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Health and cleanliness of the XMM-Newton science payload since launch
M.G.F. Kirsch1a, A. Abbey c, B.Altieri a, D. Baskill c, K. Dennerl b, J.van Dooren e, J. Fauste a, M.J. Freyberg b, C. Gabriel a, F. Haberl b, H. Hartmann d, G. Hartner b, N. Meidinger b, L. Metcalfea, B. Olabarri a, A.M.T. Pollock a, A.M. Read c, S. Rives a, S. Sembay c, M.J.S. Smith a, M. Stuhlingera, A. Talavera a a European Space Agency (ESA), European Space Astronomy Center (ESAC), Villafranca, Apartado 50727, 28080 Madrid, Spain, bMax-Planck-Institut fЭr extraterrestrische Physik, Giessenbachstrasse 1, 85748 Garching, Germany, cDept. of Physics and Astronomy, Leicester University, Leicester LE1 7RH, U.K., dEADS Astrium GmbH, eESA, ESTEC, The Netherlands
ABSTRACT On December 10th 2004 the XMM-Newton observatory celebrated its 5th year in orbit. Since the beginning of the mission steady health and contamination monitoring has been performed by the XMM-Newton SOC and the instrument teams. Main targets of the monitoring, using scientific data for all instruments on board, are the behaviour of the Charge Transfer Efficiency, the gain, the effective area and the bad, hot and noisy pixels. The monitoring is performed by combination of calibration observations using internal radioactive calibration sources with observations of astronomical targets. In addition a set of housekeeping parameters is continuously monitored reflecting the health situation of the instruments from an engineering point of view. We show trend behaviour over the 5 years especially in combination with events like solar flares and other events affecting the performance of the instruments. Keywords: XMM-Newton, calibration

1. INTRODUCTION
Scientific instruments operated in the unfriendly environment outside the atmosphere of the Earth suffer from extreme conditions due to radiation, temperature and low pressure. All three factors and their combinations can cause rapid aging and foster contamination of the instruments. This can lead, in the case of radiation for example, to effects ranging from a degradation in Charge Transfer Efficiency (CTE) of the CCDs, up to a fatal failure of the whole instrument. Should contamination occur, the effective area of the instruments will be affected lowering the efficiency of response and introducing additional absorption edges in the measured spectra. Tracking the health and cleanliness status of the system at all stages of the mission is clearly fundamental to ensuring sustained performance of the instruments and to preserving the quality of the scientific data. Vigilant monitoring is linked to appropriate safety and recovery procedures in critical cases, and in general can be expected to lead to instrument calibration refinements and refined scientific data output. XMM-Newton1 was launched in December 1999 on an Ariane 504 rocket from French Guyana. Its six instruments are operated in parallel through the course of a 48-hour highly elliptical orbit. Three Wolter type-1 telescopes with 58 nested mirror shells focus X-ray photons onto the five X-ray instruments comprising the European Photon Imaging2,3 Camera (EPIC) and the Reflecting Grating Spectrometers4 (RGS). The Optical Monitor5 (OM), employing a 30 cm Ritchey ChrИtien optical telescope, can perform parallel optical observations of the same field. EPIC is comprised of three cameras employing two distinct detector technologies. The two EPIC-MOS cameras use front illuminated EPIC-MOS (Metal-Oxide Semi-conductor) CCDs as X-ray detectors, while the EPIC-pn camera is equipped with an EPIC-pn (p-n-junction) CCD which has been specially developed for XMM-Newton. EPIC provides spatially resolved spectroscopy over a field-of-view of 30' with moderate energy resolution. The EPIC cameras can be operated in various observational modes related to the specific readout strategies in each mode. For a detailed description of the modes see Kendziorra et al. (1997)6, Kendziorra et al. (1999)7, Kuster et al. (1999)8 and Ehle et al. (2003)9. The RGS is designed for high-resolution spectroscopy of bright sources in the energy range from 0.3 to 2.1 keV. The OM extends the spectral coverage of XMM-Newton into the UV and optical, and thus opens the possibility to test physical models of source spectra against data over a broad energy band. The six OM filters allow colour discrimination, and there are two grisms, one operating in the UV and one in the optical, to provide low-resolution spectroscopy.
1

