Diamond and Related Materials
DIAMOND
UV DETECTORS FOR FUTURE SOLAR PHYSICS MISSIONS
J-F. Hochedez[1], P. Bergonzo[2], M-C. Castex[3], P. Dhez[4], O. Hainaut[5], M. Sacchi[6],
J. Alvarez[7], H. Boyer[8], A. Deneuville[9], P. Gibart[10], B. Guizard2, J-P. Kleider7,
P. Lemaire5, C. Mer2, E. Monroy11,
E. Muñoz[11], P. Muret9,
F. Omnes10,
J.L. Pau11,
V. Ralchenko[12], D. Tromson2,
E. Verwichte1, J‑C. Vial5
Word
count : 4151, Abstract
Reference : DM00280, Diamond 2000 presentation number :
16.2
Despite
their steady improvement over the last decades, the present UV detectors
exhibit some limitations inherent to their silicon technology. Yet, the utmost
spatial resolution, temporal cadence, sensitivity, and photometric accuracy
will be decisive for the forthcoming space solar missions. The advent of novel
diamond or nitride imagers would surmount many current weaknesses, thus opening
up new prospects and making the instruments cheaper. As for projects like the
Solar Probe of NASA, or the Solar Orbiter of ESA, the aspiration for diamond UV
detectors is still more sensible for these spacecrafts will approach very near
to the Sun where the heat and the radiation fluxes are tremendously high. This
triggered the initiative of an original R&T programme entitled BOLD
described in this paper. We depict motivations and intentions, and report on
dedicated experiments with several devices under EUV synchrotron light, NUV
laser, and micro-Raman spectroscopy.
Keywords : Detectors, Diamond, Nitrides, UV range
The
performance of XUV/EUV/VUV/NUV detectors has steadily increased over the last
decades in every respect, and the astrophysical instruments taking advantage of
them have improved accordingly. The focal plane properties are often the
bottleneck in the modern telescopes. Such large sensitive linear sensors
participate significantly to the achievements of the recent solar missions like
SOHO, YOHKOH, TRACE, and others (e.g. [[13]]).
Nevertheless,
CCDs designed for UV observations exhibit some shortcomings that are difficult
to overcome within silicon technology :
1.
Cooling must
be implemented to reduce the dark current and to prevent degradations from
ionizing radiations, but it is a thorny and costly solution in space missions.
2.
Additionally,
the cooled detector turns unfortunately into a cold trap for contaminants.
Unavoidable hydrocarbon molecules not only stick to the sensitive surface but
also polymerize under the UV signal degrading the detector operations
irreversibly.
3.
The
isotropic ionizing radiations leads to images that are instantly covered by
“cosmic hits” (bright points and streaks), which are hard to disentangle from
the UV signal. Moreover, the ensuing degradation of the charge transfer
jeopardizes the lifetime of the whole mission itself [[14]].
4.
The evolving
oxide deteriorates the Quantum Efficiency (QE), its stability, and its spatial
homogeneity, resulting in poor pre-launch calibration reliability.
5.
The minimal
size of the silicon UV pixel is limited to circa 10 µm.
6.
The
penetration depth of the photons in the silicon determines a pan-chromatic
sensitivity that is deleterious when observing a bright visible source like the
Sun (See Figure 1). One therefore adds filters that absorb the
undesired optical photons, but also attenuate regrettably the hunted
ultraviolet ones.
These
drawbacks become critical in the context of the future solar missions for which
the highest spatial resolution, sensitivity, temporal cadence and photometric
accuracy are sought after. The Sun is the only star that can potentially
be observed with the spatial resolution of the fundamental physical magnetic
processes at work. It is
broadly agreed nowadays that we lack spatial resolution to fully comprehend its
corona and hence, stellar objects in general (See Figure 2).
The building
blocks of the solar atmosphere are the magnetic loops, but not all is
ascertained about them. Their equilibrium is questioned. Their exact
configuration is unclear. Their filling factor is low. Filamentary and threaded
patterns are observed, etc.… All these facts point at unrevealed
unravelled sub-pixel structures. Not to mention that there are lots of various
dynamical events (nano-flares, brightenings, explosive events, blinkers, etc.…).
