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1.INTRODUCTIONAdvances in imaging solutions are a key contributor to commercial semiconductor growth. This is due to the increasing use of visible imaging technology in many applications. Space imaging is also experiencing a rapid growth, especially in New Space markets where the detectors are at the centre of many systems. This growth takes advantage of the advances in commercial technology to enable more complex missions with ever reducing development timescales. The route to support such rapid evolution is to innovate on technologies for higher intrinsic detector performance, more features and increased electronic integration. Teledyne-e2v presents the results covering the latest innovations for CCD, CMOS detectors. We present results on a new CCD for space mission: the coronagraph detector on the Nancy Grace Roman Space telescope, which will represent the first used of an electron multiplication CCD (EMCCD) in a major space mission. In addition, large area CCDs continue to be used when large arrays are required, for example in SMILE. CMOS image sensor are now used for the majority of space missions and continue to offer both improved performance and features. Three CMOS imagers and their measured performance will be presented with a focus on noise performance. CIS300 a large area 9k x 8.6k 10 μm pixel pitch detector featuring high speed, high dynamic range and ultra-low noise technology enabling sub electron performance. CIS220 a HiRho version of CIS120 (selected for ESA’s CO2M Copernicus mission) with a significant increase of the QE times MTF figure of merit in Near-Infra-Red with a QE of 60% at 950nm and an MTF of 0.55. CIS125 is the latest product from the TDI charge domain family for high resolution earth observation with high full well capacity of 30 ke- from a 5 μm pixel pitch. The last section will cover electrical interface choices which play a key part in determining the complexity of integration of the detectors with the focal planes and front end electronics. 2.CCD TECHNOLOGYCCD technology remains an important part of the detectors delivered by Teledyne-e2v for space missions. In the section an update on two more recent programs are presented: EMCCD for NASA’s Nancy Grace Roman Space Telescope and CCD for soft X-ray astronomy applications SMILE. 2.1EMCCD (electron multiplying CCD) for space science and astronomyThe CCD311-20 has been developed for use in the Coronagraph in NASA’s Nancy Grace Roman Space Telescope (RST, formerly known as WFIRST). The CCD311-20 is largely based on the CCD301-20 test chip, which itself was a variant of Teledyne e2v’s commercial CCD201-20 sensor. The CCD201-20 is a frame transfer EMCCD with an active imaging area of 1024 x 1024 13μm square pixels, designed for back-side illumination. For the RST CGI the back-surface light shield is removed from what was previously the store section, which allows the bottom half of the pixel array to be used for imaging. The key features of the CCD311-20 are summarized in Table 1 and more information on the sensor development and characterization can be found in Harding et al. [1]. Table 1:EMCCD CCD311-20 key features.
For the test chip design and characterization test activities, the CCD311 has the following changes from the CCD301 test chip design:
The CCD qualification phase of the program for RST CGI is complete with the production test phase due to start imminently. 2.2CCD for soft X-ray astronomy applications - SMILEThe Solar wind Magnetosphere Ionosphere Link Explorer (SMILE) is a soft X-ray mission observing photon energies of 200 eV to 2000 eV. This mission is a collaboration between ESA and Chinese Academy of Science [2]. For this mission the Teledyne e2v CCD370 has been selected. To minimise the CCD CTI degradation due to proton radiation impact, the focal plane has a temperature control to below -100°C. The CCD characteristics are given in Table 2 along with the schematic of the CCD370 in Figure 2. Table 2:CCD370 main characteristics.