mkirsch@sciops.esa.es +34 91 8131 345; fax +34 91 8131 172


2. WHAT DOES HEALTHY AND CLEAN MEAN?
2.1. Instrument internal ­ Radiation CCD's are sensitive detectors of radiation. That holds true whether the radiation is electromagnetic, from the infrared to the gamma ray range, or ionising particle radiation. The CCDs of XMM-Newton's X-ray instruments are designed to respond to X-ray radiation in the energy range from 0.1-15 keV. Nevertheless, they also detect particles, and photons in other energy ranges. We therefore divide the radiation detected by the XMM-Newton CCDs into 4 categories: X-ray radiation, optical radiation, "soft"-particle radiation, and "hard"-particle radiation. Optical radiation seen by the detectors has to be taken into account in the scientific analysis of XMM-Newton data, but neither does it change the properties of the devices with time. The critical component, therefore, from the point of view of instrument aging, is the particle radiation. The soft component consists of low energy protons ("soft" protons), with energies ranging up to 300 keV, that are funnelled by the XMM-Newton mirrors under grazing incidence to fall on the detectors in just the same way as X-ray photon events. Upon hitting the CCDs the protons can damage the silicon lattice and the electrode structures at the surface of the CCDs. This is problematic for the front-illuminated EPIC-MOS CCDs, leading to reduction of the Charge Transfer Efficiency (CTE) and degradation of the energy resolution. To protect the EPIC-MOS cameras from those soft protons the filter wheel is moved to a closed position in periods of high soft-proton flux. The term "hard"-particle radiation refers to cosmic background radiation particles and associated secondary particles which are not focussed by the mirrors, and may consist of protons, nuclei or other Minimally Ionising Particles (MIPs). These can also cause damage to the instruments. Regardless of their intrinsic incident energy MIPs deposit ~ 2 MeVg-1 in target material. A MIP can easily penetrate the camera boxes from any direction and deposit energy in the CCD. 2.2. Contamination A contaminant is any material in the whole light path of an instrument that should not be there and which affects the efficiency of the instrument. This can be, in the simplest case, frozen water showing-up as oxygen features in spectra, or it might be any other substance that might out-gas from the spacecraft and freeze onto any of the instruments. The two main categories of contamination are particulate contamination, which has almost energy-independent impacts on the effective area, and molecular contamination, the PFO (PPM) FOR 1 % effects of which are energy dependent. OPTICAL
ELEMENT GRAZING ANGLE EFFECTIVE AREA REDUCTION

2.2.1. Molecular contamination Grating 2.275 deg 200 Molecular contaminants typically consist of Mirror 1 39.7 arcmin 29 hydrocarbons or water. The hydrocarbon Mirror 24 26.6 arcmin 21 contamination levels are expected to be of the order Mirror 58 17.4 arcmin 13 of 5-10 10-8 g.cm-2 for smooth surfaces under Table 1: Reduction of effective area due to Particle Fall Out (PFO) (Note that atmospheric conditions in the cleanest environments the unit ppm relates to surface coverage. 1ppm means that in total 1 mmІ of 1 (XMM-Newton-SOC-PS-TN-0003). With a typical mІ is covered or shadowed by particles) -3 density of 1 g cm these values correspond to a monolayer thickness of 5-10 е. Simulations from the work reported in the above technical note show that for molecular contamination with hydrocarbons the reflectance of the hydrocarbon film over the gold coating is similar to that of a bilayer made up of a low and a high Z material. Indeed the reflectivity increases at low energies and is gradually less affected towards higher energies. For energies below the Au-M absorption edge at 2.2 keV the change in absolute reflectivity is about 0.2 % per е of hydrocarbon. 2.2.2. Particulate contamination Particles absorb and diffractively scatter X-rays. Reflective scattering can be neglected at X-ray energies and with a good approximation it can be considered that grains absorb X-rays passing through their geometrical cross-section. The dust fractional coverage of a mirror surface is related to the Particle Fall Out (PFO). That typically depends on the exposure time of the mirror surface in a clean room. Table 1 gives estimates of the PFO that would lead to a 1 % change in effective area. Although the change of effective area due to particulate contamination is almost energy independent, slight energy dependence is introduced since effective area vignetting by dust depends on grazing angle. At high energies, where only the inner mirror shells contribute to the effective area, the impact of particulate contamination on relative effective area variation can be expected to be higher by almost a factor of 2 than at low energies, where the