Their properties approximately comply with self-similarity laws, validating
hidden smaller scales. In order to fulfil this indubitable observational need,
one has to somehow square the circle given the fact that the smaller the pixel,
the lesser the signal and the more dynamical the target. Furthermore, the
higher the cadence, the lesser is the signal too. This review of the stakes
means that the quests for resolution, cadence and sensitivity are definitely
inseparable.
A markedly
superior spatial resolution can be achieved either by going close to the Sun
with a “standard” instrument, or by increasing considerably the aperture and
the focal length of a telescope in an Earth orbit. In the first category (Solar
Probe [[15]] and Solar Orbiter [[16]] missions), the whole package including
the detector is submitted to a high radiative and particle flux. In the second
case, the gain of spatial resolution happens inevitably at the expense of the
signal level, especially if the temporal resolution is to be matched with the
smallest expected observables. For instance, a resolution of tens of kilometres
on the Sun (better than 0.1 arcsec) implies exposure times smaller than
one second since expected velocities may be of a few 100 km/s
(magneto-acoustic) and higher (Alfven).
Figure
2 A strong enhancement
of spatial resolution is essential to explore the dynamical structures of the
chromosphere, transition region and corona. The left image is a full field
image of the Sun made by EIT/SoHO in the Fe XV line (284 Å).
Instrumental artefacts like the grid pattern of the mesh supporting filters and
the QE degradation at the limb are visible. The central image was made on the
same day by TRACE in the Fe IX/X line (171 Å). Many cosmic hits are
noticeable.
The
remaining of this paper is organized as follows : the BOLD investigation is
first introduced, the experimental section then describes briefly the devices
under study, preliminary measurements, and interpretations. The conclusion
presents the outlook for the various aspects of the current endeavour.
Diamond or
nitride imagers would circumvent many of the restrictions listed above. They
would open -just like the CCD in the past- new opportunities in the development
of solar telescopes and spectrometers of higher capabilities. They will be more
cost-effective as well by sparing the development and the weight of cooling
hardware, radiative shields and bake-out resources.
·
The wide
bandgap permits to operate the detector at room temperature, with no need for
cooling and with a reduced pollution risk. Such bandgaps also make the
detectors “solar-blind” (i.e. insensitive to optical light, See Figure 1). As the filters have a thermal role, and
anticipating incomplete solar-blindness, they cannot be suppressed; but their
amount can be reduced, thus improving greatly the effective area of UV
instruments (and allowing shorter integration times, improved
Signal / Noise ratios, etc.).
·
The compact
crystal networks provide radiation-hardness.
·
The absence
of an oxide will improve the QE and its stability.
·
Thanks to a
larger breakdown field, the pixel is potentially in the sub-micrometer range,
an order of magnitude smaller than present silicon detectors
·
Due to
higher carrier velocities, the detector will be read out faster.
CVD diamond
was identified as an outstanding material for UV detection years ago (See [[18]] and historical references in [[19], [20]]). In the past the material quality
prevented the development of detectors rivalling those already existing.
Recently, GaN nitride has become a promising competitor for UV photodetection [[21]].
Even now, the strategy toward useful devices has to be carefully evaluated. To
this end, the BOLD investigation (Blind to the Optical Light Detectors) was
instigated in 1999 via the coordinated expertises of most required disciplines
(material growth, device design, characterizations, application definition). As
seen from the list of authors many institutes, in different fields, contribute
to BOLD (and the list is not closed). The project includes also the Centre Lasers Intenses et Applications (CELIA),
Bordeaux, France, the Instituut
voor Materiaal Onderzoek (IMO), Diepenbeek, Belgium, the Laboratoire de
Physique des Milieux Ionisés (LPMI), Palaiseau, France, the Laboratoire de
Physique des Solides et de Cristallogenèse (LPSC), Meudon, France, the Laboratory
of Solid State Physics and Magnetism (LVSM), KU Leuven, Belgium, and the University College London (UCL), Great Britain. Several places not only have the
appropriate equipment, but also a need for the intended device [[22], [23], [24], [25], [26], [27]].
Other teams are advancing in similar directions (e.g. [[28], [29]]). Our strategic line focuses on the
following selected approaches :
1.
