A microsatellite of mass 400kg is initially drifting in space with negligible speed relative to an inertial frame. Its onboard thrusters are fired, giving it a velocity of 2.0m/s at an angle of 30∘ above the positive x–axis in the x–y plane.
a. (a) Resolve the satellite’s final velocity into its x and y components.
b. (b) Determine the corresponding components of its linear momentum.
c. (c) Write the momentum vector in component form (pxi^+pyj^) and calculate its magnitude.
d. (d) Calculate the impulse delivered to the satellite by the thrusters and state its direction using unit vector notation.