Description
Spacecraft for lunar mission is :
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Cuboid in shape of approximately 1.5 m side.
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Weighing 1380 kg at launch and 675 kg at lunar orbit.
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Accommodates eleven science payloads.
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3-axis stabilized spacecraft using two star sensors, gyros and four
reaction wheels.
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The power generation would be through a canted single-sided solar array
to provide required power during all phases of the mission. This
deployable solar array consisting of a single p