So as to
avoid the detrimental grain boundaries, solutions are considered in two
directions :
A/ the superior properties of the intra-crystallite characteristics are being
verified, and geometrically adaptable designs are sought after.
B/ structures are fabricated and tested on homoepitaxial layers.
2.
The same
equipments compare diamond and nitride devices of various architectures.
3.
The
methodology traces all devices through the largest available set of relevant experiments.
4.
In
particular, the UV tests extend from the XUV range to the visible covering the
scope of penetration depths.
5.
Transitional
objectives are conceived, as it is unlikely to attain straight away a
solar-blind 2000 x 2000 UV imager with sub-micrometer pixel and
100% QE in the EUV range. Nonetheless, experiments aim at demonstrating
its feasibility within the time slot compatible with the previously cited solar
missions (a decade). In parallel, we identify immediate and short-term
applications.
6.
Empirical
and theoretical modelling is seen as a key condition to control the expected
improvements and feedbacks from the experiment to the fabrication process.
Four
measurement campaigns were already accomplished; they are accounted here briefly.
In Nov.1999, photoemission and photocurrent measurements were done with
synchrotron light around the Carbon CK edge on LETI devices to
address surface effects. During Feb.2000, micro-Raman spectroscopy was
performed on one of the synchrotron-tested layer to confirm the absence of sp2
bonds, and assess sub-grain variations of the crystal characteristics. More
diamond samples could later be gathered originating from the GPI and the LEPES
(homoepitaxial layer), and nitride devices from UPM/CRHEA. Standard LETI
inter-digitated electrodes were deposited on the GPI layers, whereas the LEPES
and the UPM/CRHEA devices are Schottky photodiodes. The mobility-lifetime
product of the LETI and GPI devices was measured in continuous mode at LGEP.
Finally preliminary laser tests were carried out at LPL in July 2000. The NUV
and VUV lasers serve to produce micro-spots probing the detector efficiency at
small scales.
The plasma
enhanced chemical vapour deposition technique (PECVD) enables the fabrication
of large area diamond layers. The material obtained has a polycrystalline
structure with a grain size of about 10% of the layer thickness. The growth
conditions (0.5 % methane in hydrogen, and 750°C substrate temperature) had
previously been optimised in order to yield the best electronic properties [[30]]. Typical growth rates are of the order
of 0.2-0.5 µm/h for these films. Prior to the formation of electrical contacts,
the diamond samples were annealed and chemically treated. This constitutes a
critical step in the device fabrication resulting in a reduction of the device
leakage current (by up to 7 orders of magnitude compared to untreated samples)
down to values below 1 pA at 50 kV/cm [[31]]. Gold pads were deposited to form
electrodes, using an e-beam evaporator. Contact geometries were obtained using
the standard photolithographic techniques. At the typical operating voltages of
104 V.cm-1, the barrier height that results from the
use of gold on diamond is negligible with respect to the bias.
Figure
3 Scheme of the simple MSM configurations tested. The results
presented in this paper mostly relate to the coplanar structures (d).
The
membranes actually used are 20 or 200 µm thick, making the grain size of
the order of a few microns. The electrodes are deposited on the topside. The
electrode width and inter-electrode gap are 200 µm.
Undoped and heavily boron doped homoepitaxial
diamond films were deposited on Ib diamond substrates at 830°C by MPCVD of a
mixture of (B2H6/) 4%CH4/96% H2. Heavy doping allow the achievement of very low
resistance contacts. Studies are under progress to achieve multilayer
structures comprising Schottky barrier metal/ undoped diamond/ heavily doped
diamond/ Ib substrate, with low residual boron content in the
"undoped" film, and good Schottky barrier behaviour.
GPI diamond films were grown in a microwave
plasma assisted CVD reactor (5 kW, 2.45 GHz) using 1-2% CH4 diluted
in H2 as a feed gas as described elsewhere [[32]].
