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How can I calculate the necessary thrust to keep a satellite of 1 kg mass in orbit, for a Delta-V of 2 m/s, knowing that the correction force must be done once a month for 900 seconds?

uhoh
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Ricardo Casimiro
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1 Answers1

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If you mean that you need to get 2 m/s delta-v by thrusting for a period of 900 seconds, it's very straightforward to ask Wolfram Alpha:

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Russell Borogove
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