4.5.2, 4.6, 5.1.1, 5.1.2
modified. Figure added in
5.1.1, Table 11 updated, old
Table 3 removed. + modified
structure of the sections
88
27.02.2011
01.03.2011
03.03.2011
07.03.2011
28.03.2011
20.06.2011
Modified sects. 1.3, 2.2.1.3,
2.2.4.2, 2.3.2, 2.4, 2.4.3,
2.4.4, 2.4.6.1, 2.4.7, 3, 3.2,
3.3.1, 3.3.2, 3.3.3, 3.3.4,
4.1.1, 5, 5.1, 5.6.1, 5.6.2,
5.7, 5.9, 6.1.3, 6.2.3
New Sects 2.4.10, 2.4.11,
2.4.12, 2.4.13, 2.4.13,
2.4.14, 3.4, 3.4.1, 3.4.2,
3.4.3, 3.4.4, 3.4.5, 3.4.6
Modified tables: 2, 7, 11, 12,
66
New tables: 10, 13
Modified figures: 10, 15
New figures: 5, 11
New subsections 2.4.6, 6.1.3
CMa,
update wrt
the performances,
new identified problems
and status + description of
the current ones.
New items in the FAQ,
new calibration plan,
new section about the
observation strategy.
Figures updated to be more
clear and useful.
NIR 1.5” slit removed.
Intervention of July 2011
briefly described
+additional corrections of
figures and sections
according to IOT comments.
Very minor changes.
New templates added +
minor corrections
89
04.08.2011
30.11.2011
Modified Sections: 2.1,
2.2.1.4, 2.2.4.2, 2.2.4.5,
2.3.2, 2.4.6, 2.4.9, 2.4.13,
2.4.15, 3.4.1, 5.1, 5.5, 5.7,
6.1.5, 6.2.3.
New sections: 2.2.4.3, 2.4.7
Modified tables: 1, 9, 12, 13,
16, 72
New tables: 3, 4, 10
CMa, major modifications wrt
the new slits in the NIR +
new slits with K-band
blocking filter added and
background performances +
the new TCCD
performances + the new
calibration plan + correction
of typos and clarification of
different points (attached
calibrations, known
problems, etc), weblinks
modified.
Modifications regarding
phase2 + changes for the
acquisition+setup+readout+
wiping overheads.
+ additional information
regarding integration times
for the TCCD.
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90
20.02.2012
03.04.2012
Modified sections: 2.2.1.4,
2.2.4.5, 2.4.3, 3.4.3, 4.1.2,
5.1, 5.4, Table 16 revised
Clarification of 2.2.4.3 (new
NIR slits)
New 6.1.2 for better
explanation of slit orientation
and offsets.
DIT of 1800s with JH slits,
TCCD limiting magnitudes +
direct acquisition. Telluric std
star observations,
How to minimize the
overheads and optimize the
integration times. Calibration
plan revised.
Phase 2: minor
modifications, re-writing
sentences + new draws+
contacts added at the
beginning (already present
in other pages) Other minor
adjustments of the tables
and links.
90/91
08.08.2012
No ADCs mode: sect. 2.2.2,
updates of sects. 2.4.2,
24.13-1.4.15, 3.1, 3.4.3, 5.7,
5.9
Adding a new section about
the observations without
ADCs (2.2.2). Updates of
sections for the observations
in slit with disabled ADCs +
more infos for the IFU.
Updates wrt the telluric std
star policy starting in P91.
91
09.10.2012
Transmission curve of the Kband blocking filter added.
Telluric std star policy
updated for P91.
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91/92
10.02.2013
Section 3.2 split in 2: 3.2.1
3.2.2
New section 3.3
New section 1.6
Sects 3.2.1/3.2.2: main acq
loop and 3.2.2 blind offset
precision
--New section 3.3 about
examples of OBs
preparation with p2pp3
especially regarding the
acqs (direct or blind offsets)
--new section 1.6 regarding
the acknowledgements
--warning about the snapshots
during the acquisitions
offsets that will not be saved
anymore, only last
snapshots end of acquisition
kept.
--warning about the exposure
times of all calibration
frames that will be revised.
--warning about the
wavelength calibration at
night that should be
performed with 2dmap
template instead of ARC.
