Power from a Tether A few years ago, the space shuttle $\mathrm{Co}$ lumbia tricd an cxperiment with a tethered satellite. The satellite was released from the shuttle and slowly reeled out on a long conducting cable as shown in Fig. $31-57$ (not to scale). For this problem we will make the following approximations:
The shuttle is moving at a constant velocity. The Farth's magnetic ficld is constant and uniform.
The line of the tether, the velocity of the system, and the magnetic field are all perpendicular to each other.
The Earth's field produces an FiGURE 31-57 = Problem 65 . emf from one end of the cable to the other. The idea is to use a system like this to generate electric power in space more efficiently than with solar panels.
(a) Explain why a voltage difference is produced.
(b) If the Earth's magnetic field is given by a magnitude $\vec{B}$, the shuttle- satellite system is moving with a velocity $\vec{v}$, and the tether has a length $L$, calculate the magnitude of the emf $\mathscr{E}$ from one end of the tether to the other.
(c) At the shuttle's altitude, the Earth's field is about $0.3$ gauss and the shuttle's speed is about $7.5 \mathrm{~km} / \mathrm{s}$. The tether is $20 \mathrm{~km}$ long (!). What is the expected potential difference in volts?
(d) At the altitude of the shuttle, the thin atmosphere is lightly ionized, allowing a current of about $0.5$ amps to flow from the satellite hack to the shuttle through the thin air. What is the resistance of the $20 \mathrm{~km}$ of ionized air?