An electron analyser to measure the three-dimensional velocity distrib
ution of electrons in the energy range from 0.59 eV to 26.4 keV on the
four spacecraft of the Cluster mission is described. The instrument c
onsists of two sensors with hemispherical electrostatic energy analyse
rs with a position-sensitive microchannel plate detectors placed to vi
ew radially on opposite sides of the spacecraft. The intrinsic energy
resolutions of the two sensors are 12.7% and 16.5% full width at half
maximum. Their angular resolutions are 2.8 degrees and 5.3 degrees res
pectively in an azimuthal direction and 15 degrees in a polar directio
n. The two sensors will normally measure in different overlapping ener
gy ranges and will scan the distribution in half a spacecraft rotation
or 2 s in the overlapped range. While this is the fastest time resolu
tion for complete distributions, partial distributions can be recorded
in as little as 62.5 ms and angular distributions at a fixed energy i
n 7.8 ms. The dynamic range of the instrument is sufficient to provide
accurate measurements of the main known populations from the tail lob
e to the plasmasheet and the solar wind. While the basic structure of
the instrument is conventional, special attention has been paid in the
design to improving the precision of the instrument so that a relativ
e of the order of 1% could be attained in flight in order to measure t
he gradients between the four spacecraft accurately; to decreasing the
minimum energy covered by this technique from 10 eV down to 1 eV; and
to providing good three dimensional distributions.