Notes: 1- When operating with two adjacent phases held high. Defined as the point at which the response is non-linear. Measured using flat-field illumination. 2- Calculated with a camera bandwidth of 15 MHz predicted with single ended readout. The detector used for the PLATO mission, CCD280, has been used to predict the CCD370 post radiation performance [3]. The results show that the CCD370 will meet the end-of-life performance when the temperature is kept below -85 °C. Figure 3 (figure 13 from [3]) shows the CTI performance post annealing. The program is now moving to the lot acceptance testing (LAT) phase for flight model (FM) delivery. The SMILE mission has the capability to cool the image sensor down to cryogenic temperatures during evaluation testing to correctly evaluate the CCD end-of-life performance. 3.LARGE AREA CMOS DETECTOR DEVELOPMENT3.1Large area CMOS development from Teledyne e2vTeledyne e2v has developed a new CIS300 family of CMOS detectors to specifically address astronomy, space, low noise and high dynamic range applications while being a platform that can be adapted with minimum risk for many other specific applications. Teledyne e2v has completed the design of the first two products from this family: CIS301 and CIS302, which is the high NIR sensitivity version of CIS301 using the HiRho technology. This platform is the results of years of R&D innovation re-using silicon proven blocks from various projects. The key innovations that will be discussed in this section are:
CIS300 a flexible large area detector platform The CIS301 is a large area backthinned CMOS image sensor in a 3-sided close buttable package (See Figure 4 and Figure 5). It features:
The CIS302, second product of the family, is the HiRho version of the CIS301:
Package designed to be 3-side buttable (Figure 5).
The detectors predicted performance are reported in Table 3. The family is built on a 2D stitch platform which enables different detector sizes to be manufactured with the same mask set as shown Figure 6. Further the column readout for the family is based on a 5μm pitch making the platform suitable for pixel pitches of 5μm and larger. Table 3:Performance CIS301 and CIS302 detectors.
The CIS300 platform has been built on the heritage of silicon proven blocks and technologies. The low noise approach in particular was important and was addressed by 5 design considerations (represented Figure 7):
These 5 points are the focus of the next sections. 3.2Large area with High CVFTo achieve noise floor below 2 e-RMS CIS300 family relies on a high gain of 80-90μV/e- at sense node. This is higher than the typical achievable value from standard imaging process which is more around 50-60μV/e-. In order to reach 80-90μV/e- some specific design technics must be considered. Although several generations of detectors have achieved these high values a summary of the technics used for CIS300 is presented below. In order to achieve 80-90μV/e- three main considerations have been looked at:
The high CVF brings a lower sense node FWC as a consequence. It was therefore important to design a reset scheme and ADC to enable the largest possible voltage swing at the sense node by:
Although this does not impact the noise performance it helps with dynamic range by optimizing the FWC. The first large area high CVF and low noise CMOS detector demonstrated by Teledyne e2v is the CIS113, developed as part of the TAOSII mission [4]. This was a large area CMOS detector (1920 x 4608 Pixels of 16μm square) with low noise, below 3 e-RMS, and a reasonable FWC of 20 ke-. The pixel was a 5T structure similar to CIS300 pixel. The CIS113 was used in cryogenic environment which enabled the assessment of performance across a wide temperature range. The figures below shows that CVF increases (Figure 9) with lower temperature while the noise floor in electron remains constant (Figure 10). This is explained by the fact that the 1/f noise appears first as a current from the in-pixel source follower that is integrated into the column and sense node capacitances. As the temperature reduces the noise in μV increases (Figure 10) proportionally to the decrease of the sense node capacitance (or increase of the CVF) keeping the ratio of CVF increase to noise in μV constant. The implication is that the optimum sizing for the in-pixel source follower is in relation between its parasitic capacitance and the sense node targeted capacitance. Further detail can be found in [5]. Note that CIS113 is now a device in production. Having increased the gain as much as possible (using standard design rules) within the technology and design capabilities the next step was to improve the in-pixel CVF distribution across the large pixel area. This has been achieved with the implementation of HiRho technology, which along with improving QE and MTF significantly improves the inpixel gain distribution 