collecting area of the outer mirror shells dominates. Table 1 shows also clearly that mirrors are much more sensitive to contamination than gratings due to their shallower grazing angles. 2.2.3. Cleanliness Requirements Pre-launch limits for contamination levels of key components in the optical path were: REQUIREMENTS Mirror Modules Reflecting Grating Assembly PARTICULATE CONTAMINATION < 70 ppm < 350 ppm MOLECULAR CONTAMINATION < 8 10-8 g/cm2 < 4 10-8 g/cm2

In order to fulfil the requirements of an absolute effective area accuracy of 10 % at any energy between 0.1-10 keV and a relative accuracy of better than 3 %, until the end of the XMM-Newton lifetime, a maximum of 200 ppm for particulate contamination and 2 10-7g.cm-2 for molecular contamination should not be exceeded. Note that after an XMM-Newton contamination working group meeting in November 1995 the contamination budget for the mirror shells was revised anticipating that contamination levels could reach 140 ppm of particulate contamination and 1.5 10-7 g cm-2 of molecular contamination between the end of the ground calibration tests at the PANTER test facility and the start of the in-orbit operations. This is a factor of 2 above what was foreseen in the original requirements. 2.3. The importance of contamination monitoring Contamination on instruments can significantly change the detection efficiency. This may for example lead to a change in effective area. Where the change is detected and can be quantified the calibration can be adjusted and scientific data quality is not greatly affected. Contamination, if it is substantial, may be revealed through its impacts on scientific results, but where it is slight it may be very hard to detect, since it may mimic a slightly higher astrophysical absorption column density in astronomical spectra. Therefore it is crucial to perform systematic contamination measurements before and after launch in order to fully track the contamination history. 2.4. Contamination prevention In the design phase the cleanliness requirements have been accounted for by making the mirror modules, the telescope tube and the experiments separately closed units having their own doors and purging devices. The tube and the mirror modules had to be kept closed, except for relatively brief moments during optical testing. Special mirrors were used for alignment such that the flight mirror units did not have to be opened. All mirror modules, the telescope tube and the optical monitor have been continuously purged with pure nitrogen or synthetic air. The EPIC cameras were evacuated while the RGS cameras were pressurised with nitrogen. The telescope tube is sealed from Carbon Fibre Reinforced Plastic (CFRP) out gassing towards the inside by a continuous aluminium foil, acting as a vapour barrier. In addition the aluminium foil is covered for stray-light suppression with a 25 m thick black kapton foil that is glued with low outgassing adhesive. After thermal-vacuum testing in the Large Space Simulator (LSS) at ESTEC, tape-lifts measured 50 ppm average inside the tube, respectively < 0.1 10-7 g cm-2 from wipe tests.

3. XMM-NEWTON OPERATIONS - 5 YEARS IN ORBIT
3.1. Thermal history The EPIC-pn-CCD camera aboard XMM-Newton shows a correlation between the gain in the signal processing chain and the temperature of the quadrant boxes, which house the CCD electronics. A temperature decrease of 1 C corresponds to an energy shift of ~0.4 adu (~ 2 eV) at the Mn-K energy of 5.9 keV (Dennerl 200116). Figure 1 shows the EPIC-pn quadrant box temperature for quadrant Q1 (where the on-axis CCD is located) for all available Full-Frame mode data, averaged over an exposure. The step-like feature originates in the intrinsic resolution of the temperature sensor data acquisition. The line is a linear regression to most of the data (during revolutions 120-140 sometimes EPICMOS or RGS was switched off and the temperature environment was different for this known reason, the fit uses only revolutions later than 150). There is a clear trend, seen in fact for all modes, with a temperature decrease of about 3.2 mK per revolution (~ 0.59 C per year).