The samples 5x5 mm and 7x7 mm in size were cut with laser from free-standing
diamond wafers. Two films #117b (0.65 mm thick) and #118 (1.15 mm)
were produced with growth rate 2.8 μm/hr, they contained 1 ppm
of nitrogen. These samples were polished, while the unpolished thin film #81
(80 μm) produced at growth rate of 0.4 μm/hour contained
about 4 ppm nitrogen impurity as revealed from UV absorption spectra. All
the tested films were translucent; no features of other carbon phases except a
strong diamond line at 1332 cm-1 were seen in Raman spectra. Interleaved (200µm gold / 200µm gap) electrodes
have been deposited on the growth side of the films. To check the effect of surface pre-treatment
one sample #81-1R was metalized as received (without annealing and chemical
treatment), while the sample 81-1C from the same batch was cleaned and
metalized identically to samples #117b and #118.
Si-doped
AlGaN samples were grown on c-sapphire by metal-organic vapor phase epitaxy
(MOVPE) in CRHEA (devices X262 and X300), and on Si(111) by molecular beam
epitaxy (MBE) in DIE/UPM (device M395). Mirror-like surface morphologies were
typically obtained for all AlGaN layers. MOVPE GaN samples present a typical
full width at half maximum (FWHM) of 300 arc sec for the (0002) X-ray
diffraction peak in the w configuration, which increases up to 800 arc sec for
material with a 35% of Al. Room temperature Hall mobilities range from 140 cm2/Vs
in GaN to 50 cm2/Vs in Al0.35Ga0.65N layers.
Surface roughness was evaluated by atomic force microscopy (AFM) obtaining
typical rms values of 0.5 nm in GaN, increasing up to ~1.5 nm for Al0.35Ga0.65N.
Growth and characterization details were published elsewhere [[33]].
Si-doped GaN samples grown on Si(111) by
MBE present a FWHM of 8 arc min for the (0002) X-ray diffraction peak,
increasing up to 15 arc min for an Al content of 35%. A surface roughness of
around 4 nm rms was determined by AFM, without any significant dependence with
the Al content. Growth details are given elsewhere [[34]].
The nitride photodetectors received from
the DIE/UPM are planar AlGaN Schottky barrier photo-detectors [[35],
[36]]. The schematic structure of the
devices is shown in Figure 4. Ohmic contacts consist in a Ti/Al (300 Å / 700 Å)
bilayer, and Schottky contacts consist in semitransparent 100 Å disks with a
Ni/Au (300 Å / 1000 Å) pad. All the photodetectors present an active area of
200 to 400 µm.
|
|
|
Figure 4 a/ Schematic structure
of AlGaN Schottky photodiodes, and b/ normalized spectral response of the
devices measured with a Xe arc lamp.
Details of
the devices under study are summarized below :
·
M395 :
AlXGa1-XN:Si (250 nm) over AlXGa1-XN
(150 nm) on an AlN buffer and a Si (111) substrate (X ~ 0.08)
·
X262 :
AlXGa1-XN:Si (1.8 µm) on a GaN buffer, and a
sapphire substrate (X ~ 0.35)
·
X300 :
GaN : Si (1.7 µm) on a GaN Buffer, and a sapphire substrate
AlGaN
produces UV detectors with a cut-off between 295 nm and the plain GaN
cut-off at 360 nm, as shown in Figure 4b.
LETI MSM
devices have been illuminated with monochromated synchrotron light around the Carbon CK edge
(289 eV » 43 Å) where the penetration depth of the photons spans
from 100 nm to 1 µm. A
channeltron collected the photoelectrons produced by the impinging XUV photons.
The partial (PY) or total (TY) electron yield mode separated bulk from surface
properties [[37]]. A bias potential was applied between
the interdigitated electrodes. A floating picoammeter measured the current
flowing through the electrodes as a function of the bias potential, impinging
photon flux or energy. By varying the sample preparation (e.g. cleaning) and the electrodes geometry, some insight has been
gained into the physics of the signal collection. Results were obtained on the
surface vs. bulk properties as a
function of post-processing treatments, and on the efficiency of
inter-digitated devices. The detail of this campaign is given elsewhere [[38]].
Another similar XUV synchrotron campaign is accepted this year to test new
devices, and gain more insights.
1.
To the
extent of the experiment sensitivity, the volume (500-1000 Å) was shown to
be devoid of non-diamond bonds.
2.
QE curves
could not be obtained with sandwich geometries [(b) or (c) of Figure
3]; the electron emission subsequent to photon
interaction on the diamond surface gives rise to the creation of a charged
layer that screens the electric field in the device volume.
