Planck Pre-Launch Status Papers - APC - Université Paris Diderot ...

Planck Pre-Launch Status Papers - APC - Université Paris Diderot ... Planck Pre-Launch Status Papers - APC - Université Paris Diderot ...

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A&A 520, A6 (2010)Table 1. Calibration test list.TEST IDRCA_AMBRCA_CRYRCA_TUNRCA_OFTRCA_TNGRCA_LISRCA_STnRCA_UNCRCA_SPRRCA_THFRCA_THBRCA_THVDESCRIPTIONFUNCTIONALITYFunctional test at ambientFunctional test at cryoTUNINGGain and offset tuning of the DAETuning of the front end module(phase switches and gate voltages)BASIC PROPERTIESRadiometer offsetmeasurementNoise temperature andphotometric gainRadiometer linearityNOISE PROPERTIESNoise performances tests:WN, f k and α, β, rVerification of the effectof the radiometer switchingon the noise spectrumBAND PASS RESPONSEBandpassSUSCEPTIBILITYSusceptibility toFEM temperature variationsSusceptibility toBEM Temperature variationsSusceptibility to V-groovetemperature variationsNotes. The first column reports the test identification. In the secondcolumn the purpose of each test is described; WN is the white noiselevel; f k , α are the 1/ f knee frequency and slope respectively; β is theequivalent radiometer bandwidth derived from noise; r is the modulationfactor. Apart from the first test RCA_AMB, whichisperformedatambient temperature, all the other tests are performed at the operationaltemperature (i.e. at a temperature as close as possible to in-orbit conditions).CHain EvaLuator) software for quick-look analysis and datastorage (Malaspina et al. 2009). The data files were stored inFITS format. As two chains were calibrated at the same time at70 GHz, separate EGSEs and analysis workstations were usedfor each RCA. Below the cryofacilities and skyloads are summarizedwith the emphasis on the issues related to the analysisof the calibration data.3.1. The cryofacility for the 30 and 44 GHz RCAsThe chamber with its overall dimensions of 2.0×1.2×1.0m 3 wasable to accept one RCA at a time. The chamber was designed toallow the pressure to reach less than 10 −5 mBar, and containedseven thermal interfaces to reproduce the flight-like thermal conditionsof an RCA. During tests it was possible to control and stabilizethe BEM temperature, the waveguide-to-spacecraft interfacetemperature, and the FEM temperature. In addition the tworeference targets (the referenceloadandtheskyload)werecontrolledin temperatures in the range 4−35 K to allow temperaturestepping for radiometer linearity tests (RCA_LIS). In addition tothe electrical connections for the DAE breadboard and to controlthe thermal interfaces, two thermal-vacuum feedthroughs (onefor the 30 GHz and the other one for the 44 GHz RCAs) withKapton windows were provided to allow access for the RF signalfor the bandpass tests (RCA_SPR).Fig. 2. Radiometer chain assembly integrated into the 30 and 44 GHzcryofacility for calibration. In the picture at the top the skyload facingthe horn is visible together with the FEM insulated from the 50 Kshroud (the copper box). In the bottom picture the BEM and its thermalinterface are shown. See the text for details of the cryochamber.During the RCA27 and RCA28 calibrations an uncertainty inthe reference targets’ temperature was experienced. A visual inspectionof the cryochamber after the RCA28 test gave a possibleexplanation and in the RCA27 test, an additional sensor wasput on the back of one of the reference targets in order to verifythe probable source of the problem. The observed behaviorwas consistent with an excess heat flow through the 4 K referenceload (4KRL), via its insulated support caused by a contactcreated during cooldown. A dedicated thermal model was thusdeveloped to derive the Eccosorb 4KRL temperature, T ref fromthe back plate controller sensor temperature, T ctrlref(Terenzi et al.2009b). A quadratic fit was found with T ref = a + b · T ctrlref+ c ·( )Tctrl 2ref for each pair of detectors coupled to the same radiometerarm and for each 30 GHz RCA. The coefficients derived fromthe fit are shown in Table 2.3.2. Sky load at 30 and 44 GHzThe calibrator consisted of a cylindrical cavity with walls coveredin Eccosorb CR110 6 (see Fig. 6). The back face of the6 Emerson & Cuming, http:www.eccosorb.comPage 4 of 14