A similar trend has independently been found for the EPIC-MOS electronics boxes and also for the total satellite temperature. It has been suggested that the known orbit drift and consequently reduced reflected emission from Earth decreased the temperature. Up to now no significant drift in line energies of Al-K, Mn-K , and CuK in EPIC-pn could be identified. However, it should be noted that a small (< 10-5) systematic long-term variation of the EPIC-pn oscillator frequency has been found which could be related to the temperature variation described here (Freyberg et al. 200517). As another example of the housekeeping monitoring the temperature of all focal plane CCDs is shown in Figure 2. As a consequence of the cooling of the EPIC-MOS and RGS instruments (see Section 3.2) these temperatures drop at the end of 2002. Figure 2 shows, in addition, the

Figure 1: Evolution of the EPIC-pn quadrant box temperature

excursions of the temperature due to eclipse seasons when the cameras are switched off during spacecraft passages through the Earth's shadow and are, for safety reasons, heated with the substitution heaters. This causes an increase of the temperature. Moreover a seasonal effect is seen that causes a kind of wave structure in temperature with a maximum around Christmas. The increase of the temperatures only happens at the end and the beginning of the revolution and is due to the influence of the albedo of the earth. It is assumed that scientific data is not affected by those temperature excursions since scientific observations are only started when the nominal CCD temperatures are reached. 3.2. Cooling During November and December 2002 a series of operations Figure 2: Temperature of the XMM-Newton focal plane CCDs for all instruments. The data gaps at the end of one year are due to system were performed to lower the nominal operating temperatures memory problems at the time of recreating the data. of the RGS and EPIC-MOS instruments, and to subsequently re-establish their calibration. The purpose of the cooling was to move important detector characteristics back towards the values which they had earlier in the mission. Parameters such as CTE (and therefore energy determination and energy resolution), and number of hot pixels etc. had deteriorated since launch in the hostile space radiation environment. 3.2.1. Cooling the EPIC MOS cameras While ground-based software corrections for EPIC-MOS-CTE managed to recover most of the energy loss, inevitably the detector line-profile FWHM had widened due to imperfect correction and statistical noise of charge trapping. Since the EPIC-MOS CCDs are qualified to operate down to -130 C it was expected that an improvement would be seen in CTE at reduced temperatures (optimised at ­120 C). Many bright pixels had developed, as expected, due to radiation and micrometeoroid impacts. It was expected that, also for those pixels, cooling should have had a curative effect. The two EPIC-MOS instruments were cooled in the night of November 6-7 2002, with the instruments in Closed/CalClosed configuration. The instruments were cooled from the previous operating temperature of -100 C, down to ­120 C. The EPIC-MOS1 and EPIC-MOS2 cameras were cooled in parallel. The new temperature value was reached within 2.75 hours. The Charge Transfer Inefficiency (CTI=1-CTE) changed by a factor of 2-3 depending on the CCD considered. The serial CTI was unchanged. Prior to the cooling the CTE had tended to degrade, with much of the degradation occurring discontinuously in association with radiation bursts from solar flares. Following the cooling the CTE degradation evolves with the underlying slope, a trend unbroken even after strong solar flares in 2003 and 2004. That


