A&A 520, A9 (2010)with warm preamplifier and read-out Electronics delivering thedigital signal through the DPU to the electrical ground supportequipment (EGSE). It also provided an opportunity to test thedilution cooler in conditions similar to those of the PFM. In addition,it was the first complete test for the calibration facilityand offered excellent preparation for the calibration of the PFM.Once the HFI was integrated in the spacecraft, the most importanttest of the qualification, acceptance and verification processwas the cryogenic test performed in the Focal V vacuumchamber of the Centre Spatial de Liège in Belgium. The CQMdemonstrated the capability of HFI to reach the objectives of themission, i.e. meeting the major required characteristics, like thephotometric sensitivity and the lifetime of the dilution cooler.The test of the complete cryogenic chain was successfully completedat the PFM. The dilution cooler, 4 K cooler, 18 K sorptioncooler and the passive radiators were all mounted in the flightconfiguration. A large number of procedures for the flight weresuccessfully tested in preparation to the cool down, commissioningand flight operations.6.2. HFI calibration philosophyThe cryo-qualification model (CQM) and the proto-flight model(PFM) of the HFI were extensively tested and calibrated on theground (Pajot et al. 2010). In parallel, numerical models of theinstrument and of its response (Catalano 2008)weredeveloppedto interpret the test data and to check that the obtained resultswere consistent with those expected, thereby validating the operationof the instrument. At the same time, deviations from themodels alerted us to unanticipated behaviour, like the low frequencyexcess response of the bolometers. Finally, the instrumentmodels can be used to interpolate ground calibration resultsinto the phase space of operating parameters that were notexplored finely enough during tests. The final calibration willrely on data obtained in-flight, as far as possible. Some groundcalibration data, like the spectral transmissions, will remain thereference (Pajot et al. 2010).6.3. ScheduleThe development and testing of HFI was complex, and so thetwo models were delivered in groups of functional units on timeto be integrated on the S/C. The main dates in the history of HFIwere– CQM delivery of the units in 2004;– integration on the CQM S/Cfromendof2004tomid2005;– cryotest at CSL June to September 2005;– PFM delivery of units from mid 2006 to mid 2007;– integration of both LFI and HFI FPUs at the end of 2006;– integration with the S/C and environment tests up toMarch 2008;– cryogenic test at CSL from June to September 2008.The S/C wasthenfinallytestedandpreparedforthetransportationto Kourou for the launch. The last ground operations on HFIwere mixed with regular health verifications, the cleaning of the4Kcoolerduring120h,thepurgeofthepipesofthedilutioncooler and the filling of the 3 He and 4 He tanks.6.4. ManagementFollowing the selection of the <strong>Planck</strong> mission, the LFI andHFI instruments, each led by a principal investigator (PI), wereselected for flight. Each PI had full responsibility for the deliveryof their respective instrument. HFI was built by a consortiumof institutes from France, Italy, Spain, the UK and theUSA. A work-breakdown structure defined the work to be doneup to the completion of the instrument. In each institute a coinvestigator(Co-I) and an element manager were responsible forthe delivery of their specific equipment. The industry often participatedas a subcontractor. Funding was provided by nationalagencies, and the relationship between the PI and the Co-Is isdefined in a Memorandum of Understanding, which is the referencedocument in the work and responsibilities on the project.The HFI project is organized around the PI with key personslike the Co-PI, who supervises the data processing, the instrumentscientist responsible for the instrument, and the scientistin charge of calibrations and operations. The technical team isorganized around the project manager with a project controller,asystemengineer,amanagerresponsibleforintegrationverificationand test (AIV-AIT), a product assurance manager, and ateam of architects responsible for the various engineering taskslike cryogenics and thermics, mechanics, optics, EMI-EMC. Thetechnical team also includes engineers and scientists responsiblefor the delivery of identified sub-systems: the dilution cooler, the4Kcooler,readoutelectronics,andtheDPU.Theintegrationand system tests were managed by the AIV-AIT manager with ateam of specialists. They also operate during the AIT phase onthe S/CandinKourou.7. ConclusionsThe ambition of the HFI instrument is to provide a new pictureof the CMB with much improved sensitivity, high angular resolutionand a low level of systematic effects. It will map the sky inthe sub-THz range with sensitivity limits near to the fundamentalfluctuations of the observed radiation itself. The calibrationand tests on the ground indicate that this goal should indeed beachieved in flight, with a sensitivity to within a factor of two ofthe photon noise in all channels (i.e. in line with the goal sensitivityannounced in the instrument proposal) and about two timesbetter than required by the scientific goals. This performancewas achieved by experts in all of the relevant instrumental fieldsworking together and agreeing on goals that were close to thelimit of what could be achieved in the time-frame of this project.The preliminary concepts definingthearchitectureandthespecificationof sub-systems provided a robust design that could beadapted to cope with some variability of individual components.Some progress in