The Fresnel Diffractive Imager project --Principles, Instrumentation and Mission scenarios Université de Toulouse, CNRS France Laurent Koechlin, Denis Serre, Paul Deba, Truswin Raksasataya, Christelle Peillon, Emmanuel Hinglais, Paul Duchon, Pierre Etcheto, Christian Dupuy, Benoît Meyssignac, Laurent Doumic. The Fresnel Diffractive Imager project I. Optical Principles Focalization by diffraction Chromatic correction High dynamic range II. Lab prototype, optical and numerical tests Optical setup Tests results on artificial sources Tests planned on sky sources Numerical simulations for large arrays III. Space mission scenarios Orbits and Formation flying configuration Primary array vessel design Focal instrumentation design IV. Astrophysical targets Some of the possible scenarios I. Optical Principles Focalization : different ways Lens focus Plane wavefront Lens (or miror): focusing by refraction (or reflexion) Fresnel array: focusing by diffraction … Order 1 : convergent Order 0 : plane wave focus 2D radial expansion Concentric geometry (Soret 1875) Efficiency at order 1: 10% Exemple for 15 Fresnel zones 2D Cartesian expansion Orthogonal geometry (2005) Efficiency at order 1: 4 to 8 % Exemple for 30 Fresnel zones g(x)= 1 si (x2 +f2)1/2 [(f/ml + (k-off) +1/2) ml ; (f/ml + (k-off) +1) ml[ Fresnel Zone plate or Aperture synthesis array ? (here: 1740 ouvertures) sinon g(x) = 0 Transmission (x, y) = g (x) xor g (y) Image formation circular geometry => isotropic PSF Image Aperture non linear luminosity scale In order to show the faint isotropic rings. Image formation Orthogonal geometry => orthogonal PSF Image Aperture Quasi no stray light except in the spikes. Transmission: g(x) g(y) non linear luminosity scale In order to show the faint spikes. Image formation Case of a second source in the field: Image formation Case of a second source in the field: Image formation Case of a second source in the field: Comparison: Fresnel arrays versus a solid aperture Images of a point source by: 150 Fresnel zones luminosity scale: Power 1/4 to show spikes 1500 Fresnel zones Solid square aperture "for" Fresnel Arrays: No mirror, no lens to focalize : just vacuum and opaque material. => a potentially very broad operational domain: 90nm - 25 mm Angular resolution: as high as with a mirror the size of the whole array. High dynamic range: 108 on compact objects for a 300 zones array Large tolerance in positioning of subapertures for l/20 wavefront quality: 100 mm in the plane of the array 10 cm in the wave propagation direction (perp. to array) The tolerance is wavelength independent => Opens a way to build very large aberration-free apertures for astrophysics. "against" Fresnel Arrays: C F = C2/8N l Chromaticity... corrected by small diffractive lens after focus, (order 1 chromaticity cancelled by order -1 chromaticity), but bandpass limitations remain: Dl/l = √2 S/C kilometric focal lengths => requires formation flying in space Low transmission compared to a mirror : t = 5 to 10% Optical scheme of the Fresnel Diffractive Imager Primary Fresnel array e.g. 20 m Diffractive lens at order -1 e.g. 10 cm Field Optics 10 to 100 km e.g. 2m Converging lens e.g. 10 cm mask Order 0 rays Focal Instrumentation image plane 1 dispersed Img. plane 2 : achromatic pupil plane Order 1 rays, focused by primary array Spacecraft 1 holding primary Fresnel array Spacecraft 2 holding focal instrumentation The field - bandpas compromise Chromatically aberrated beam at prime focus Field delimited by field mirror The chromatic corrector does a good job, but it corrects only what it collects. II. Lab prototype, optical and numerical test results Prototype built at Observatoire Midi Pyrénées in Toulouse 2006 - 2008 