Aerospace Engineering > GATE 2009 > Satellite Operations
The life of a geo-stationary communications satellite is limited by
A
the working life of the on-board electronic circuitry
B
the time it takes for its orbit to decay due to atmospheric drag
C
the quantity of on-board fuel available for station-keeping
D
the number of meteorite impacts that the satellite structure can withstand before breaking up

Correct : c

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