Experimental demonstration of a crossed cubes nuller for

Multi-axial combiner. (exit pupil plane). Z. O'. F'. Wavefront sensor. Wavefront sensor. B'. P'2. Focal plane. P'1. X”. (P'). Crossed- cubes nuller. Monolithic.
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Experimental demonstration of a crossed cubes nuller for coronagraphy and interferometry François Hénault, Brahim Arezki Institut de Planétologie et d’Astrophysique de Grenoble, Université Grenoble-Alpes, CNRS, B.P. 53, 38041 Grenoble – France Alain Spang Laboratoire Lagrange, Université Côte d’Azur, Observatoire de la Côte d’Azur, CNRS, Parc Valrose, Bât. H. FIZEAU, 06108 Nice – France Y

eiπ/2

AT AT

eiπ/2

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eiπ/2 AR AT

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eiπ/2 AR AR

AR

X-polarized

AR AT

eiπ/2

π/2

π

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π

π

-π/2

π

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eiπ/2 eiπ/2 Y

Y-polarized

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Cubes polarization model

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Summary - Two “crossed” beamsplitter cubes have their semi-reflective layers perpendicular one to the other - The input beam propagates parallel to both cubes layers. It is spitted into four parallel beams, being recombined axially - Only two of those beams are used to generate a “null” at the focal plane centre - It is independent of wavelength and polarization orientation → This is actually an Achromatic phase shifter

Two beams (ATAT–ARAR)

Four beams

Interference fringes

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Z

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Two beams (ATAR–ARAT)

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Cube 2

Cube 1

256 pixels of 5.2 µm

Spectral power density

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N ≈ 1.8 10-3 N ≈ 2.210-3 First fringes

Image plane Focusing optics Cube 1

Cube 2

Secondary Mirror

Advantages Monolithic telescope

(P)

Converging optics Diverging optics Fold mirror Beamsplitter or dichroïcs

Primary Mirror

Relay optics

Wavefront sensor

Crossedcubes nuller

Multi-axial combiner (exit pupil plane)

P’1

O’

(P’) P’2 F’

B’ Focal plane

O” Z

X”

Simple, compact, low mass and volume Reasonable manufacturing tolerances Potentially not expensive Not sensitive to chromatic flux mismatch Can be implemented into a nulling coronagraph telescope or a sparseaperture nulling interferometer • Very small Inner working angle (IWA) when used as a coronagraph • Capacity for fringes rotation and baseline modulation • Good candidate for future space missions characterizing extra-solar planets atmospheres • • • • •

B

P1

O

P2 (P)

Telescope 1

Telescope 2

Relay optics 1

Crossedcubes nuller

Relay optics 2

Fringe tracker 1-4 Tip-tilt sensors

Fringe tracker 2-3 Tip-tilt sensors

Fringe tracker 14-23

(P’) O’ F’

O”

Focal plane Z

Contacts [email protected] [email protected]