Lab Prototype: light source module • Étoiles doubles photo source test • Galaxies en spirales photo Exemples de sources test Disque Ø 0,8" d'arc Binaire Disque Ø 32 " d'arc Gravure : Micro Usinage Laser. mire 72 " d'arc Lab prototype: Fresnel array module C = 8 cm 116 zones (26 680 apertures) Opaque foil: inox 80 µm thick Tested in the visible (450-850 nm) F= 23 m for l= 600 nm Lab prototype, Focal module Field "lens" 23 m Order 0 Mask Chromatic correction + doublet focalization Final image Lab prototype, focal module, zoom on the corrector lens • 116 zones, 16 mm diameter, Blazed for 600 nm • Fused silica • Résolution selon le plan de la lentille de 1nm, hauteur des marches PTV 1.37 µm • Ion beam etched (SILIOS), 128 levels, • 1 mm "location" precision, 10 nm "depth" precision Diverging Fresnel lens mounted in the optical train Qualitative results: images of artificial sources broad spectral illumination: 550 - 750 nm uniform Disk 0.8 arc sec uniform Disk 0.8 arc sec with turbulence uniform Disk 32 arc sec double source high dynamic range Galaxy-shaped target 72 arc sec Quantitative results: measured angular resolution Diffraction limited theoretical profile Sampled optical point spread function The prototype is quasi diffraction limited Quantitative results: dynamic range optically measured versus numerically simulated In these saturated images of a point source, the average background is at 2 *10 -6 Luminosity scale amplified x1000 8 cm 116 zones Optical image Luminosity scale amplified x1000 8 cm 116 zones Numerical Fresnel wave propagation Through all the optical elements The numerical Fresnel propagation tool has been developed for testing large arrays Quantitative results: PSF of a 300 zones Fresnel Imager (720 000 apertures) numerically simulated Log dynamc range QuickTime™ et un décompresseur TIFF (non compressé) sont requis pour visionner cette image. Not apodized, no order 0 mask Quantitative results: PSF of a 300 zones Fresnel Imager (720 000 apertures) numerically simulated Log dynamc range Apodized, order 0 masked Quantitative results: PSF of a 300 zones Fresnel Imager (720 000 apertures) Prolate apodized, order 0 masked Log dynamc range Position in the field (resels) 1/4 of the field represented Beyond Orthogonality : improving transmission efficiency and dynamic range directionnal " Spergle" type Quantitative results: PSFs of non-orthogonal, square aperture imagers 300 zones, Square aperture cosine apodized, order 0 masked luminosity scale: Power 1/4 to show background Quantitative results: Convolution simulations 300 zones, Square aperture cosine apodized, order 0 masked The spikes do not degrade extended images PSF HH_30BW, raw image (from HST) HH_30BW, convoluted III. Space missions scenarios To be proposed for the 2020-2025 period Generation II prototype: tests on high dynamic range sky sources Not quite yet QuickTime™ et un décompresseur TIFF (non compressé) sont requis pour visionner cette image. XIXth century, 19 meter long, 76 cm Nice Obs refractor Generation II prototype: tests on the sky 350 zones, 20 cm aperture 20 meter focal, 700 mas resolution 106 or more dynamic range To be built and operated 2008-2010, financed by CNES, subject of a present Ph.D. thesis III. Space missions scenarios Space Missions scenarios: Formation flying configuration "lens" and "receptor" vessels for a 10m circular array configuration Space Missions scenarios: Formation flying configuration simple pare soleil multi couches Mat isolent structure type Astromesh ressorts à force constante 100K 10 à 30K sat 50K V-groove difficulté de mise en œuvre (voir JWST) Space Missions scenarios: Navigation Control Scheme Principe des mesures (2x2 d.d.l. + F) : 1) Le « dépointage » du grand axe optique (Zopt) par rapport à la cible ZG est représenté par DqL. Il permet d’estimer le déport latéral DxL = F. DqL. Sa figuration sur le plan focal du SSSL (ci-contre) est représenté par l’écart entre le motif des diodes laser implanté sur la grande lentille et la cible stellaire, caractérisée, en fait, par un « motif stellaire » avec ou sans la cible (cachée par la lentille en « contrôle fin »). 