F. Villa et al.: Calibration of LFI flight model radiometersTable 2. Reference load target temperature.RCA27MSa 5.7 ± 0.2 2.5 ± 0.1b 0.58 ± 0.02 0.81 ± 0.01c 0.00686 ± 5.8 × 10 −4 0.00322 ± 3.2 × 10 −4RCA28MSa 2.47 ± 0.05 5.50 ± 0.09b 0.799 ± 0.007 0.57 ± 0.01c 0.00407 ± 2.5 × 10 −4 0.00831 ± 4.1 × 10 −4Table 3. Temperarture of the sky load pyramids. Quadratic fit coefficients.30 GHz 44 GHza 0.9185 ± 0.0006 0.5430 ± 0.008b 0.9540 ± 0.0001 0.9795 ± 0.0008c 0.0008460 ± 4.4 × 10 −6 0.000217 ± 1.9 × 10 −5Notes. Quadratic fit coefficients.Fig. 4. T sky as a function of back plate controller skyload temperatureT ctrlsky. The left plot refers to the 30 GHz RCAs, based on RCA28 data(circles). The right plot refers to the 44 GHz RCAs, based on RCA25and RCA26 data (squares). The lines are the quadratic fit to the data.Fig. 3. Thirty minutes of data acquired during RCA28. Noisetemperatureand linearity tests are shown with T ctrlsky in red, T sky in green, andin blue. This represents the worst case of these differences. Thestability of the temperatures with the values T ctrlsky= 8.50000 ± 0.00006,T sky = 9.0981 ± 0.0004, and T side = 9.9560 ± 0.0007 are also evident.skyT sideskycavity was covered with Eccosorb pyramids to guarantee a returnloss of about −30dB. Details of the skyload are reportedin Cuttaia (2005). Four temperature sensors were placed on thesky load, but only two cernox sensors were taken as referencefor calibration. The first one was placed on the back plate of thesky load to measure the temperature of the PID control loop ofthe sky load, T ctrlsky .ThesecondwasplacedontheEccosorbpyramidsinside the black body cavity and was assumed as the blackbodyreference temperature, T sky .Thecontributiontotheeffectiveemissivity due to the pyramids was estimated by Cuttaia(2005) tobe0.9956 for the 30 GHz channel and 0.9979 for the44 GHz channel. The effective emissivity was calculated assumingthe horn near field pattern and the emissivity of the material.In the case of the skyload side walls the effective emissivity is4.29 × 10 −3 and 2.07 × 10 −3 for the 30 GHz and 44 GHz respectively.In the data analysis only the contribution of the pyramidswas considered assuming its emissivity equal to 1. Assuming theemissivities reported above and the temperatures as in Fig. 3,the approximation leads to an uncertainty in the brightness temperatureof about 0.04 K and the same uncertainty in the noisetemperature measurements.Due to a failure in the sensor on the pyramids an analyticalevaluation of T sky temperature from T ctrlskytemperature wasperformed during the calibration of RCA24 and RCA27. Thedata are shown in Fig. 4. Althoughthedatashowalinearbehavior,the differences between T ctrlsky and T sky decrease as theFig. 5. Differences between T sky and T ctrlskyas a function of Tctrlsky showingthe non-linear behavior of the difference. Circles are for 30 GHz RCAsand squares for 44 GHz RCAs.temperature increases (see Fig. 5) asexpectedfromthethermalbehavior of the system, suggesting that a quadratic fit withT sky = a+b·T ctrl ctrl 2sky+c·(Tsky)is more representative. This quadraticfit was performed, and the coefficients are reported in Table 3.3.3. The cryofacility of the 70 GHz RCAsThis cryofacility has the dimensions 1.6 × 1.0 × 0.3 m 3 .Thefacility has a layout similar to that at 30–44 GHz, although the70 GHz facility was designed to house two radiometer chainssimultaneously (Fig. 7).Page 5 of 14