3.
From current
measurements and wavelength calibration curves (using a GaAs photodiode), the
quantum efficiency of the diamond detectors could be estimated :
Figure 5 QE as a function of photon energy for an
inter-digitated device. 50 Volts were applied between the electrodes. The two
curves correspond to opposite polarities. The QE is defined as being the number
of sensed photon per incident photon at any
Raman
spectroscopy is a well-established method for characterizing CVD diamond films.
Confocal micro-Raman imaging using a microscope and a motorized X-Y stage
allows the study of both interfaces as well as intermediate planes inside the
film. Because of its high spatial resolution (~1 µm), the potential
presence of sp2 bonded carbon or localized mechanical stress may be
examined specially at the grain boundaries. We aimed at confirming the absence
of graphite as observed on the same LETI sample in the synchrotron experiments
reported above. We have been also training to learn how to correlate with
electrical and UV properties in the future. The area was scanned with a
LABRAM/Jobin-Yvon instrument over 50x35 µm with 2 µm steps, and a
633 nm (1.96 eV) laser excitation. Inspection of
the recorded spectra did not reveal any presence of graphitic carbon. It was
observed that the baseline of individual spectra contains frequently small
lines at different wavenumbers changing from one point to another which origin
is unclear at the moment. Raman images of the FWHM distributions demonstrate
the quality improvement of the film with growth [[39]].
The overall FWHM diminishes when going from the substrate interface to the
growth surface from 3.4 cm-1 to 2.7 cm-1. At
both interfaces, the individual spectra exhibit particularly large lines but
splitting is not observed.
|
A |
B |
C |
|
D |
Figure
6 A/
Video
image of the scanned area as
seen from the film-air interface. One large crystal surrounded by others of
various sizes is clearly visible. B/ An image of the FWHM
map in the diamond line obtained by a curve fitting of the recorded Raman
spectra at a plane inside the sample provides a rapid inspection. The very high
quality of the diamond film is ascertained by the low median FWHM (2-3.5 cm-1).
Important deviations are reported in three dark spots. C&D/ Individual
spectra from the dark zones of (B). In (C) the diamond line is exceptionally
wide, whereas in (D) the line splits into two components. This very localized
behaviour has already been observed [[40]].
It is attributed to the effect of high shear stresses that enlarge the line
abnormally and finally raise the triple degeneracy into two or even three
components.
Electrical measurements have been carried out at
LGEP on the GPI and LETI samples. The flux was 4´1012
photons.cm-2.s-1 under steady-state illumination
conditions at 190 nm. The photocurrent data were recorded in the ohmic
region of the current - voltage characteristics. Owing to the large
thickness of the samples, it is assumed that all photons are absorbed in the
diamond film. Thus, from the photocurrent DI one can deduce the
mobility-lifetime product µt
(representative of the majority carrier transport) as µt = DI/q.h.x.F, q being the electron
charge, h the electrode length, x the applied electric field and F the photon
flux. The results are reported below. We observe that the photosensitivity
significantly increases with the sample thickness. It is known that in this
kind of polycrystalline material, the grain size increases with the film
thickness. The increase of the photosensitivity could also reveal that the
electrical grain quality is improving the same way. The different data obtained
on samples #81-1R and #81-1C show that the photosensitivity measured on
coplanar devices also depends on the surface treatment. Indeed, the additional
cleaning performed on sample #81-1C has improved the photosensitivity by a
factor of 10. The mt is of the same order for the LETI
samples : 10-8-10-6 cm2/V [[41]],
but an exact comparison will have to be undertaken with all devices in the same
state.
|
|
Thickness |
Configuration |
mt (cm2V-1) |
|
GPI #118 |
1150 µm |
5x5 mm2;
polished both sides,
30 µm removed from nucleation side. |
9,6×10-7 |
|
GPI #117b |
650 µm |
7x7 mm2;
polished both sides,
20 µm removed from nucleation side. |
1,22×10-7 |
|
GPI #81-1C |
~80 µm |
5x5 mm2;
oxidized in chromium
acid. Non-polished, cleaned surface. |
5,9×10-8 |
|
GPI #81-1R |
~80 µm |
5x5 mm2;
oxidized in chromium
acid. Non-polished surface. |
5,74×10-9 |
We report here on preliminary tests made with
the UV lasers of the LPL facility in July 2000. GPI diamond photoconductors and
UPM nitride diodes were submitted to UV pulses (a few ns, 12 Hz) from an
ArF laser at 193 nm. The spot size was 20 µm at the focal point.
