dc.contributor.author |
Whittlesey, A. |
en_US |
dc.date.accessioned |
2004-10-06T17:35:50Z |
|
dc.date.available |
2004-10-06T17:35:50Z |
|
dc.date.issued |
1993-03-09 |
en_US |
dc.identifier.citation |
Manhattan Beach, CA |
en_US |
dc.identifier.clearanceno |
92-2007 |
en_US |
dc.identifier.uri |
http://hdl.handle.net/2014/36713 |
|
dc.description.abstract |
This talk is about ground testing of spacecraft to determine immunity to the electrostatic discharges (ESDs) in certain Earth orbits. The particular spacecraft used as an example is the TOPEX/Poseidon spacecraft, an Earth orbiter with a 1334 km, 62 degree orbit. The talk is based on my recent experience with that spacecraft, but is an example of a generally good program. The program and this talk consist of the following elements: a discussion of the environment, showing the specific hazard areas on the spacecraft to illustrate the space charging and ESD process; spacecraft design features related to the environmental threat; the test device used for TOPEX/Poseidon; the test itself, including logistic and actions to avoid inadvertent damage to the spacecraft; and conclusions and lessons learned. |
en_US |
dc.language.iso |
en_US |
|
dc.subject.other |
electrostatic discharge orbits spacecraft TOPEX/Poseidon hazard areas space charging ESD |
en_US |
dc.title |
System Electrostatic Discharge Testing for Space Charging Caused ESD Events |
en_US |