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G. Tagliaferri, D. Spiga, G. Pareschi, et al.

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Presentation on theme: "G. Tagliaferri, D. Spiga, G. Pareschi, et al."— Presentation transcript:

1 Development of grazing-incidence X-ray optics @ INAF/OAB and proposed optics for XIPE
G. Tagliaferri, D. Spiga, G. Pareschi, et al. INAF – Osservatorio Astronomico di Brera Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

2 Gianpiero Tagliaferri – INAF/OABr
Simbol-X design, study and development WFXT Feasibility Study eROSITA SPECTRUM X-Gamma CNR - Milano Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

3 Gianpiero Tagliaferri – INAF/OABr
Beppo-SAX soft X-ray (0.1 – 10 keV) concentrators Wolter I double-cone approx. – Au coating 4 modules – 30 shells/mod. F.L. = 180 cm Max diam = 16.1 cm Aeff @ 1 keV = 85 cm2 /module HEW= 60 arcsec (corresponding to the double-cone geom. aberration!) GRB970228 Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

4 Gianpiero Tagliaferri – INAF/OABr
JET-X (optics ready since1996) / SwiftXRT(2004) optics Wolter I profile – Au coating (pathfinder of XMM) 2 mod. (JET-X) / 1 mod (Swift) – 12 shells/mod. F.L. = 350 cm - Max diam = 30 cm Aeff @ 1 keV= 150 cm2 /module HEW= 15 arcsec Source separation: 20” Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

5 Gianpiero Tagliaferri – INAF/OABr
SWIFT-XRT Layout XRT mating with Swift spacecraft Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

6 The optic wheel necessary to mount the mirror modules
POLARIX The optic wheel necessary to mount the mirror modules Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

7 Gianpiero Tagliaferri – INAF/OABr
Fabrication of a thin (130 mm) MS from the largest JET-X mandrel To verify the imaging capabilities of thin Ni electroformed mirrors, we realized a 0.13 mm Au coated shell exploiting the largest JET-X mandrel  the thickness has been diminished of a factor 8.5 with respect JET-X/SWIFT  = 30 cm Height = 60 cm Focal Length = 3.5 m Thickness = 0.13 mm Mirror mass = 660 g Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

8 Gianpiero Tagliaferri – INAF/OABr
X-ray imaging test of a thin JET-X mirror shell (July ‘02) diam. = 30 cm thickness = 130 mm wall thickness 8.5 times less than JET-X HEWmeas = 25 arcsec X-Ray Panter-MPE (July ’02) - E = 1.5 keV Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

9 Multilayer coated Ni mirror shells tested at Panter
1 keV 40 keV Energy (KeV) HEW (arcsec) 1.5 23 8 24 20 27 35 31 50 33 Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

10 Proposed new Mirror design for XIPE
3-mirror modules with FL=3.5 m 27 shells with the same thickness as for NHXM, diameter min=183 mm, max=400 mm Electroformed in Ni (or NiCo) with Ir+C coating Total weight of 1 MM is ~40 kg (shells 30kg, 30% structure, total for 3MM=120 kg) Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

11 Proposed new Mirror design for XIPE
3500 Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma

12 Gianpiero Tagliaferri – INAF/OABr
CONCLUSIONS 3 MMs with ~1400 cm2 at 1-3 keV and 750 cm2 at 8 keV Same shell properties as the ones developed for the Simbol-X & NHXM programs Same technology and integration scheme used for BeppoSAX, XMM-Newton, Swift, eROSITA, so TRL≥6? Gianpiero Tagliaferri – INAF/OABr XIPE – ESA/M4 -Roma


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