Abstract
We report on the development of a polarization-sensitive dichroic (150/220 GHz) detector array for the Cosmology Large Angular Scale Surveyor (CLASS) delivered to the telescope site in June 2019. In concert with existing 40 and 90 GHz telescopes, the 150/220 GHz telescope will make observations of the cosmic microwave background over large angular scales aimed at measuring the primordial B-mode signal, the optical depth to reionization, and other fundamental physics and cosmology. The 150/220 GHz focal plane array consists of three detector modules with 1020 transition edge sensor bolometers in total. Each dual-polarization pixel on the focal plane contains four bolometers to measure the two linear polarization states at 150 and 220 GHz. Light is coupled through a planar orthomode transducer fed by a smooth-walled feedhorn array made from an aluminum–silicon alloy (CE7). In this work, we discuss the design, assembly, and in-laboratory characterization of the 150/220 GHz detector array. The detectors are photon-noise limited, and we estimate the total array noise-equivalent power to be 2.5 and 4 \({\text {aW}}\,\sqrt{{\text {s}}}\) for 150 and 220 GHz arrays, respectively.
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1 Introduction
Precise measurement of the cosmic microwave background (CMB) polarization at large angular scales enables us to characterize cosmic inflation, pinpoint the epoch of reionization, constrain the mass of neutrinos, and probe new physics beyond the standard model including early dark energy models intended to resolve the Hubble constant problem. However, characterizing the faint polarized CMB signal is challenging due to large polarized foreground contamination at millimeter wavelengths from galactic synchrotron and dust emission. It is therefore essential to pursue multi-band observations using large arrays of efficient background-limited detectors with excellent control over instrumental systematics.
The Cosmology Large Angular Scale Surveyor (CLASS) maps the microwave sky from the Atacama Desert in Chile at four frequency bands from 40 to 220 GHz, optimized for maximum signal to noise based on the atmospheric emission. The addition of a dichroic (150/220 GHz) detector array to the existing 40 [1] and 90 GHz [2] telescopes provides additional sensitivity to CLASS’s CMB observations and helps to characterize the dust foreground. The 150/220 GHz high-frequency (HF) instrument was delivered to and tested at the CLASS site in June 2019. The HF focal plane array consists of three detector modules, shown in Fig. 1, with 255 dichroic dual-polarization pixels in total. Each pixel consists of four transition edge sensor (TES) bolometers that couple to light through a planar orthomode transducer (OMT) [3, 4] fed by a smooth-walled feedhorn array made from an aluminum–silicon Controlled Expansion 7 (CE7) alloy.Footnote 1 Here, we describe the design and assembly and present laboratory characterization of the HF detector array.
2 Detector Design
The CLASS HF detectors are fabricated on 100-mm silicon wafers each consisting of 85 dichroic polarization-sensitive pixels as shown in Fig. 2. The beam is defined by a smooth-walled CE7 feedhorn, which couples light onto an OMT. The OMT separates two orthogonal states of linear polarization and couples them to microstrip transmission lines. The signals from opposite OMT probes are combined onto a single microstrip line using the difference output of a magic tee [5]. A diplexer then splits each signal path into two, followed by on-chip filters that define the frequency band. The signal continues on the microstrip line to the TES membrane through a stubby beam and is terminated at a PdAu resistor. The stubby beam precisely controls the thermal conductance of the TES island with ballistic-dominated phonon transport [6]. The long and meandered legs that support the TES bias leads have rough side walls and contribute very little to the thermal conductance. The Pd seen in the TES island in Fig. 2 is used to define the detector time constant through the electronic heat capacity of Pd.
Similar to the 90 GHz architecture described in [2,3,4], the HF wafer package consists of three separate wafers hybridized together: a photonic choke wafer, a detector wafer, and a backshort assembly. The photonic choke [7] acts as a waveguide interface between the feedhorn array and the detectors. The backshort assembly [8], among its many functions [4], forms a quarter-wavelength short for the OMT antenna probes. The middle detector wafer contains the detectors fabricated on single-crystal silicon that has excellent microwave and thermal properties [4]. The hybridized wafer package is mounted to the CE7 feedhorn array as a single assembly.