P92
Change of format .doc to
.odt, allowed 2dmap wave
calibrations at night, Move of
XSHOOTER from UT2 to
UT3
minor changes in various
sections
P93
Back to format .doc
Introduction of the
XSHOOTER imaging mode
(new sect 4), comments in
various sections
Minor changes every where
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P94
26.02.2014
Minor changes, references
to the imaging mode user
manual added. New table
about the limiting magnitude
for a S/N=10 in sec 2.2.1.4.
Some details provided for
the dichroic dip oscillation,
corrected cross-references.
30.06.2014
All
CMA: Merging imaging
mode manual with main
manual as per ESO
standard.
Correction of some language
issues, obsolete sections
removed or reorganized.
Radial velocity accuracy
added, telluric lines
correction tool reference
added, updates of
references and features
ESO, Karl-Schwarzschild-Str. 2, 85748 Garching bei München, Germany
Range: 1000-2500 nm in 16 orders
Resolution: 5100 (0.9" slit)
Slit width: 0.4”, 0.6”, 0.9”, 1.2”, 1”, 5.0”,
0.6”JH, 0.9”JH
Detector: 2k x 1k Hawaii 2RG
Slit length
11” (SLIT) or 12.6” (IFU)
Beam separation
Two high efficiency dichroics
Atmospheric dispersion compensation
In the UV-Blue and Visual-red arms
Disabled on Aug. 1st ,2012
Integral field unit
Acquisition and guiding camera
1.8" x 4" reformatted into 0.6" x 12"
1.5’x1.5’ +Johnson and SDSS filters
1. Introduction
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Table 2: collaborating institutes and their contributions
Collaborating institutes
Contribution
Copenhagen University
Observatory
Backbone unit, UVB spectrograph, Mechanical
design and FEA, Control electronics
ESO
Project Management and Systems Engineering,
Detectors, final system integration,
commissioning, logistics, Data Reduction
Software
Paris-Meudon Observatory,
Paris VII University
Integral Field Unit, Data Reduction Software
INAF - Observatories of Brera,
Catania, Trieste and Palermo
UVB and VIS spectrograph, Instrument Control
Software, optomechanical design.
Astron, Universities of
Amsterdam and Nijmegen
NIR spectrograph, contribution to Data
Reduction Software
1.1 Scope
The X-shooter User Manual provides extensive information on the technical characteristics of
the instrument, its performances, observing and calibration procedures and data reduction.
1.2 X-shooter in a nutshell
X-shooter is a single target spectrograph for the Cassegrain focus of one of the VLT UTs
covering in a single exposure the spectral range from the UV to the K band. The spectral
format is fixed. The instrument is designed to maximize the sensitivity in the spectral range
through the splitting in three arms with optimized optics, coatings, dispersive elements and
detectors. It operates at intermediate resolutions (R=4000-18000, depending on wavelength
and slit width) sufficient to address quantitatively a vast number of astrophysical applications
while working in a background-limited S/N regime in the regions of the spectrum free from
strong atmospheric emission and absorption lines. A 3D CAD view of the instrument
attached to the telescope is shown on Figure 1. Main instrument characteristics are
summarized in Table 1.
A Consortium involving institutes from Denmark, Italy, The Netherlands, France and ESO
built x-shooter. Name of the institutes and their respective contributions are given in Table 2.
