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NASA-STD-4005, NASA TECHNICAL STANDARD: LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN STANDARD (03 JUN 2007)

NASA-STD-4005, NASA TECHNICAL STANDARD: LOW EARTH ORBIT SPACECRAFT CHARGING DESIGN STANDARD (03 JUN 2007)., 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-STD-4005

    
 Status:
Active

 FSC Code:
 1810 - Space Vehicles

Version:
A02-2016130.23 KB NASA-STD-4005A
06-200751.30 KB NASA-STD-4005

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