2) Le dépointage de l’axe optique du Récepteur par rapport au grand axe optique (DqR) est représenté par l’écart angulaire Olp[ ZOR, ZOPT ]. ZOR Oor ZG(étoile) F DqL Zopt DqL P ZL P Grand Axe « optique » Plan focal du SSSL dans l’Optique Réceptrice ZG (la Axe Optique du Récepteur : cible) ZOR DqL(= DxL/F) DqR Lentille de Fresnel Diode Laser Dq R Dx L Satellite Satellite Lentille de Récepteur Fresnel Schéma de principe de l’instrument distribué ZOPT (grand axe optique) 3) Mesure de la distance Focale: En fin de phase d’acquisition, on estimera F à partir de la taille du motif de diodes laser. Par contre, la mesure fine de la focale sera effectuée par télémétrie Laser en phase de contrôle fin. Space Missions scenarios: key parameters for spacecraft architecture Orbit and mission - environment - Communications to ground - Vessel to vessel communications - technology - fabrication - Lissajou orbits Moon 40° SUN small Lissajou sun period: 6 months line of sight 1 avoidable eclipse every 6 years Fresnel lens Trajectoire typique montrant qu'au-delà de 100 000 km de la Terre, light shield sun ecliptic plane acceptable depointing angle of the line of sight = total shield angle protection – Earth, Sun and Moon covering (fonction of the L2 orbit) Earth L2 Moon worst case every 28 days TMI Reflector Array (0 à 40°) 1 on receptor spacecraft facing earth 200 000 km typically: la MGA pointée comme le GS voit la Terre avec ses 40° d'ouverture fixed RA Antenna & GS Possible a partir de 100 000km from Earth TM/TC 2 par satellite terre/antiterre Liaison RF sensing (type SimbolX) inter-satellite pour la formation Space Missions scenarios: focal instrumentation Intégration of science and navigation channels: privileged Scenarios Space Missions scenarios: focal instrumentation chromatic correction optics LFC By réfraction By reflection MFCF • NUV+VIS+NIR : lentille de Fresnel blazée à l’ordre –1 qui fonctionne en transmission, suivie d’un doublet convergent et achromatique technologie validée TRL04 : R&T CNES 2004-2007 • UV : miroir de Fresnel blazée à l’ordre –1 ayant double fonction : 1- Réseau correcteur en réflexion et hors axe. 2- Focalisation du faisceau par une concavité globale additionnelle R&T CNES à venir. IV. Astrophysical targets Extra Galactic and Young Universe Scientific Requirements Mission Physical Phenomenon Spectral Range (nm) Dynamic Range within. Angular Resolutions (mas) 5 resels Extra Galactic lensing Column density mapping Black Body, Axion Ray Detection" 2000 5000 10-4 14 - 34 Extra Galactic lensing Column Density mapping, Black Body 600 2000 10-4 12 - 41 Extra Galactic to Z, Lyman a Young Universe, Galaxy formation 1000 2000 10-4 7 - 14 Extra Galactic to Z, Lyman break Re-inonization period of the universe 600 1200 10-4 12 - 25 Color Code => Spectral Band : IR NIR Vis NUV FUV Extra Galactic and Young Universe Instrumentation specifications t =3 h : for Changing Object Mission D (m) Extra Galactic lensing 30 D, Field of View (m) t = 6 h :for Changing Spectral Band Channel Capture size and Bands xy l Transfer Rate kbps Amount Integr Mission captured ated Duration Images time (h) (years) 2 Pointing M2 2000*2000 3 bands 11 4300 10 6,4 2000*2000 3 bands 11 9262 3 6,3 36 3993 20 8,9 11 9160 3 6,3 Extra Galactic lensing 10 1,2 Pointing M2 /Separati