component design can be expected for futureCMB experiments. However, the experience of the HFI suggeststhat significantly higher sensitivities can only be achieved by usingmuch larger numbers of detectors.Careful attention was paid to reduce systematic effects to levelscommensurate with the high sensitivity of the HFI. This requiredsubstantial efforts in the optical and electrical designs.The instrument was carefully calibrated during tests on theground, though there remain a few uncertainties as described inthis paper. Some systematic effects could be identified and measuredduring tests of the HFI, providing the HFI data processingcentre with a wealth of information for future data reduction.Together with the Low Frequency Instrument, the HFI shouldbe able to produce a new picture of the CMB and of the submillimetresky.Acknowledgements. The <strong>Planck</strong>-HFI instrument (http://hfi.planck.fr/)was designed and built by an international consortium of laboratories, universitiesand institutes, with important contributions from the industry, under thePage 18 of 20
J.-M. Lamarre et al.: <strong>Planck</strong> pre-launch status: the HFI instrumentleadership of the PI institute, IAS at Orsay, France. It was funded in particularby CNES, CNRS, NASA, STFC and ASI. The authors extend their gratitudeto the numerous engineers and scientists, who have contributed to the design,development, construction or evaluation of the HFI instrument. The authors arepleased to thank the referee for his/her very useful remarks.ReferencesAde, P. A. R., Savini, G., Sudiwala, R., et al. 2010, A&A, 520, A11Baranov, V. K., & Mel’nikov, G. K. 1966,Sov.J.Opt.Technol.,33,408Benoît, A., Sirbi, A., Bradshaw, T., et al. 1997, in Sixth European Symposiumon Space Environmental Control Systems, ed. T.-D. Guyenne, ESA SP, 400,497Benoît, A., Zagury, F., Coron, N., et al. 2000, A&AS, 141, 523Benoît, A., Ade, P. A. R., Amblard, A., et al. 2002, Astroph. Phys., 17, 101Bersanelli, M., Mandolesi, N., Butler, R. C., et al. 2010, A&A, 520, A4Bock, J. J., Chen, D., Mauskopf, P. 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A., Mandolesi, N., Puget, J.-L., et al. 2010a, A&A, 520, A1Tauber, J. A., Norgaard-Nielsen, H.,Ade,P.A.R.,etal.2010b,A&A,520,A2The <strong>Planck</strong> consortium 2005, PLANCK – The Scientific Programme (The<strong>Planck</strong> Bluebook), ESA-SCI(2005)1Triqueneaux, S., Sentis, L., Camus, P., Benoît, A., & Guyot, G. 2006,Cryogenics, 46, 288Tristram, M. 2005, Ph.D. Thesis, Université Joseph Fourier, Grenoble 1Vaillancourt, J. E. 2005, Rev. Sci. Instrum., 76, 043107Welford, W. T., & Winston, R. 1978, The optics of nonimaging concentrators,Light and solar energy (Academic <strong>Pre</strong>ss)Woodcraft, A. L., Sudiwala, R. V., Ade, P. A. R., et al. 2003, Appl. Opt., 42,5009Yvon, D., Panh, J., Landé, J., et al. 2008, J. Low Temperature Phys., 151, 4481 Laboratoire d’Étude du Rayonnement et de la Matière enAstrophysique (LERMA), Observatoire de <strong>Paris</strong>, ENS, UPMC,UCP, CNRS, 61 avenue de l’Observatoire, 75014 <strong>Paris</strong>, Francee-mail: jean-michel.lamarre@obspm.fr2 IAS, Institut d’Astrophysique Spatiale, CNRS & Université <strong>Paris</strong>11, Bâtiment 121, 91405 Orsay, France3 Cardiff University, School of Physics and Astronomy, The Parade,Cardiff CF24 3AA, UK4 Institut d’Astrophysique de <strong>Paris</strong>, UMR 7095, CNRS and UniversitéPierre & Marie Curie-<strong>Paris</strong> 6, 98 bis boulevard Arago, 75014 <strong>Paris</strong>,France5 Department of Physics, California Institute of Technology, Mailcode: 59-33, Pasadena, CA 91125, USA6 Jet Propulsion Laboratory, California Institute of Technology, 4800Oak Grove Drive, Pasadena, CA 91109, USA7 European Space Agency – ESTEC, Astrophysics Division,Keplerlaan 1, 2201 AZ Noordwijk, The Netherlands8 LAL, Laboratoire de l’Accélerateur Linéaire, CNRS & Université<strong>Paris</strong> 11, Bâtiment 200, 91898 Orsay Cedex, France9 Institut Néel, CNRS, Univ. Joseph Fourier Grenoble I, 25 rue desMartyrs, BP 166, 38042 Grenoble Cedex 9, France10 CESR, Centre d’Étude Spatiale des Rayonnements, CNRS, 9 Av. ducolonel Roche, BP44346, 31038 Toulouse Cedex 4, France11 CNES, 18 avenue Edouard Belin, 31401 Toulouse Cedex 9,France12 Laboratoire Astroparticule et Cosmologie (<strong>APC</strong>), CNRS &Université <strong>Paris</strong> <strong>Diderot</strong> – <strong>Paris</strong> 7, 10 rue A. Domon et L. Duquet,75205 <strong>Paris</strong> Cedex 13, France13 STFC, Rutherford Appleton Laboratory, Harwell Science andInnovation Campus, Didcot, OX11 0QX, UK14 Kavli Institute for Particle Astrophysics and Cosmology andDepartment of Physics, Stanford University, 382 via Pueblo Mall,Stanford, CA 94305, USA15 Dipartimento di Fisica, Universitá La Sapienza, Piazzale Aldo Moro2, 00185 Roma, Italy16 Laboratoire d’Astrophysique Observatoire de Grenoble (LAOG),CNRS, BP 53, 38041 Grenoble Cedex 9, France17 European Space Agency – ESAC, PO box 78, 28691 Villanueva dela Cañada, Madrid, Spain18 Institute of Astronomy, University of Cambridge, Madingley Road,Cambridge CB3 OHA, UK19 Princeton University, Department of Physics, Joseph HenryLaboratory, USAPage 19 of 20
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ABSTRACTThe European Space Agency
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A&A 520, A1 (2010)Table 4. Summary
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A&A 520, A1 (2010)57 Instituto de A
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3.3.1. SpecificationsThe main requi
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M. Sandri et al.: Planck pre-launch
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