F. Villa et al.: Calibration of LFI flight model radiometersTable 2. Reference load target temperature.RCA27MSa 5.7 ± 0.2 2.5 ± 0.1b 0.58 ± 0.02 0.81 ± 0.01c 0.00686 ± 5.8 × 10 −4 0.00322 ± 3.2 × 10 −4RCA28MSa 2.47 ± 0.05 5.50 ± 0.09b 0.799 ± 0.007 0.57 ± 0.01c 0.00407 ± 2.5 × 10 −4 0.00831 ± 4.1 × 10 −4Table 3. Temperarture of the sky load pyramids. Quadratic fit coefficients.30 GHz 44 GHza 0.9185 ± 0.0006 0.5430 ± 0.008b 0.9540 ± 0.0001 0.9795 ± 0.0008c 0.0008460 ± 4.4 × 10 −6 0.000217 ± 1.9 × 10 −5Notes. Quadratic fit coefficients.Fig. 4. T sky as a function of back plate controller skyload temperatureT ctrlsky. The left plot refers to the 30 GHz RCAs, based on RCA28 data(circles). The right plot refers to the 44 GHz RCAs, based on RCA25and RCA26 data (squares). The lines are the quadratic fit to the data.Fig. 3. Thirty minutes of data acquired during RCA28. Noisetemperatureand linearity tests are shown with T ctrlsky in red, T sky in green, andin blue. This represents the worst case of these differences. Thestability of the temperatures with the values T ctrlsky= 8.50000 ± 0.00006,T sky = 9.0981 ± 0.0004, and T side = 9.9560 ± 0.0007 are also evident.skyT sideskycavity was covered with Eccosorb pyramids to guarantee a returnloss of about −30dB. Details of the skyload are reportedin Cuttaia (2005). Four temperature sensors were placed on thesky load, but only two cernox sensors were taken as referencefor calibration. The first one was placed on the back plate of thesky load to measure the temperature of the PID control loop ofthe sky load, T ctrlsky .ThesecondwasplacedontheEccosorbpyramidsinside the black body cavity and was assumed as the blackbodyreference temperature, T sky .Thecontributiontotheeffectiveemissivity due to the pyramids was estimated by Cuttaia(2005) tobe0.9956 for the 30 GHz channel and 0.9979 for the44 GHz channel. The effective emissivity was calculated assumingthe horn near field pattern and the emissivity of the material.In the case of the skyload side walls the effective emissivity is4.29 × 10 −3 and 2.07 × 10 −3 for the 30 GHz and 44 GHz respectively.In the data analysis only the contribution of the pyramidswas considered assuming its emissivity equal to 1. Assuming theemissivities reported above and the temperatures as in Fig. 3,the approximation leads to an uncertainty in the brightness temperatureof about 0.04 K and the same uncertainty in the noisetemperature measurements.Due to a failure in the sensor on the pyramids an analyticalevaluation of T sky temperature from T ctrlskytemperature wasperformed during the calibration of RCA24 and RCA27. Thedata are shown in Fig. 4. Althoughthedatashowalinearbehavior,the differences between T ctrlsky and T sky decrease as theFig. 5. Differences between T sky and T ctrlskyas a function of Tctrlsky showingthe non-linear behavior of the difference. Circles are for 30 GHz RCAsand squares for 44 GHz RCAs.temperature increases (see Fig. 5) asexpectedfromthethermalbehavior of the system, suggesting that a quadratic fit withT sky = a+b·T ctrl ctrl 2sky+c·(Tsky)is more representative. This quadraticfit was performed, and the coefficients are reported in Table 3.3.3. The cryofacility of the 70 GHz RCAsThis cryofacility has the dimensions 1.6 × 1.0 × 0.3 m 3 .Thefacility has a layout similar to that at 30–44 GHz, although the70 GHz facility was designed to house two radiometer chainssimultaneously (Fig. 7).Page 5 of 14

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