means that the detectors are much more robust against radiation at a temperature of -120 centigrade. The energy resolution was improved by 13% and 17% for EPIC-MOS1 and EPIC-MOS2 respectively at Mn energies (6 keV) and by about 10 % at Al energies (1.5 keV), varying somewhat among the CCDs. The number of bad pixels in the Current Calibration Files was reduced by a factor of 2.6 (EPIC-MOS1) and 7.0 (EPIC-MOS2). The few remaining ones are mostly the defects from micrometeoroid impacts. We saw no change in the quantum efficiency following the cooling. Observations on the isolated neutron star RXJ 0720.4-3125 and the Vela SNR before and after cooling substantiate that statement. We performed, after cooling, a contamination monitoring using the SNR N132D, the isolated neutron star RXJ 0720.4-3125 and the Vela supernova remnant. There was no sign of post-cooling adsorption of contaminants onto the detectors, which had been the main perceived risk factor in the process. With this new thermal set point (-120 C), the EPIC-MOS focal plane is now sensitive to the thermal impact of the Earth at every perigee passage. Consequently, the focal plane temperature can increase to ­115 C at perigee. Note that the amplitude of the thermal excursion also depends on the relative alignment of Sun/Earth/Satellite. From an operational point of view it is important that the EPIC-MOS focal plane temperature is stabilized at ­120 C at the start of the observation window. Further studies have shown that this requirement is met even in the worst case. Nevertheless, in case a further cooling is to be performed in the future this operational constraint will have to be taken into account. 3.2.2. Cooling the RGS spectrometers The RGS CCDs were cooled to a new operating temperature of -110 C. The main result of cooling for RGS was a huge reduction in the incidence of flickering pixels. The CTI was restored to close to its preflight values. Previously poor CTI near the edges of the detectors, where it had been 100 times worse than for the inner regions, was almost eliminated. The CCD noise was greatly reduced, and the width of the noise distribution peak became, and remains, narrower than before launch. There is now just one hot column and one hot pixel in RGS2. 3.3. Radiation history, seasonal radiation The high fluctuations and variability of the particle background in the cameras was one of the main surprises and concerns after launch. It can Figure 3: Average level of soft-proton radiation events be divided into two main components: a) A rather quiescent component, seen by RGS through the XMM-Newton revolution is plotted against time since perigee passage (PP). This due to the interaction of high-energy particles (energies larger than parameter is a good indicator of soft-proton flaring. It about 100 MeV) with the structure surrounding the detectors and shows that the probability of high background periods is possibly with the detectors themselves, and its associated fluorescence, higher toward the perigee, with higher radiation at the and b) A variable and flaring component attributed to soft-protons (with beginning and end of the revolution, but with significant energies smaller than a few 100 keV), which are presumably funnelled asymmetry: Higher radiation is found on the descending part of the orbit. On average, toward the detectors by the X-ray mirrors and hence form a vignetted found between PP+6 hours and good observing time is PP-10 hours. The dashed background. This flaring component of the soft-protons was not horizontal line is 5 sigma above the quiescent level. foreseen before launch. The spectra of soft-proton flares are variable. The probability of encountering soft-proton flaring decreases with altitude (distance from Earth), as for higher-energy radiation detected by the Radiation Monitor (a few MeV) (see Fig. 3). Hence this population of soft-protons must be linked, to some extent, to the radiation belts, but in a much more unpredictable and loose way than is the case for higher-energy particles. A higher fraction of the descending part of the orbit (in-bound leg, toward perigee) is affected by radiation, as can be seen in Fig. 3, due to the offset and tilt of the geomagnetic axis with respect to the Earth's rotational axis. A seasonal effect can also be seen due to the one-year rotation of the magnetosphere and magneto-tail in the XMMNewton orbit reference frame (revolution of two sidereal days): the portion of the orbit crossing the magneto-tail and/or the night side of the magnetosphere is more prone to radiation flaring. In spring the descending part of the orbit is more affected, while in autumn the ascending part is affected. These two geometric effects lead to asymmetries in the radiation profile along the XMM-Newton orbit. Overall, up to 15-20 % of the XMM-Newton-observing time (the 40 hours available for scientific observations above the radiation belts, out of the 48 hour orbit) can be lost, although this is difficult to assess quantitatively as the impact of radiation on science output depends on the scientific goal of an


