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The VLTI Auxiliary Telescopes |
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| Last Breaking News | |
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ESO Press Release 06/05 VLTI First Fringes with two Auxiliary Telescopes |
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ESO Press Release 01/04: First Auxiliary Telescope for the VLT Interferometer Installed at Paranal. (30/January/2004). |
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ESO PR Video 01/05 Two Auxiliary Telescopes at Paranal [QuickTime:
160 x 120 pix - 37Mb - 4:30 min] |
ESO PR Photo 07a/05 [Preview
- JPEG: 493 x400 pix - 44k] |
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Captions: ESO PR Video Clip 01/05 is an extract from ESO Video Newsreel 15, released on March 14, 2005. It provides an introduction to the VLT Interferometer (VLTI) and the two Auxiliary Telescopes (ATs) now installed at Paranal. ESO PR Photo 07a/05 shows the impressive ensemble at the summit of Paranal. From left to right, the enclosure of VLT Antu, Kueyen and Melipal, AT1, the VLT Survey Telescope (VST) in the background, AT2 and VLT Yepun. |
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The contract with AMOS is for the design, manufacturing, testing in Europe, and packing of three Auxiliary Telescopes and of the full set of on-site equipment for the 30 AT observing stations.
The AMOS deliverable items include the complete set of optics (11 mirrors plus camera optics), the complete mechanics for the Telescope, Transporter and site equipment, all drives, encoders and associated electronics as well as all control functions for the Transporter. However, the following tasks are outside the scope of the contract and will be performed directly by ESO:
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Preview [JPEG: 800 x 944 pix - 536k]
[High-Resolution [JPEG: 3000 x 3540
pix - 3.3Mb]
This photo shows a model of an Auxiliary Telescope during Observing Conditions. The 1.8-m telescope (with an Alt-Az mount, i.e. exactly like the Unit Telescopes) is rigidly anchored to the ground by means of a special interface. The light is directed via a series of mirrors (the Coudé Optical Train) to the bottom of the Telescope. From the Coudé Relay Optics it is sent on to the underground Delay Line Tunnel.
The AT Enclosure (telescope dome) consists of 2 x 3 segments and is here fully open. It protects the lower part of the Telescope structure from strong winds. The Enclosure is supported by the Transporter that also houses electronic cabinets and service modules for liquid cooling, air conditioning, auxiliary power, compressed air, etc.
During astronomical observations, the Enclosure/Transporter is mechanically disconnected from the Telescope and is anchored independently of the Telescope on the rail foundations that rest on soft elastomeric pads. This ensures that vibrations generated by the Enclosure/Transporter or from the ground are not transmitted to the Telescope. At the time of the observations, the Telescope is controlled remotely from the VLTI Control Room.
This picture shows the Auxiliary Telescope during Relocation from one observing station to another. The Transporter carries the Telescope using a rail network connecting all 30 stations.
The Relocation is a complex operation that involves quite a few steps:
First, the Telescope inside the closed enclosure is undocked from the ground
and lifted by jacks located on the Transporter. The electrical cables
to the station are disconnected and power is supplied by the on-board battery
set. The Transporter is then unlocked and moved sideways so that the Coudé
Relay Optics Box can be lifted up from inside the station. This box can
be seen in the photo after it has been lifted on the left side of the Transporter.
The lid that protects the station (the white octagon) is then placed on top
of the station.
Next, the Transporter is moved along the rails to the chosen station. This movement
may include a rail crossing at which the Transporter wheels are first lifted,
then rotated by 90° and again placed on the tracks in the perpendicular
direction. When reaching the desired station, the station lid is opened, the
Coudé Relay Optics is lowered inside the station pit and the Telescope
and Transporter are anchored to their respective foundations.
The positioning accuracy of the various mechanisms is so good that no local
re-alignment should be necessary, although this can be done remotely from the
control room before the next observation.
During the Relocation itself, the control of the Transporter is done locally from a handset by a maximum of two operators.
| Optical Configuration | Ritchey Chretien with Coudé train and Coudé Relay Optics sending a 18 mm collimated beam horizontally underground towards the Delay Line Tunnel. |
| Primary mirror | f 1.8 m, F/1.5 (k=-1.0006) |
| Secondary Mirror | f 138 mm, F/1.6 (k=-1.281) |
| Coudé Mirrors | 8 mirrors (flat, cylindrical and spherical) with intermediate pupil image to locate an Adaptive Optics deformable mirror. |
| Coudé focus | F/36.2. Located underground. Equipped with field acquisition camera (CCD) and fast tip-tilt sensor (APD Quad-Cell) |
| Coudé Relay Mirrors | 1 dichroïc + 2 mirrors including steerable field mirror for lateral pupil adjustment. |
| Output beam | f 18 mm collimated, 1.25 m underground |
| Optical Quality | < 110 nm FWE rms in the output pupil. |
| Optical Path stability | < 15 nm rms over any 0.01 sec (allowing interferometry down to visible spectral range) |
| Magnification Factor | 100 +/- 1 |
| Polarization | < 30° linear retardation: (fp-fs)Tel.2-(fp-fs)Tel.1 |
| Spectral range | 0.4 to 25 µm |
| Mount type | Alt-Az. Altitude axis 5 meters above ground to limit the impact of "ground seeing". |
| Telescope drives (Alt & Az) | Direct drives with tachometers and high accuracy incremental optical encoders |
| Pointing accuracy | < 2.0 arcsec rms absolute (over all sky) < 0.2 arcsec rms relative (over 10 arcmin) |
| Tracking accuracy | < 0.2 arcsec rms over 10 sec < 0.5 arcsec rms over 10 min |
| Sky coverage | Zenith distance: 0.5° to 60°. Azimuth: >360° |
| Atmospheric compensation | Tip-tilt in a first phase: diffraction limited at 2.2 µm
(< 0.025" rms, for mV<16) Full Adaptive Optics in a later phase |
| Total mass of the system (including telescope) | < 30Tons |
| Time to relocate between observing stations (worst case) | < 3 hours |
| Positioning accuracy of the Telescope after relocation | +/- 0.1 mm displacement, +/- 10 arcsec angular |
| Enclosure type | Segmented half sphere retractable down to Altitude axis for
good ventilation (dome seeing). Air conditioned during daytime. |
| Heat dissipated close to the light path | < 25W |
| Primary mirror thermal control accuracy | +/- 0.5°C |
| Operational Wind Speed (full performance) | 10 m/sec |
| Survival Wind Speed | 47 m/sec (no damage) 54 m/sec (minor damages allowed) |
| Operational Temperature range (full performance) | 0 to 15°C |
| Micro-seismic activity (full performance) | 0.2 µg/ÖHz in [2-100]Hz |
| Survival seismic activity | MR=7.75 at 100 km / Peak acceleration 0.24g (no
damage) MR=8.5 at 150 km / Peak acceleration 0.34g (damages allowed) |
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| Kick-off |
June 1998
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| Preliminary Design Review |
November 1998
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| Final Design Review |
April 1999
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| AT #1 ready at Paranal |
November 2004
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| AT #2 ready at Paranal |
March 2005
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| AT #3 ready at Paranal |
November 2005
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| AT #4 ready at Paranal |
May 2006
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| First Fringes AT#1 & AT#2 at Paranal |
February 2005
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| First Fringes AT#1, AT#2,AT#3 at Paranal |
November 2005
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| First Fringes AT#1, AT#2, AT#3, AT#4 at Paranal |
May 2006
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