4 Contents
understanding turbulence in galaxy clusters to the accretion processes in binary systems or active galactic
nuclei.)
Microcalorimeters are non-dispersive thermal detectors that will provide the next major step in imaging
spectroscopy capabilities compared to gas proportional counters or charge coupled devices (CCD) which
have been extensively used in X-ray space instrumentation over the past several decades. Microcalorimeters
will full-fill the needs of X-ray astrophysics in the 21st century, combining eV level energy resolution in the
soft X-ray energy range in large format imaging arrays with potentially 1000’s of pixels. With resolving
powers >1000, microcalorimeters are competitive with dispersive grating spectrometers, but with the
advantage of high collection efficiency. This enables efficient observations of point sources and extended
sources with the same instrument. The sensor technology used in microcalorimeters can come in different
forms - silicon thermistors, transition-edge sensors (TESs) and magnetic microcalorimeters (MMCs) - but
the basic principle is the same. A microcalorimeter measures the temperature rise resulting from the energy
deposited by a single X-ray photon. The sensor transduces the change in temperature to an electrical signal
(either through a resistance change for thermistors and TESs or a change in magnetism for MMCs), from
which the photon energy can then be determined. In order to achieve resolving powers of ∼1000’s at keV
energies, extremely low detector noise is required, only achievable when operating at mK temperatures. The
potential power of microcalorimeters to revolutionize X-ray astrophysics has already been demonstrated
by the observation of the Perseus galaxy cluster by the Hitomi satellite’s Soft X-ray Imaging Spectrometer
(SXS) [63].
In this chapter, we describe microcalorimeters based around highly sensitive transition-edge-sensors
(TESs). TESs are next generation microcalorimeters based on a thin superconducting film that is electri-
cally biased in the narrow region between superconducting (zero-resistance) state and the normal resistive
state. The transition region is typically only a few mK in width and as such, TES detectors are extremely
sensitive to temperature changes making them ideal detectors for high resolution X-ray spectroscopy. We
start by outlining the basic principles behind the operation and design of TESs, and their fundamental
noise limits. We will elaborate on the key fundamental physics effects that guide the design and optimiza-
tion of the TESs. We will then describe important calibration considerations for space flight instruments.
We will continue by introducing novel multi-pixel TES designs and conclude the chapter by presenting the
applications in future X-ray space missions over the coming decades.
Theoretical and Experimental Background
Basic Principles
A TES-based X-ray detector is a thermal equilibrium calorimeter. It consists of three fundamental com-
ponents: an absorber with heat capacity C, a thermometer (the TES), and a weak thermal link, with a
conductivity Gbath, to the heat sink at temperature Tbath, which is below the operating temperature of the
device. Details on the design of each of these components is described in Section . A simplified scheme of
a TES calorimeter is shown in Fig. (1).
TESs are based on superconducting thin films, voltage biased in the narrow transition region between
the onset of resistance and the fully normal state. A single photon deposits its energy Einto the absorber,
which converts it into heat. The temperature rise, proportional to the energy, causes a change in resistance
of the TES. The resistance change is determined by monitoring the current through the TES using a super-
conducting quantum interference device (SQUID) ammeter. Within this general description, there is room
for countless variations. Important device parameters such as the noise, Gbath and Care strongly dependent
on the operating temperature of the device. Thus, the transition temperature of the TES must be chosen
to achieve the desired energy resolution and response time, whilst being compatible with the instrument
cryogenic architecture. For typical astrophysics applications a transition temperature of below 100 mK is
ideal.