Average end of charge voltages and pressures, and capacity output in ampere hours are presented. Test limits specify those values at which a cell is to be terminated from charge or discharge. Requirements are based on past cell performance data. The requirement does not constitute a limit for discontinuance from testing. The nickel cadmium batteries were screened for internal shorts, low capacity, electrolyte leakage, or inability of any cell to recover its open circuit voltage above 1.150 volts during the internal short test
Results are presented of acceptance tests conducted on eleven nickel cadmium batteries of the Nimbus...
A group of 29 cells with capacities ranging from 21.7 to 28.8 ampere-hours were tested. A summary of...
The standard plate cells exhibited higher average end-of-charge (EOC) voltages than the cells with t...
The tests are to insure that all cells put into the life cycle program are of high quality by the sc...
Five cells provided by NASA's Goddard Space Flight Center were evaluated at room temperature and pre...
This evaluation test program had the purpose to insure that all cells put into the life cycle progra...
Evaluation tests of 10 nickel cadmium cells are described. Although pressures were greater than what...
An evaluation test program was conducted to insure that all cells put into the life cycle program ar...
The capacity of the cells ranged from 6.6 to 7.6 ampere hours during the three capacity tests. No vo...
Quality control measures for Ni-Cd spacecraft cells were analyzed. Cells were examined for electroly...
Cells found to have electrolyte leakage, internal shorts, low capacity, or inability of any cell to ...
The report describes testing and performance of 20.0 ampere-hour Ni-Col spacecraft batteries
The capacity of the cells ranged from 3.58 to 3.97 amperehours during the three capacity tests. Thre...
Evaluation tests of eight nickel cadmium cells are described. Although high cell pressures were obse...
Tests were conducted on a group of 29 cells for the purpose of removing from the life cycle program ...
Results are presented of acceptance tests conducted on eleven nickel cadmium batteries of the Nimbus...
A group of 29 cells with capacities ranging from 21.7 to 28.8 ampere-hours were tested. A summary of...
The standard plate cells exhibited higher average end-of-charge (EOC) voltages than the cells with t...
The tests are to insure that all cells put into the life cycle program are of high quality by the sc...
Five cells provided by NASA's Goddard Space Flight Center were evaluated at room temperature and pre...
This evaluation test program had the purpose to insure that all cells put into the life cycle progra...
Evaluation tests of 10 nickel cadmium cells are described. Although pressures were greater than what...
An evaluation test program was conducted to insure that all cells put into the life cycle program ar...
The capacity of the cells ranged from 6.6 to 7.6 ampere hours during the three capacity tests. No vo...
Quality control measures for Ni-Cd spacecraft cells were analyzed. Cells were examined for electroly...
Cells found to have electrolyte leakage, internal shorts, low capacity, or inability of any cell to ...
The report describes testing and performance of 20.0 ampere-hour Ni-Col spacecraft batteries
The capacity of the cells ranged from 3.58 to 3.97 amperehours during the three capacity tests. Thre...
Evaluation tests of eight nickel cadmium cells are described. Although high cell pressures were obse...
Tests were conducted on a group of 29 cells for the purpose of removing from the life cycle program ...
Results are presented of acceptance tests conducted on eleven nickel cadmium batteries of the Nimbus...
A group of 29 cells with capacities ranging from 21.7 to 28.8 ampere-hours were tested. A summary of...
The standard plate cells exhibited higher average end-of-charge (EOC) voltages than the cells with t...