A&A 520, A7 (2010)the main beam, which degrade the angular resolution and increasethe uncertainty in the measurements at high multipoles(particularly for polarization) as the texture of the cosmic signalis smeared and distorted; (ii) the sidelobes in the feed/telescoperadiation pattern, which contribute to the straylight inducednoise, i.e., the unwanted power reaching the detectors and notcoupled through the main beam. These introduce contaminationmainly at large and intermediate angular scales, typically at multipolesless than ≃100.In this paper, we present the definition, optimization, andcharacterization of the LFI optical interfaces. The work involvedhere has been carried out by means of electromagnetic simulationsdevoted to maximizing the angular resolution and at thesame time minimizing systematic effects. The starting point ofthe optimization activity was the <strong>Planck</strong> telescope, which is anoff-axis Gregorian telescope satisfying the Mizuguchi-Dragonecondition. Initially, the LFI focal surface configuration included(in addition to the frequency channels at 30, 44 and, 70 GHz),also a channel at 100 GHz comprising seventeen horns distributedaround the HFI front-end. The LFI 100 GHz channelwas subsequently removed, but it was part of the initial studyand much of the analysis was completed for this channel and appliedto the lower frequencies. The position and orientation ofeach horn was determined by taking into account the mechanicalconstraints imposed by the LFI interfaces and 4 K referenceloads attached to the HFI instrument (see Mandolesi et al. 2010)and assuming a Gaussian model. We emphasize that the simulationsdiscussed in this paper were carried out by assuming aradio frequency model composed of the ideal telescope, the baffle,and the coldest V-groove thermal radiator (see Sandri et al2002b). The current most suitable model of the detailed beamsfor both LFI and HFI, taking into account a realistic model ofthe telescope, are given in Tauber et al. (2010).The assumed <strong>Planck</strong> telescope design and the focal surfacelayout are described in Sects. 2 and 3, respectively. In Sect. 4,edge-taper degradation of the horns is presented. The edge-taperwas degraded to improve the angular resolution while maintainingstraylight rejection to within the requirements. Section 5presents the feedhorn alignment process, complete so that CMBpolarization measurements can be made. In Sect. 6, given theedge-taper values and the location andorientationofthefeedsdetemined in the previous sections, each horn design was thenoptimized in terms of sidelobe level, cross polarization response,and beamwidth. This optimization was first carried outat 100 GHz, i.e., the most critical channel for LFI, and the resultswere extrapolated to lower frequencies, taking care to check theconsistency at the end of the activity. Finally, the fully optimizedperformance of the LFI beams is reported in Sect. 7.2. Telescope optical designThe <strong>Planck</strong> telescope was designed to comply with the followinghigh level opto-mechanical requirements: wide frequency coverage(about two decades), 100 squared degrees of field of view,wide focal region (400 × 600 mm), and a cryogenic operationalenvironment (40−65 K). These unique characteristics for an experimentalcosmology telescope have never been previously implemented.The <strong>Planck</strong> telescope represents a challenge for telescopetechnology and optical design (Villa et al. 2002; Tauberet al. 2010).The telescope optical layout is based on a dual reflectoroff-axis Gregorian design. This configuration allows it tohave a small overall focal ratio (and thus small feeds), an unobstructedfield of view, and low diffraction effects from theFig. 1. Lateral and top view of the telescope unit consisting of the reflectorsand the support structure; the hexagonal support structure is readilyseen as well as the field of view (in gray) (left panel). The telescope unitallocated into <strong>Planck</strong> satellite (right panel). The vertical axis is the spinaxis of the satellite and the line of sight is tilted by 85 ◦ with respect tothe spin axis. The baffle aroundthetelescopeisnotshown.secondary reflector and struts. It allows, at the same time, thesecondary reflector to be appropriately oversized. To improvethe image quality, the design has been optimized by changing theconic constants, the radius of curvature, the distance between themirrors, and the tilting of both mirrors, using the spillover leveland the wave front error as optimization parameters (Dubruelet al. 2000). The primary mirror is elliptical in shape (but nearlyparabolic since the conic constant is about −0.9) as in aplanaticconfigurations (Wilson 1996), and the size of the rim is1.9 × 1.5m.Theoffset of the primary reflector, i.e., the distancebetween its center and its major axis, is 1.04 m, while the secondaryreflector offset is 0.3 m.Thesecondarymirrorisellipticalwith a nearly circular rim about 1 m in diameter. The overallfocal ratio, F # ,equals1.1,andtheprojectedapertureiscircularwith a diameter of 1.5 m.Thetelescopefieldofviewis±5 ◦centered on the line of sight (LOS), which is tilted at about 3.7 ◦relative to the main reflector axis, and forms an angle of 85 ◦ withthe satellite spin axis, which is typically oriented in the anti-Sundirection during the survey (Dupac 2008). The <strong>Planck</strong> telescopeas a complete satellite subsystem is shown in Fig. 1 and a detaileddescription is reported in Tauber et al. (2010).3. LFI optical interfacesIn its flight configuration, LFI is coupled to the telescopeby eleven dual-profiled, corrugated, conical horns (Villa et al.2010): six feed horns at 70 GHz (FH18 – FH23), three feed hornsat 44 GHz (FH24 – FH26), and two feed horns at 30 GHz (FH27and FH28). Figure 2 shows the arrangement of the horns insidethe LFI main frame. It should be noted that the feed position inthe focal surface is axisymmetric (for instance, FH27 is symmetricto FH28 at 30 GHz), a natural design choice based on thesymmetry of the telescope and satellite. As a consequence, onlysix different feed elements have been considered in the optimisationanalysis: one feed at 30 GHz, two at 44 GHz, and threeat 70 GHz (Villa et al. 2010). The center of the focal surfaceis occupied by the HFI horns. This optical layout, with one instrument(LFI) around the other (HFI), required that aberrationeffects in the LFI beams be accurately controlled in the telescopeand instrument design optimization phases. Corrugatedhorns were selected as the most suitable solution in terms ofcross polarization levels, sidelobes levels, return and insertionPage 2 of 12