observation. This fraction of time lost is highly variable from revolution to revolution and observation to observation, but there is a higher probability that observations planned toward the end of the revolutions will be affected, where EPIC exposures have often to be aborted before their scheduled end times. The effect of soft-proton flaring is a bigger nuisance for XMM-Newton than for Chandra, for several reasons: Chandra's orbit brings it further from the Earth than XMM-Newton, so that it spends much more time above the region of quasi-trapped soft-proton clouds. XMM-Newton's effective area (i.e. capacity to collect X-rays) is much higher, by a factor of 5-10 depending on energy. It therefore not only collects more X-ray photons, but also focuses more soft-protons into the focal plane. 3.4. EPIC-MOS patch redistribution A small patch of anomalous responsivity has been found on the central CCD of each MOS camera by examining all archived observational data for the source1ES0102. In addition, a raster scan has been performed to identify positional and temporal variability of the patches. The patches have degraded over time. The locations of the patches are coincident with the nominal position of sources when placed at the two effective pointing boresights for XMM-Newton: the EPIC-pn and RGS boresights. The patterns coincide with the peak in received photon dose of the detectors. The patches cause a significant change in the low energy redistribution characteristics of the EPIC-MOS cameras, which is spatially and temporarily dependent. However the situation seems to have stabilised and the characteristics of the patches are not consistent with being caused by a contamination mechanism. Epoch dependent canned Response Matrices (RMFs), currently under test, will convey the characteristics of the patches to the user community for application in their data analysis. The task rmfgen, for release with v6.5 of the XMM-Newton Scientific Analysis Software (SAS), will be able to produce spatially and epoch dependent RMFs for all epochs and off axis angles.

Figure 4: Smoothed images of the SNR 1ES0102 in the 0.1-0.35 keV energy band. Left: EPIC-MOS1 Right: EPIC-MOS 2. Upper rev 247. lower rev 447

3.5. Impacts on CCDs EPIC cameras have suffered, so far, 4 events interpreted as micrometeoroid impacts in five years of in-orbit operation. These occurred in revolutions 107 (EPIC-MOS2), 156 (EPIC-pn), 325 (EPIC-MOS1), and 961 (EPIC-MOS1), and are understood to be the result of dust particles coming down the boresight direction and interacting with the mirror shells, so that they or the associated debris are channelled by the mirror shells onto the focal plane. The most recent event (discussed in more detail in Section 3.5.1 below) was by far the worst, leading to the loss of EPIC-MOS1 CCD6 (one of the 7 CCDs in the EPIC-MOS1 focal plane) in March 2005. For EPIC-MOS the impacts were characterized by an optical flash and the occurrence of FIFO data buffers full, and the sudden appearance of several high energy and high-recurrence frequency hot pixels. In the EPIC-pn case several new hot pixels also appeared within 1 frame time (Large Window mode, 48 ms) again pointing toward the impact of a dust micro-particle. RGS has not been affected so far, possibly because of the diffraction geometry leading to an off axis position of the RGS focal plane with respect to the mirror shells and the diffraction gratings. Assuming that the acceptance solid angle is about the same for dust particles as for X-rays, with reflections occurring for angles of incidence up to 3.5 degrees off-axis, one can derive a telescope effective aperture of 21.5 cm2Sr for an effective area of 1500 cm2, and hence one can estimate the rate at which particles may hit the focal plane using the micrometeoroid mass spectrum measured by GrЭn et al. (1985)10 and Divine (1993)11. The typical particle mass Figure 5: EPIC-MOS zeta pupis observations: at the patch matching the observed rate of events is m~10-13 g, corresponding to location on rev. 156 (black), at the patch location on rev. 542 a particle size of 0.2-0.3 m. These particles are either (red), patch location rev. 636 (dark blue), off-patch location interplanetary or interstellar dust, but are not linked to meteor rev. 903 (light blue) showers, which do not contain particles smaller than about 10-8 g.


