To find the acceleration of the astronaut and satellite, we can use Newton's second law, \( F = ma \), where \( F \) is the force applied, \( m \) is the mass, and \( a \) is the acceleration.
For the astronaut:
\[ a_{astronaut} = \frac{F}{m_{astronaut}} = \frac{30\,N}{60\,kg} \]
\[ a_{astronaut} = 0.5\,ms^{-2} \]
For the satellite:
\[ a_{satellite} = \frac{F}{m_{satellite}} = \frac{30\,N}{300\,kg} \]
\[ a_{satellite} = 0.1\,ms^{-2} \]
Both the astronaut and the satellite will experience these accelerations in opposite directions due to Newton's third law of equal and opposite reaction.
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