M. Sandri et al.: <strong>Planck</strong> pre-launch status: Low Frequency Instrument opticscoordinate system, placed in the centeroftheFPUandwiththeZ RDP axis aligned along the chief ray of the telescope.The focal plane configuration is a result of a long iterationprocess. Apart from the horn aperture definition, which is theresult of edge-taper optimization (see Sect. 4), the location, theorientation, and the length of the feed horns were determined onthe basis of the mechanical interfaces, feed mutual obscuration,and pointing direction as derived form the telescope characteristics.The horn pointing was obtained from the optical study ofthe telescope and the tilting angles were derived by means of raytracing simulations. This study was addressed at the end of thetelescope optimization process when the focal plane design wasnot frozen. However, this was sufficient to derive analytical formulaefor pointing that have been used in additional focal planeoptimizations, ending with the final design. We consider the referencedetector plane coordinate system (X RDP , Y RDP , Z RDP ) asastartingpointtodefinehornpointing.Thehornpointingdependsonly on the (X RDP , Y RDP ) coordinates, while Z RDP definesthe phase centre location only. We also define the two rotationangles as α the rotation angle around Y RDP ,andβ the rotationaround X RDP axis. For the <strong>Planck</strong> telescope, and in the regionwhere the LFI feeds are located (i.e., outside the centre of thefocal plane), the two angles were derived from a linear fit to theoptical simulation results:α = a x · X RDP + b x , (1)β = b x · Y RDP + b y . (2)Fig. 2. ACADmodelofthe<strong>Planck</strong> focal plane, which is located directlybelow the telescope primary mirror. It comprises the HFI bolometricdetector array (small feed horns on golden circular base) andthe LFI radio receiver array (larger feed horns around the HFI). Thebox holding the feedhorns appears to be transparent in this view, toalso show the elements inside and behind it (top panel). The HFI andLFI feed horns are seen reflected in the primary mirror of the <strong>Planck</strong>telescope in the clean room at Kourou, French Guiana (bottom panel).c○ ESA/Thales.loss. Dual-profiled corrugation shaping was chosen for the controlof the main lobe shape, the phase centre location, and compactness(Clarricoats 1984; Olver&Xiang1988). The corrugationprofile of each horn was designed to achieve a trade-offbetween angular resolution and straylight rejection. Each feedhorn is connected to an orthomode transducer (OMT) to dividethe field propagating into the horn into two orthogonal linear polarizationcomponents, X and Y (D’Arcangelo et al. 2010).The feeds and corresponding OMTs are adjusted in the focalsurface so that the main beam polarization directions of the twosymmetrically located feed horns in the focal plane unit (FPU)are at an angle of 45 degrees when observed in the same directionin the sky. This configuration permits measurement of theQandUStokesparametersandthusthelinearpolarizationofthe CMB. The location and orientation of each horn is reportedin Table 1, withrespecttothereferencedetectorplane(RDP)The lengths of the horns were chosen to satisfy the followingconstraints: (i) to guarantee the interface specifications of the4Kreferenceload(whichareattachedtotheHFIinstrument,and are thus a driver on the LFI focal plane interface design);(ii) to guarantee matching with both the focal surface and theobscuration criterion of the LFI horns. These criteria fixed theclearance as a cone of 45 ◦ from the horn aperture rim. It wasset after measurements performed by the LFI team (Ocleto et al2009) and simulations performed by the industrial contractor 2 .In this way, it was possible to optimize the focal plane with theLFI CAD solid model without performing time consuming electromagneticcomputations. Once the horn location and orientationwere frozen, the phase centre position and the edge-taperwere used as inputs to the corrugation design.4. Edge-taper evaluationThe angular resolution (expressed here in terms of full width halfmaximum, FWHM) ofthebeamintheskydependsontheillumination,g(x,y), of the primary mirror. For an aperture-type antenna(such as a reflecting telescope), the far field is the Fouriertransform of the aperture illumination function. If a Gaussian illuminationis assumed, the main beam shape is Gaussian too.The flatter the illumination, the narrower the resulting pattern;in contrast, if the illumination is more centrally peaked, then theangular resolution of the pattern is degraded. For a dual reflectortelescope, the illumination function g(x,y)isproducedbythe feed-horn pattern, reflected and diffracted by the subreflector,and distorted by aberrations mainly due to the off-axis positionof the feeds. This is the case for the LFI focal plane configuration.The trade-off between the angular resolution (which impactsthe instrument’s ability to reconstruct the anisotropy powerspectrum of the cosmic microwave background radiation at highmultipoles) and the edge-taper (which controls the systematic2 Thales Alenia Space – France, formerly Alcatel Space.Page 3 of 12
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ABSTRACTThe European Space Agency
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