3.3Enhanced sensitivity and improved in-pixel gain distributionThe sensitivity of the device is also an important characteristic of photon starved applications especially for NIR and soft X-ray missions. Teledyne e2v has already successfully transferred the CCD back thinning capability to CMOS and more recently has implemented of its HiRho CMOS technology. The pixel of the CIS300 family has been designed with this technology. A weak point of CMOS technology is the photodiode depletion depth which is smaller in comparison to the CCD. This is due to the fact that CMOS uses lower voltages. This lack of deep depletion implies that once back thinned the total thickness cannot exceed around 10 μm without a strong MTF degradation, even when using high resistivity epitaxial material. This limits the QE in NIR. The HiRho technology addresses this dilemma. This technology consists of supplying a negative voltage, named reverse bias, to the back surface while preventing the transistor from leaking [6]. Figure 11 shows a representation where the Deep Depletion Extension (DDE) is a special implant added in the pixel to protect the in-pixel transistors from the reverse bias. This technology has been implemented successfully as part of a European Space Agency GSTP funded program. The device designed (CIS22) is a HiRho version of the CIS120 general multi-purpose detector, 2k x 2k, 10 μm pitch, 5T pixel with global and rolling shutter operation. This device has been selected for ESA’s Copernicus CO2M mission) [7]. The QE and MTF have been measured for two EPI thicknesses of 17 μm with -6 V reverse bias, and 33 μm with -20 V reverse bias, see Figure 12 and Figure 13. The MTF is almost a constant across the wavelengths which demonstrates full depletion, although the values are slightly lower than the perfect theoretical value and slightly lower for the 33 μm thickness compared to 17 μm. This is explained by the aspect ratio between the pixel pitch of 10 μm and the thicknesses (17 μm and 33 μm). Some electrons can escape the pixel depletion region due to lateral diffusion to be captured by a neighbouring pixel. Nevertheless, these results show an important sensitivity increase in the NIR compared to the CIS120 non-HiRho detector. The QE response of CIS220 is significantly higher at wavelengths above 700 nm and almost double from 850 nm onwards for the 33 μm thick device compared to the CIS120. Importantly MTF performance of the CIS220 is not compromised by using thicker silicon and is improved compared to CIS120. It is worth pointing out that as the QE roll off appears later, the fringing effect is reduced improving performance for narrow wavelength bandwidth applications like hyperspectral imaging or spectroscopy. This is another important key point of this technology. The in-pixel gain distribution of the HiRho device is also significantly improved. The CCF (Charge Conversion Factor, digital equivalent of CVF for analogue devices) has a much tighter distribution. This is key for large area devices and critical for sub electron performance. Figure 14 reports a comparison between the distribution of CCF for CIS120 (non-HiRho) and CIS220 (HiRHo with 17μm thick EPI). A substantial improvement of 2 to 3 can be observed. The two devices have been tested on the same camera using the same analysis software. Further CIS220 was expected to have a good Parasitic Light Sensitivity (PLS) performance as it is using thick material (17μm EPI) and it is fully depleted. The left graph Figure 15 indicates that PLS performance in percent is constant up to saturation level and after this point the PLS increases. This right graph Figure 13 shows a decrease of PLS performance with longer wavelength which is expected as the device is back illuminated and therefore at longer wavelength the electrons are generated too close to the sense node. The observation can be categorized as:
Note that CIS220 is targeting to close TRR in coming months. A campaign of radiation is planned by end 2022. 3.4Column amplifier and Ultra-Low noise in-pixel source follower:Figure 16 is an illustration of a typical readout out digital path with a column PGA (Programmable Gain amplifier). For the CIS300 family the gains proposed varies from x 1 (bypass), x 2 to x 31. A similar approach was already used successfully on CIS124 [8]. This is a large array detector of 800 x 800 4T pixel, with low noise (3 e-RMS) and high frame rate (700 fps) designed for the ELT program as a wavefront sensor for ESO. Since the noise target was below 3 e-RMS PGA in this case had a gain of only up to x 8. However, as the CIS300 family is targeting a noise floor below 2 e-RMS and even sub electron in some mode the gains of the PGA needed to be increased. The choice of gains is also a function of the ADC noise floor. Here we have implemented a single slope ADC from industrial application optimized