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V Part A A small rocket burns a mass 0.0550 kg of fuel per second, ejecting it as a gas with a velocity relative to
V Part A A small rocket burns a mass 0.0550 kg of fuel per second, ejecting it as a gas with a velocity relative to the rocket of magnitude 1570 m/s. What is the thrust of the rocket? Express your answer in newtons. AEd 2 F = N Submit Request
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