Development of a PPT for the EO-1 Spacecraft
The analysis reveals that the majority of the PPT operations occur with charge duration of about 320 msec and below. ... interference/compatibility testing was conducted at NASA GRC to characterize protoflight PPT emissions. ... Manual frequency tuning and time domain observation of emissions supplemented, or replaced when necessary, conventional ... Worst case voltage spike magnitudes of 3 to 5 V peak-to-peak were well within the EOal specification of +50 to ~150 percentanbsp;...
| Title | : | Development of a PPT for the EO-1 Spacecraft |
| Author | : | |
| Publisher | : | - 2000 |
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