These experiments will give essentially access to 2 types of results :
evaluation of the dynamical mt product at the same wavelength as in §3.4, and
small scales sensitivity maps. However the quantitative interpretation is not
yet done; raw measurements are presented. An XYZ picomotor stage is
operational, but non-linearities currently prevent the production of
homogeneity maps.
|
|
Figure
7
The left column corresponds to a nitride Schottky diode, the right column to an
MSM diamond device. Responses are fast in both cases.
From the data, the diamond MSM is 3 to 5 times
faster than the nitride Schottky. Conversely, the nitrides can lead to a signal
10 times larger under the same flux conditions. However, the
GaN/AlGaN devices being Schottky barriers, they have a larger capacitance and
thus a slower time response and higher responsivity,
so differences are related to the different structure of the
devices. Research on nitride
metal-semiconductor-metal structures is currently been developed in the
consortium with promising results [[42]].
Comparing the nitrides mutually to M395#5 gives 1 a.u. (arbitrary unit) for
M395#5 (Æ = 400 µm), 7.2 a.u. for
X262#9 (Æ = 400 µm) and 5.4 a.u.
for X300#2 (Æ = 200 µm) which sorts
their performances like at higher wavelength. The lower
response in M395 is due to the lower structural quality of AlGaN material grown
on Si(111), as already reported [24].
Although
preliminary, the reported results look promising. More work needs to be done,
and this will happen in the following directions : the same samples will be
characterized in the EUV using the IAS synchrotron beamline facility, and by
AFM techniques at the LVSM/KUL laboratory. A new lot of optimised devices will
also undergo a full range of characterizations, including the ones described in
this paper. In parallel, electrical tests and modelling will be achieved in an
attempt to correlate all spatially resolved properties. At present, whether
diamond or nitride is superior is undecided, but by taking advantage of the
gained insights, we expect to progress toward the advent of the predicted
sensors. Updated information will be found at http://bold.oma.be.
This project
is supported by the CNES agency. The authors acknowledge the LURE for providing
time on the Super-Aco synchrotron, Jobin-Yvon for the micro-Raman experiments,
LGEP for the electrical tests, and LPL for the laser facility. We gratefully
thank Dr. Mourad Idir, Dr. Jean Larour, Dr. Jean Manca,
Dr. Denis Mencaraglia, Dr. Alessandro Mirone, Dr. Milos
Nesladec, and Dr. Edouard Rzepka for many fruitful discussions.
[1]
Royal Observatory of Belgium, Brussels, Belgium
Corresponding author: J-F. Hochedez, Royal Observatory of Belgium, Solar Physics Department, Circular Av. 3., B1180
Brussels, Belgium
Tel: +32 2373 0302, Fax: +32 2374 9822, email : hochedez@oma.be, http://bold.oma.be/
[2] LETI(CEA - Technologies Avancées)/DEIN/SPE, Saclay, France
[3] Laboratoire de Physique des Lasers, Villetanneuse, France
[4] Laboratoire de Spectroscopie Atomique et Ionique, Orsay, France
[5] Institut d'Astrophysique Spatiale, Orsay, France
[6] Laboratoire pour l'Utilisation du Rayonnement
Electromagnétique, Orsay, France
[7] Laboratoire de Génie Electrique de Paris, Gif/Yvette, France
[8] Jobin-Yvon / Horiba, Palaiseau, France
[9] Laboratoire d’Etudes des Propriétés Electroniques des
Solides, Grenoble, France
[10] Centre de Recherche sur l'Hétéro-Epitaxie et ses
Applications, Valbonne, France
[11]
Departamento. de
Ingeniería Electrónica (DIE), Universidad Politécnica de Madrid (UPM), Madrid,
Spain
[12]
General Physics Institute of the Russian Academy of Sciences, Moscow, Russia
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