3 Module Design and Assembly
As shown in Fig. 1, the HF focal plane consists of three identical modules mounted on a mixing chamber plate maintained at a stable bath temperature of \(\sim \) 80 mK by a pulse-tube cooled dilution refrigerator.Footnote 2 Each module consists of 85 smooth-walled feedhorns made from a Au-plated CE7 alloy, which is machinable and has lower differential contraction to silicon detector wafers than copper or aluminum [9]. Figure 3 shows the tripod clips, alignment pins, and the side spring used to mount and align the detector wafer onto the feedhorn array. During assembly, four layers of flexible aluminum circuits are stacked on top of each wafer package and wire bonded to the detector bond pads on four sides of the wafer. The other end of the circuits is mounted onto four separate readout packages shown in Fig. 3.
Each readout package consists of eight time-division multiplexer (MUX) chips [10] and eight interface chips mounted on a printed circuit board (PCB), sandwiched between two Nb sheets for magnetic shielding. The interface chips have 200 \(\upmu \Omega \) shunt resistors and 310 nH Nyquist inductors. The inductance value was chosen to keep the readout noise aliased from higher frequencies below 1% of the noise level within the audio bandwidth of the TES. We also performed tests with and without this inductor to ensure that its addition does not affect the detector stability. Four MUX chips on each side of a readout package are combined into one readout column for multiplexing 44 rows, i.e., a multiplexing factor, or number of detectors per readout channel, of 44:1. The 150 and 220 GHz detectors are mapped to separate readout packages, each with two columns, so that they can be biased separately, if needed.
Detector bias signals and MUX addressing, feedback, and output signals are routed via twisted pairs of NbTi superconducting cables (Fig. 3), soldered directly into the PCB. In particular, this cabling connects the MUX output to a set of SQUID series array (SSA) amplifiers. The 4K SSA and the warm electronics are identical to the CLASS 90 GHz components as described in [2]. Figure 3 shows the layout of a module during and after assembly. After all the components are assembled and wire bonded, the readout packages are folded up and bolted to the feedhorn array on one side and attached to a backplate on the other. The backplate is finally bolted to the mixing chamber plate with the help of a Web structure and posts as shown in Fig. 1.
4 Detector Characterization
4.1 Electro-thermal Parameters
We characterize electro-thermal properties of the detectors by capping off all the cold stages of the cryostat with metal plates so as to minimize optical loading. We measure the TES saturation power (\(P_{\mathrm{sat}}\)) at 80% TES normal resistance (\({{R}}_{{\text {N}}}\)) for multiple bath temperatures (\(T_{\mathrm{bath}}\)) from 70 to 250 mK through I–V curves. At each \(T_{\mathrm{bath}}\), we ramp up the voltage bias to drive all the detectors normal and then sweep the bias down through the superconducting transition while recording the current response of the detectors. We fit \(P_{\mathrm{sat}}\) versus \(T_{\mathrm{bath}}\) to the following power law:
where \(\kappa \) is a thermal conductance parameter, and n is a power law index governing the power flow between the TES island and the bath. For CLASS detectors, this power flow is dominated by ballistic phonons, so we fix \(n = 4\) [6]. Table 1 shows the mean and standard deviation of \(T_{{\text {c}}}\) and \(\kappa \) values obtained from the fit to Eq. 1 for three CLASS HF modules. The \(P_{\mathrm{sat}}\) value is calculated at \(T_{\mathrm{bath}}\) = 50 mK, and the yield is the fraction of detectors that fit Eq. 1 with median absolute deviation (MAD) < 1 pW. Detectors with MAD > 1 pW are not included in the mean and standard deviation calculations for Table 1 and are excluded from further analysis in this paper.
