Question 1
State the law of conservation of angular momentum.
[1 mark]
Figure 1 shows an orbiting satellite fitted with two small instrument pods attached to the ends of telescopic arms. The arms can be extended or retracted by a motor in the body of the satellite.
With the telescopic arms fully extended, the centre of mass of each instrument pod is at a radius of 4.1 m from the axis of rotation.
moment of inertia of satellite body about axis = 71 kg m2 mass of each instrument pod = 5.0 kg
The mass of the telescopic arms is negligible.
Show that the total moment of inertia of the satellite with the arms fully extended is
[2 marks]
The satellite is initially rotating slowly about its axis with the arms fully extended. The arms are slowly retracted so that the instrument pods move closer to the body of the satellite.
State and explain the change in the angular speed of the satellite as the arms are retracted.
[3 marks]
The satellite is initially rotating at 1.3 rad s−1 with the telescopic arms fully extended. When fully retracted the instrument pods are at a radius of 0.74 m from the axis. The satellite contains sensitive equipment that may be damaged if the rotational speed exceeds 4.2 rad s−1
Deduce whether the arms can be retracted fully without the satellite exceeding its maximum permitted angular speed.
[3 marks]