and featuring a noise floor below 100 μVRMS. Between the PGA and ADC a correlated double sampling (CDS) circuit is used to remove KTC noise and very low frequency and very high frequency noise components as the CDS acts as a bandpass filter. Figure 17 reports CIS124 noise floor versus PGA gain showing a significant noise reduction. Note that CIS124 is now in its production phase. To fully take advantage of the high CVF, the reduction of in-pixel gain distribution and column PGA structure it was important to have a tighter in-pixel source follower noise distribution. A new structure called ultra-low noise has been successfully experimented on silicon. Figure 18 shows a significant improvement in the noise tail. Further we can see a mean value measured at 1.6 e-RMS with a modest CVF of 70μV/e-. This value is now low enough to target sub electron performance using non-destructive readout or multi-sampling technics. The CIS300 family targets a noise floor close to 1.6 e-RMS using high CVF, in-pixel ultra-low noise source follower with a tight distribution and a column amplifier to render the ADC readout noise negligible. The non-destructive read out or multi-sampling will further reduce the noise floor to achieve sub electron performance. These modes can be important features for applications where long integration time is used and where cosmic ray artefacts must be removed for instance. However, more work is required to choose the best option between non-destructive read out and multisampling. In CMOS technology non-destructive read out relys on building-up a voltage at the sense node. This node is not pinned and its dark current is significantly higher than the dark current of the photodiode. This might be a limitation post radiation and a multi-sampling approach with sub electron performance might be preferred in some applications. 4.TDI CHARGE DOMAINThe Earth Observation satellites uses linear TDI (Time delay integration) detectors to maximise the level of signal gathered in order to achieve the required signal-to-noise ratio (SNR) to at low ground sampling distance (GSD). In this section an update is reported on CIS125 a 5μm pixel pitch TDI charge domain CMOS detector. A testchip was first developed to establish the performance of TDI charge domain pixels of 5μm and 7μm pixel pitch with anti-blooming included. The first use of such pixel was for the development of CIS125 (Figure 19). This device development started under a CEOI EO Technology and Instrumentation Program funded by the UK Space Agency. And it has now has been selected as part of the ESA InCubed funding stream. The architecture developed is reported in Figure 20. This TDI charge domain detector is composed of 4 panchromatic (PAN) bands and 6 multi-spectral (MS) bands. The configuration reported here is optimised and each PAN and MS are composed of sub-TDI bands (A&B) that to enhance the full well by adding off-chip digital summation to the charge domain performance. The PAN and MS number of TDI lines were carefully chosen to optimise application needs versus silicon area. Each sub-TDI needs to be read out separately and therefore needs its own conversion. This is the equivalent of reading out 16 independent bands. This implies that each quarter of line is dedicated to the conversion of a 1 PAN and 1 MS as shown Table 4. More information on the implementation of this device can be found in [10]. Table 4:Configuration for CIS125.
Table 5:PAN and MS readout timing organisation.
The pixel, Figure 21, is a 4 phases (P1…P4) CCD structure, with gated anti-blooming (AB). This sensor is a stitched device with 16k columns for the PAN bands and 8k columns for the MS bands. The pixels are 5μm square and for the PAN band and 10μm square for the MS band, see Table 1. To speed up the frame rate the sensor uses a high speed ADC per column allowing 12 bits conversion in 0.9μs. This is a single slope ADC architecture with a counter generating ten gray codes and four phase-shifted unary codes providing 12 bits output in total at very high line rates. The column readout path is illustrated Figure 18. A single read path is shared between all bands to implement a maximum number of bands without the need of 2D stitching technology and optimising power consumption. The data resulting of the image conversion is then sent to a gigabit transmitter (GTX) composed of a serialiser working in double data rate mode (DDR) at 3.6 GHz operation and a Common Mode Logic (CML) data driver working at 2.8 Gb/s. The high speed CML output driver standard has been selected to minimize the number of outputs reducing the complexity of any associated front end electronics. Input signals such as clock, integration control and SPI interface use LVDS format. A key parameter for CMOS TDI technology is the Charge Transfer Inefficiency (CTI) performance. This also indicates the maximum FWC of the