on Extra Galactic at Z, Lyman a 30 2 Pointing M2 2000*2000 Extra Galactic at z, Lyman break 30 2 Pointing M2 2000*2000 10*10*2000 10*10*2000 Active Regions in Our Galaxy Scientific Requirements Missions Physical Phenomenon Spectral Band Dynamic range in 5 (nm) resels Angular Resoluti on (mas) Central Galactic Region, Dust and Globular Cluster Density mass, Central Black hole, I.R. absorption in interstella 2000 5000 10-4 14 - 34 Ionized density of Galactic Clouds, Active Core “Astrochemistry” - Extra Galactic core 280 450 10-4 6-9 Ionized density of Galactic Clouds, Active Core Astrochemistry, development of interstellar in Heavy element, High Energy 120 280 10-4 7 - 17 Distance Between Objects : 0,2° - 0,5° No of Objects per spectral Band : 20 Color Code => Spectral Band : IR NIR Vis NUV FUV Active Regions in Our Galaxy Instruments specifications Mission Cgr (m) D, Field of View (m) 2 Channel Capture size and Bands Transfe r Rate kbps xy l Pointing M2 2000*2000 Central Galactic Region, Dust and Globular Cluster 30 Ionized density of Galactic Clouds, Active Core 10 1,2 Pointing M2 /Separatio n 2000$2000 Ionized density of Galactic Clouds, Active Core 3,5 0,6 Pointing M2 2000*2000 Amoun Integrat Mission ed time Duration t (h) (years) capture d Images 11 5192 120 7,7 21 6438 10 6,0 43 4050 5 5,9 3 bands IR NIR Vis NUV FUV 10*10*2000 10*10*2000 Imagery Stellar and Circumstellar With a 500 m array ? Imagery Stellar and Circumstellar Scientific Requirements Missions Accretion disk, Jets, Photospheres Physical Phenomenon Evolution of stellar, Mass in Extreme conditions Spectral Band (nm) 130 Dynamic range in 5 resels 10-5 10-5 Angular Resoluti on (mas) 1 Pphotospheres and Circumstellar Physic stellar 280-450 Photospheres and Circumstellar : Near objects Physic stellar, Circumstellar Clouds 250 10-5 5 Photosphere et Circumstellar : Far objects Physic stellar, Circumstellar Clouds 250 10-5 2 IR NIR Vis NUV FUV 15 - 29 Imagery stellar et circumstellar Instrument Specifications Mission Cgr (m) Accretion disk, Jets, Photospheres 30 D, Field of View (m) Channel 2 none Capture size and Bands xy l Photospheres, Circumstellar 3,5 0,6 Pointing M2 /Seperati on Photospheres, Circumstellar : Near objects 10 1,2 none Photosphere, Circumstellar : Far objects 30 2 none IR NIR Vis NUV FUV 4000*4000 400*400*1000 2000*2000 400*400*400 2000*2000 400*400*400 4000*4000 400*400*1000 Transfer Rate kbps Amount Integra Mission ted Duration captured Images time 43 2683 20 7,0 213 19299 1 8,8 213 23217 1 10,6 85 6191 10 9,2 (h) (years) Exoplanets Earth @ 10 pc detection and spectroscopy 40m array, 300 Fresnel zones, PIAA, spectral resolution 50, 2*48h "Exoplanets" Scientific Requirements Missions Physical Phenomenon Spectral Band (nm) Dynam ic range in 5 resels Angular Resolution (mas) Exoplanets joviennes Planets Systems, atmospheres 600 -1200 10-8 17 - 25 Exoplanets telluric in IR Planets Systems, atmospheres 2000-5000 10-8 40 - 100 Exoplanets joviennes and telluriques Planets Systems, atmospheres 600 -800 10-8 4-6 Exoplanets tellurics in IR Planets Systems, atmospheres 2000-5000 10-8 14 - 34 IR NIR Vis NUV FUV Exoplanets Instruments Specifications Mission Cgr (m) D, Field of View (m) Channel Capture size and Bands xy l Transfer Rate kbps Amou Integra Mission ted Duration nt (years) captur time (h) ed Images Exoplanets Exoplanets Exoplanets Exoplanets 10 10 30 30 1,2 1,2 3 3 Point at M2 4000*4000 Point at M2 4000*4000 Point at M2 4000*4000 Point at M2 4000*4000 71 6500 10 9,6 43 6300 10 9,4 213 4400 10 6,6 85 6000 10 9,0 300*300*100 300*300*100 300*300*100 300*300*100 IR NIR Vis NUV FUV ¡Muchas gracias por su atencion! Bonus slides Achromatisation principle Converging lens Operating at order -1