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NASA STD-4005 Rev. A PDF

NASA STD-4005 Rev. A PDF

Name:
NASA STD-4005 Rev. A PDF

Published Date:
02/01/2016

Status:
Active

Description:

Low Earth Orbit Spacecraft Charging Design Standard

Publisher:
National Aeronautics and Space Administration

Document status:
Active
Format:
Electronic (PDF)
Delivery time:
10 minutes
Delivery time (for Russian version):
200 business days
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Choose Document Language:
$8.7
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This standard provides requirements relative to various plasma interactions that can result when a high-voltage system is operated in the Earth's ionosphere and standard practices to eliminate or mitigate such reactions. The purpose of this standard is to provide a design standard for high-voltage space power systems (> 55 volts) (V))that operate in the plasma environment associated with LEO (altitude from 200 and 1000 km and latitude between -50 and +50 degrees). Such power systems, particularly solar arrays, are the proximate cause of spacecraft charging in LEO; and these systems can interact with this environment in a number of ways that are potentially destructive to themselves as well as to the platform or vehicle that has deployed them. NASA Endorsed. OCE.
Edition : A
File Size : 1 file , 130 KB
Number of Pages : 27
Published : 02/01/2016

History

NASA STD-4005 Rev. A w/Chg 1
NASA STD-4005 Rev. A w/Chg 1
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NASA STD-4005 Rev. A
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