3.5.1. Latest and severest EPIC-MOS impact As introduced above, at about 01:30 hrs. UT on 09 March, 2005, during XMMNewton revolution 961, an event was registered in the focal plane of the EPIC-MOS1 instrument. The characteristics of the event were reminiscent of very similar, but less energetic, events registered in the EPIC-MOS1 focal plane on September 17, 2001, the EPIC-MOS2 focal plane on August 12, 2002, and the EPIC-pn focal plane on October 19, 2000, which have been attributed to micrometeoroid impacts scattering debris into the focal plane. The consequences of the recent event have been the most significant. In the period immediately following the light flash it became apparent that EPIC-MOS1 CCD6 was no longer recording events, and that all CCD6 pixels were, in effect, returning signal at the saturation level. Standard recovery procedures were immediately applied, but had no effect on the observed behaviour, leading to the eventual conclusion that CCD6 had sustained terminal damage. New hot pixels were also recorded elsewhere in the EPIC-MOS1 focal plane. 3.5.2. EPIC-pn impact During revolution 156 about 35 individual bright pixels lit up out of approximately Figure 6: Exposure maps corresponding to 150000 pixels of the 6 cm x 6 cm EPIC-pn exposures before (upper) and after detector area. The amount of leakage current (lower) the loss of MOS1 CCD6 generated in the pixels cannot be explained by single heavy ion impacts. The only reasonable possibility found to explain the observation was that a micrometeoroid13, scattering off the mirror surface under grazing incidence, reached the focal plane detectors and produced the bright pixels. This proposal was studied experimentally, on the ground, at the Heidelberg dust accelerator. Micron-sized iron particles were accelerated to speeds of the order of 5 km s-1 impinging on the surface of an X-ray mirror under grazing incidence14. Figure 7: Experimental verification of The experiments micrometeoroid impact as result of the experiment at the dust accelerator. The SEM verified that a dust image shows the top view of a crater in particle under these silicon caused by a particle scattered off the conditions can cause mirror surface under grazing incidence damage consistent with the behaviour of the focal plane CCD-detectors of XMM-Newton. All the characteristics of the event and the damage could be reproduced in the laboratory. The formation of the bright pixels was caused by fragments of the primary dust particle.

4. INSTRUMENT PERFORMANCE MONITORING
4.1. Monitoring flow Since XMM-Newton is in continuous contact with its Figure 8: Science Operations Centre (SOC) at the European Space Evolution of the CTE of the EPIC camera CCDs for the energies of the Astronomy Centre (ESAC), near Madrid in Spain, we can internal calibration source at Mn, 5896 eV, (blue crosses) and Al, 1486 perform a real time health monitoring. The health eV (red triangles). Upper panel: EPIC-MOS, Lower panel EPIC-pn. The different blue and red tones in the upper pannel of the figure represent monitoring of the instruments is carried out in two steps. A the EPIC-MOS1 (light blue (Mn), orange (Al)) and EPIC-MOS2 (dark so called Instrument Controller (INSCON) monitors the blue (Mn), red (Al)). The discontinuity around rev.533 is related to the instrument performance 24 hours a day. Suspicious cooling of the EPIC-MOS cameras. Note that all EPIC-MOS CCDs have behaviour of the instruments is immediately reported to the recovered some CTE after the cooling. Only the EPIC-MOS1 boresight CCD has not recovered as strongly - as shown by the orange crosses. instrument teams at ESAC and the PI institutes for further investigation. Further monitoring is then pursued offline by instrument-dedicated teams.


4.2. EPIC Since launch the EPIC instrument consortium and the XMM-Newton SOC have performed an off line monitoring of the EPIC camera. It is separate from and complementary to the real time monitoring performed at the SOC by the INSCON team. The monitoring tools employed are largely automatic supporting the trend analysis of parameters which affect instrument performance and health. The main monitoring inputs are the regularly performed exposures with the filter in CalClosed position. Parameters monitored are charge transfer efficiency (CTE), energy resolution and gain, through the monitoring of the measured energies and widths of the internal calibration source lines. These parameters are essential for the reconstruction of photon event energy and system response, and are important diagnostics of instrumental health and performance. They therefore require close monitoring in order to detect, anticipate and possibly correct for larger than acceptable variations.

It is known that harsh radiation conditions may induce the formation of electron traps in the detectors, thus degrading the CTE. According to well-defined criteria the filter wheel is put in a closed position during periods of high background radi