pixel before the pixel changes from a buried channel operation to surface Channel. The latter is not preferred in space applications because the post radiation degradation will affect the CTI and hence MTF performance. This is not the case for a pixel working in buried channel mode only. In this section the author will refer the FWC obtained in buried channel operation as CTI FWC and a FWC obtained in surface channel operation as saturation FWC. The pixel was initially designed and optimised on a testchip. This testchip also included a 7 μm pixel version. Results are given in Figure 22 of the CTI curves with FWC associated obtained on both 5μm and 7μm pixel pitch of the testchip using a back illuminated version, backthinned down to about 12μm. CLK_HIGH is the high voltage of the phase (P1… P4). This voltage is adjusted for best CTI FWC. Preliminary performance of 5μm pitch PAN and 10μm pitch MS of CIS125 confirms the good results from the testchip. The Figure 24 shows preliminary silicon measurements from the CIS125 PAN1A channel:
The Figure 25 shows the silicon measurements done of the MS1A from CIS125:
The performance for CIS125 looks very promising with a high CTI FWC of 30 ke- and saturated FWC of 45 ke- per PAN channel. Including the digital summation of PAN A and B will bring the CTI FWC to 60 ke-. The CIS125 front illuminated version is expected to be fully characterised by end 2022 and the back illuminated version early 2023. 5.ELECTRICAL INTERFACEThe electrical interface plays a critical role in the design of an image detector since some trade-off depend on it, such as:
For example CIS300, CIS125 or ChromaD (an IR detector from Teledyne [11] selected for instance for ESA’s CHIME program) all have implemented a serialiser with CML output standard. This standard enables operation at much higher frequency than LVDS and therefore enables to reduce number of pins (video channels) and static current. This approach will also cover future generation of detector running at faster frame rate with more data to output. Furthermore the CML format can drive meters of cables. This allows large part of the front end electronic to be positioned remotely from the detector and therefore more protected from radiation. This is obviously interesting for large satellites. In order to ease the integration at high speed and with large volumes of data the output format is of data stream type (Figure 26) and includes per line:
This data stream approach includes the clock in the data transmitted removing the need for a clock driver. Further since the clock is simply recovered from the data it removes the problem of the setup and hold constraints between data and clock too small at such high frequency and difficult to master at system level. The encoding 8b and 10b guarantee enough data transition to secure a good clock recovery (Figure 27). 6.CONCLUSIONSTwo new CCD have been presented including an EMCCD for the NASA’s Nancy Grace Roman Space Telescope. This will be the first EMCCD selected for a space mission. A large CCD for soft X-ray astronomy applications SMILE was also presented. The large 2D array CMOS detector, 9000 x 8600 with 10 μm 5T pixel pitch, from CIS300 family was presented with a focus on the different technologies used to achieve low noise: high CVF, use of column amplifiers, improved sensitivity and in-pixel gain distribution, implementation of ultra-low noise in-pixel source follower and new features such as nondestructive readout and multi-sampling. The various programs on which these technologies have been verified on silicon were presented indicating a high level of maturity. The HiRho version of the large area array (CIS302) is expected to have a noise floor below 2 e-RMS with high gain and a FWC of 140 ke- using a lower in-pixel gain. The preliminary results of CIS125; a 16k column charge domain TDI 5 μm pixel device with anti-blooming are discussed. The first results confirm the pixel performance with a CTI FWC of 30 ke- (45 ke- saturated FWC) per PAN band. Including the digital summation of the paired (A and B) PAN bands gives a CTI FWC of 60 ke-. This confirms earlier back illuminated test chip measurements also reported in this document. The results of a 7 μm pixel array on the test chip are also reported, which give a CTI FWC above 90 ke- per band. Finally the importance of the electrical interface in saving power and reducing the number of pins while running at higher frame rates and with high data handling capability was discussed. 7.ACKNOWLEDGEMENTThe author gracefully acknowledges the support to write this paper from Katherine Lawrie, Iain Reads, Paul Jerram and Dave Barry from Teledyne e2v and Open University and in particular Konstantin Stefanov for the characterization work of the TDI charge domain testchip. REFERENCESL. K. Harding et al.,
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