The differences in \(P_{\mathrm{sat}}\) values obtained with increasing versus decreasing bath temperatures were \(\lesssim \) 0.2 pW; therefore, measurement errors were ignored in the standard deviation values of Table 1. As shown in Table 1, the spreads of \(T_{{\text {c}}}\) (3–6%) and \(\kappa \) (4–10%) parameters across all three modules for both frequencies are small. This results from uniform and controlled fabrication processes and ballistic thermal transport to the bath in all the TESs. The spread in \(P_{\mathrm{sat}}\) (8–20%) is mostly explained by the spread in \(T_{{\text {c}}}\). The uniformity of the detector parameters across the array and the observed in-laboratory detector stability over a wide range of bias voltages will allow the array to be optimally biased during sky observations. At the time of writing, the warm readout Multichannel Electronics (MCE) [11] firmware supports multiplexing over a maximum of 41 rows. Through a firmware upgrade, we expect to get all 44 rows working, which will increase the 150 GHz array yield to \(\sim \) 86% and 220 GHz to \(\sim \) 61%. Most of the remaining detectors are not operational due to complications in the bonding geometry. In particular, the lower yield in 220 GHz versus 150 GHz is due to wire bonding difficulty when trying to bond to the upper layers of the Al flex circuit stack as shown in the inset of Fig. 3.
4.2 Bandpass
We use a polarizing Martin–Puplett Fourier-transform spectrometer (FTS) to measure the bandpasses of the HF detectors in laboratory. Refer to [13] for detailed description of the FTS used and [2] for the filters used in the laboratory-cryostat setup. Figure 4 shows the measured CLASS detector bandpasses compared to simulation and the atmospheric transmission model at the CLASS site in the Atacama Desert with precipitable water vapor (PWV) of 1 mm. The raw measured bandpass values have been corrected for the feedhorn’s frequency-dependent gain and the transmission through the cryostat filters used in the laboratory setup.
The measured CLASS bandpasses in Fig. 4 have been averaged over all working detectors in the band. The CLASS Q and W bandpasses are added for completeness and are described further in [1, 2], respectively. The bandpasses safely avoid strong atmospheric emission lines, as designed. We also do not see any evidence of high frequency out-of-band leakage. The simulated bandpasses for the two HF bands are 132–162 GHz and 202–238 GHz as defined by their half-power points, whereas the respective measured bands are 134–168 GHz and 203–241 GHz. So, compared to simulation, the measured bandpasses for 150 and 220 GHz detectors are wider by 4 and 2 GHz, respectively, and both bands are shifted by a few GHz toward higher frequencies. We are currently investigating the source of these apparent shifts in the bands, which may be due to FTS systematics. We also plan to make FTS measurements through the receiver optics in the field.
4.3 Noise and Sensitivity
We took noise spectra of the HF detectors “in the dark” (capping off all the cold stages of the cryostat with metal plates) and measured the detector dark noise-equivalent power (\({\text {NEP}}_{\mathrm{dark}}\)) as shown in Fig. 5. In the CLASS audio signal band centered at the variable-delay polarization modulator (VPM) [14], frequency is 10 Hz, and the mean and standard deviation of \({\text {NEP}}_{\mathrm{dark}}\) are 22 ± 4 \({\text {aW}}\,\sqrt{{\text {s}}}\) and 25 ± 4 \({\text {aW}}\,\sqrt{{\text {s}}}\) for 150 and 220 GHz detectors, respectively. TES phonon noise (\({\text {NEP}}_{\mathrm{G}}\)), detector Johnson noise, and SQUID readout noise contribute to the measured \({\text {NEP}}_{\mathrm{dark}}\). We measured the current noise of “dark SQUIDs” (SQUIDs that are not connected to detectors) to be \(\sim \) 35 pA \(\sqrt{{\text {s}}}\). Using an average detector responsivity of \(\sim \ 5 \times 10^6 \, {\text {V}}^{-1}\), the SQUID readout noise is 7 \({\text {aW}}\,\sqrt{{\text {s}}}\). The detector Johnson noise is highly suppressed through electro-thermal feedback at lower frequencies, and we estimate it to be ~ 1.5 \({\text {aW}}\,\sqrt{{\text {s}}}\). The expected \({\text {NEP}}_{\mathrm{G}}\) values calculated from the detector parameters are shown in Table 1. \({\text {NEP}}_{\mathrm{G}}\) is the dominant noise source for \({\text {NEP}}_{\mathrm{dark}}\) as the readout and the Johnson noise contribute only a few percent when added in quadrature.
