DocumentCode :
11855
Title :
An Overview of Spacecraft Charging Research in India: Spacecraft Plasma Interaction Experiments—SPIX-II
Author :
Gupta, Suryakant B. ; Kalaria, Keena R. ; Vaghela, Naresh P. ; Mukherjee, Subroto ; Joshi, Rashmi S. ; Puthanveettil, Suresh E. ; Shankaran, Muthusamy ; Ekkundi, Ranganath S.
Author_Institution :
Facilitation Centre for Ind. Plasma Technol., Inst. for Plasma Res., Gandhinagar, India
Volume :
42
Issue :
4
fYear :
2014
fDate :
Apr-14
Firstpage :
1072
Lastpage :
1077
Abstract :
When a satellite leaves earth´s atmosphere, the satellite potential floats negatively with respect to the surrounding plasma environment. Once the satellite surface consisting of different materials is charged and depending upon the dielectric constant of various materials, a potential difference develops between the surface of insulators and that of conductors, and under favorable conditions it exceeds the threshold value, which finally results in an electrostatic discharge (ESD). The potential difference arises on the solar panels when satellite bus voltage is increased to meet the present demand of the transponders. The resultant ESD may trigger a secondary arc, which can destroy the solar panel circuit and severely damage the substrate. Therefore, there is a need to test the performance of these solar arrays in a ground simulation facility. Recently, based on the collaborative research work in France, USA, and Japan, international standards for space solar panels have been finalized. This ISO document [ISO-11221] specifies qualification and characterization test methods to simulate plasma interaction and electrostatic discharges on solar array panels in the space. A linear circuit model has been jointly developed by Facilitation Center for Industrial Plasma Technologies, Institute for Plasma Research and ISAC, Indian Space Research Organization. This model explains the primary arc in low Earth orbit like plasma environment and geo-synchronous Earth orbit like electron irradiation environment. This paper discusses about the automated ISO test facility developed for detection and analysis of arc on the solar coupon. From the initial test results it has been confirmed that there is a gradual increase in surface potential on the solar coupon. The velocity of arc is measured based upon the neutralization currents in the adjacent solar cell strings. Damage caused by permanently sustained arc on solar coupon´s surface is also studied.
Keywords :
Earth orbit; aerospace simulation; arcs (electric); artificial satellites; conductors (electric); electrostatic discharge; ground support systems; insulators; solar cell arrays; spacecraft charging; surface potential; terrestrial atmosphere; transponders; ESD; ISAC; ISO document; Indian Space Research Organization; Industrial Plasma Technology; Institute for Plasma Research; SPIX-II; adjacent solar cell strings; arc analysis; arc detection; arc velocity measurement; automated ISO test facility; conductor; dielectric constant; earth atmosphere; electron irradiation environment; electrostatic discharge; geo-synchronous Earth orbit; ground simulation facility; insulator; international standards; linear circuit model; low Earth orbit; neutralization current; nonsustained arc; permanently sustained arc; primary arc; satellite bus voltage; satellite potential difference; satellite surface; solar array panel; solar coupon; space solar panel circuit; spacecraft charging; spacecraft plasma interaction experiments; surface potential; temporary sustained arc; threshold value; transponder; Electric potential; Electrostatic discharges; Plasmas; Satellites; Space vehicles; Surface discharges; Voltage measurement; Arc velocity; low Earth orbit (LEO) and geo-synchronous Earth orbit (GEO) spacecraft charging; non sustained arc (NSA); permanently sustained arc (PSA); primary arc (PA); surface potential; temporary sustained arc (TSA); temporary sustained arc (TSA).;
fLanguage :
English
Journal_Title :
Plasma Science, IEEE Transactions on
Publisher :
ieee
ISSN :
0093-3813
Type :
jour
DOI :
10.1109/TPS.2014.2306019
Filename :
6750087
Link To Document :
بازگشت