Spacecraft charging standard
The spacecraft charging protection requirements for space vehicles which are to operate in the magnetospheric plasma environment are presented.
Engineering topics
Publications and source records attributed to Bunn, M. H..
The spacecraft charging protection requirements for space vehicles which are to operate in the magnetospheric plasma environment are presented.
Aerospace environments are reviewed in reference to spacecraft charging. Modelling, a theoretical scheme which can be used to describe the structure of the sheath around the spacecraft and to calculate the charging currents within, is discussed. Materials characterization is considered for experimental determination of the behavior of typical spacecraft materials when exposed to simulated geomagnetic substorm conditions. Materials development is also examined for controlling and minimizing spacecraft charging or at least for distributing the charge in an equipotential manner, using electrical conductive surfaces for materials exposed to space environment.