                                                     1°C rate.
      4.5  Nickel-metal hydride secondary         2.  The  voltage  profile  on  charge  for  nickel-metal
       atteries                                      hydride cells shows a less dramatic decline at over-
                                                     charge  than  seen  with  nickel-cadmium  cells.  As
      For those battery users who need high power in a small   nickel-cadmium  cells  move  into  overcharge,  the
      package and are willing to pay a premium for it, there   voltage  peaks,  and then  begins  a  distinct decline.
      is  a  new  opti'on. Battery  manufacturers  have  begun   Some  nickel-cadmium  charging  schemes  have
      to  tap  the  potential  of  nickel-metal  hydride  couples   based charge termination on this negative slope to
      which  offer  significant increases  in  cell  power  den-   the voltage curve (-AV  charging). Design of  such
      sity. These extensions of  the  sealed nickel-cadmium   systems  to  work  with  nickel-metal  hydride  cells
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