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Figure 1: A Carlina version using six computer-controlled winches to define the position and attitude of the focal beam combiner. These can be combined as three differential winches. |
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Figure 2: The optics in the gondola will consist of a clam-shell corrector of spherical aberration, a pupil densifier and an EM-CCD camera. Adaptive optics will also be needed to correct the positioning errors of the fixed primary mirrors, in tip-tilt and piston, as well as the atmospheric seeing. |
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Figure 3: Equatorial mode of star tracking with a Carlina. A single computer-controlled winch suffices to track the star. |
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Figure 4: Clam-shell corrector of spherical aberration and coma calculated with the Lasso code for F/2 acceptance. The paraxial and marginal foci of the primary mirror M1 ( located far at right and not shown) are indicated. The corrected focus is at left, near the central hole of M2. |
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Figure 5: Spot in the image plane of the clam-shell Mertz corrector for stars located up to 16.7'' (top-right) from the optical axis, as calculated with the Lasso code. The smaller scale units on the X and Y axes correspond to 5 microns. |
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Figure 6: Coudé feed in the gondola's focal optics. After the focal corrector of spherical aberration and the pupil densifier, using a pair of lens arrays, a flat mirror directs a coudé beam towards the focal station at ground level. The mirror must be rotated to accomodate different stellar declinations |
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Figure 7: Alternate scheme to Fig. 6 for coudé optics, using a small tiltable flat mirror and a paraboloidal mirror. The pupil densifier and the CCD are in the coudé station at ground level. |
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Figure 8:
The top-left of the figure shows a preliminary measurement of the
residual oscillations at OHP.
A gondola without optics is placed under a balloon at 35.6 m above ground. It oscillates by a few millimeters
(rms) in the wind (![]() ![]() |
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Figure 9: Test optics arranged in the optical tunnel to develop phasing techniques. Two Carlina mirror segments spaced 35 cm apart produce fringes in the image of a point source located at their common center of curvature, 71.2 m away. A camera records the fringes, found by using a laser with adjustable coherence length. With a white source, the piston balance can be adjusted within one micron. |
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Figure 10: Scale drawing of the Carlina prototype at the observatory. Pending crater sites, the flat ground is usable with a limited sky coverage in declination. The 4 mm Kevlar cables are thickened to make them visible. The 20-m dome of the 193 cm telescope appears on top to indicate the scale. The 1.5 m boule telescope at bottom-left, initially built as a prototype for the Optical Very Large Array (Arnold et al. 1999), is here potentially usable as a coudé collector receiving light from the focal gondola (described in Sect. 2.3). |
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Figure 11: Star acquisition system for Carlina. A small telescope is placed at the edge of the primary mirror segment and tracks the star. The light of a LED near the CCD in the gondola is reflected from the primary mirror segment towards a corner-cube reflector attached on top of the small telescope. The LED and the star are seen in the telescope eye-piece and must be superposed by moving the gondola. |
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Figure 12: top: tethered balloon, 140 m above ground. The black disc seen near the tail of the balloon is at the curvature center of the primary mirror, 71.2 m above it, and also at the top of the fixed cable tripod (see Fig. 3). The black triangle frame is the gondola, about 3 m in size and made of 16 mm diameter carbon fiber tubes, which carries the CCD, 35.6 m below this point. Bottom: first light for the Carlina prototype with a single primary mirror segment on star "Psi Ursae Majoris'' obtained on 02/03/2004. The lateral field of the CCD image shown is about one arc minute and the size of the star image is close to 7 arcsec due to astigmatism, focus error and seeing. |
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Figure 13: Fringes obtained on Vega with the pair of adjacent mirrors stopped down to about 5 cm and providing a 40 cm baseline. |
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