As shown in Fig. 5, the estimated photon NEPs in the field for the 150 and 220 GHz detectors are 44.4 and 62.3 \({\text {aW}}\,\sqrt{{\text {s}}}\), respectively [15]. Given the measured \({\text {NEP}}_{\mathrm{dark}}\) values, all the working detectors on the HF array are photon-noise limited. With the current array yield, the total array NEP is 2.5 \({\text {aW}}\,\sqrt{{\text {s}}}\) for 150 GHz and 4 \({\text {aW}}\,\sqrt{{\text {s}}}\) for 220 GHz. Assuming nominal bandpass and 50% total optical efficiency, we estimate array NETs of 17 and 51 \(\upmu {\text {K}}\ \root \of {{\text {s}}}\) for 150 and 220 GHz, respectively. Since the HF VPM is optimized for 150 GHz, we estimate the modulation efficiency to measure the Stokes parameter Q to be 70% for 150 GHz and 50% for 220 GHz. This leads to array noise-equivalent Q (NEQ) of 24 \(\upmu {\text {K}}\,\sqrt{{\text {s}}}\) for 150 GHz and 101 \(\upmu {\text {K}}\, \sqrt{{\text {s}}}\) for 220 GHz.
5 Conclusion
The CLASS HF detector array has been delivered to the telescope site and installed inside the cryostat receiver. This dichroic array sensitive to 150 and 220 GHz will provide additional sensitivity to CLASS’s CMB observations and help characterize the dust foreground. The detectors within each HF module show uniform parameter distributions. FTS measurements performed in laboratory show that the detector bandpasses safely avoid strong atmospheric emission lines with no evidence for high frequency out-of-band leakage. The HF detectors are photon-noise limited with average \({\text {NEP}}_{\mathrm{dark}}\) of 22 \({\text {aW}}\,\sqrt{{\text {s}}}\) for 150 GHz and 25 \({\text {aW}}\,\sqrt{{\text {s}}}\) for 220 GHz. With current array yield and expectations for optical and VPM modulation efficiencies, we estimate the CLASS HF array NEQ of 24 \(\upmu {\text {K}}\,\sqrt{{\text {s}}}\) for 150 GHz and 101 \(\upmu {\text {K}}\,\sqrt{{\text {s}}}\) for 220 GHz.
Notes
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Acknowledgements
We acknowledge the National Science Foundation Division of Astronomical Sciences for their support of CLASS under Grant Nos. 0959349, 1429236, 1636634, and 1654494. CLASS uses detector technology developed under several previous and ongoing NASA grants. Detector development work at JHU was funded by NASA Grant No. NNX14AB76A. We further acknowledge the very generous support of Jim and Heather Murren (JHU A&S ’88), Matthew Polk (JHU A&S Physics BS ’71), David Nicholson, and Michael Bloomberg (JHU Engineering ’64). CLASS is located in the Parque Astronómico de Atacama in northern Chile under the auspices of the Comisión Nacional de Investigación Científica y Tecnológica de Chile (CONICYT).
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Dahal, S., Amiri, M., Appel, J.W. et al. The CLASS 150/220 GHz Polarimeter Array: Design, Assembly, and Characterization. J Low Temp Phys 199, 289–297 (2020). https://doi.org/10.1007/s10909-019-02317-0
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DOI: https://doi.org/10.1007/s10909-019-02317-0