1.3 Shortcuts to most relevant facts for proposal preparation
The fixed spectral format of X-shooter: see Table 11 on page 49
Spectral resolution as a function of slit width: see Table 12 on page 51
Information on the IFU: see Section 2.2.1.3
Information on limiting magnitudes in the continuum: see Section 2.3.3 on page 52
Information on observing modes: see section 3.1 on page 61
Observing strategy and sky subtraction: see Section 3.3 on page 64
Overhead computation: see Section 4 on page 81
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A&G/AG
Acquisition and Guiding
ADC
Atmospheric Dispersion Compensator
AFC
Active Flexure Compensation
DCS
Detector Control Software
DEC
DFS
Declination
Data Flow System
DIT
Detector Integration Time
ESO
European Southern Observatory
ETC
FDR
Exposure Time Calculator
Final Design Review
FF
Flat Field
GUI
Graphical User Interface
ICS
Instrument Control Software
IFU
Integral Field Unit
ISF
Instrument Summary File
IWS
Instrument Workstation
LCU
Local Control Unit
N/A
Not Applicable
OB
PAE
Observing Block
Preliminary Acceptance Europe
P2PP
Phase 2 Proposal Preparation
RA
RMS
RON
SM
TBC
Right Ascension
Root Mean Square
Readout Noise
Service Mode
To Be Clarified
TCCD
QE
Technical CCD
Quantum Efficiency
SNR
Signal to Noise Ratio
TBD
To Be Defined
TCS
Telescope Control Software
TLI
Threshold Limited Integration
TSF
Template Signature File
VLT
VM
Very Large Telescope
Visitor Mode
WCS
ZP
World Coordinate System
Zeropoint
1.4 List of Abbreviations & Acronyms
This document employs several abbreviations and acronyms to refer concisely to an item,
after it has been introduced. The following list is aimed to help the reader in recalling the
extended meaning of each short expression:
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1.6 Acknowledgements
Please if you use XSHOOTER data, cite the following articles:
1. main article:
Vernet et al., 2011A&A...536A.105V
X-shooter, the new wide band intermediate resolution spectrograph at the ESO Very
Large Telescope
2. For the flux calibrations:
Vernet et al., 2010HiA....15..535V
Building-up a database of spectro-photometric standards from the UV to the NIR
Hamuy et al., 1994PASP..106..566H
Southern spectrophotometric standards, 2
3. For the pipeline and data reduction:
Modigliani et al., 2010SPIE.7737E..56M
The X-shooter pipeline
4. For the Reflex interface:
Freudling et al., 2013A&A...559A..96F
Automated data reduction workflows for astronomy. The ESO Reflex environment
5. For the imaging mode:
Martayan et al., The Messenger, 156, June 2014
The X-shooter Imaging Mode
1.7 Contact
In case of instrument related questions, use xshooter@eso.org
In case of phase1/2 related questions, use usd_xshooter@eso.org or usd-help@eso.org
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1.8 News
-In P94, XSHOOTER will probably go back to UT2. The imaging mode will again be
available.
- In P93 as in P92, XSHOOTER will be available at UT3 instead of UT2. This would allow
decreasing a bit the pressure factor on this instrument.
- In P93 is introduced the light imaging mode of XSHOOTER performed with the acquisition
and guiding camera. At the same time only a single snapshot is taken of the last image
during the acquisition loop (2 in case of blind offset before and after the blind offset). More
details will come in a dedicated document.
- Note: in P92 some tests were started of a new mode that allows observing very bright
objects (even negative magnitudes). Once the tests completed this mode could eventually be
offered to the community (manpower and time dependent).
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Figure 2: Schematic overview of X-shooter
2. Technical description of the instrument
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2.1 Overview of the opto-mechanical design
Figure 2 shows a schematic view of the layout of the instrument. It consists of four main
components:
The backbone which is directly mounted on the Cassegrain derotator of the
telescope. It contains all pre-slit optics: the calibration unit, a slide with the 3positions mirror and the IFU, the acquisition and guiding camera, the dichroic box
which splits the light between the three arms, one piezo tip-tilt mirror for each arm to
allow active compensation of backbone flexures, atmospheric dispersion
compensators (ADCs) in the UVB and VIS arms and a warm optical box in the NIR
arm.
The three arms are fixed format cross-dispersed échelle spectrographs that operate
in parallel. Each one has its own slit selection device.
o The UV-Blue spectrograph covers the 300 – 550 nm wavelength range with a
resolving power of 5100 (for a 1” slit)
o The Visible spectrograph covers the range 550 - 1000 nm with a resolving
power of 7500 (0.9” slit).
o The near-IR spectrograph: this arm covers the range 1000 - 2500 nm with a
resolving power of 5300 (0.9” slit). It is fully cryogenic.
2.2 Description of the instrument sub-systems
This section describes the different sub-systems of X-shooter in the order they are
encountered along the optical path going from the telescope to the detectors (see
Figure 2). The functionalities of the different sub-units are explained and reference is made
to their measured performance.
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Figure 3: 3D view of a cut through the backbone.
2.2.1 The Backbone
2.2.1.1 The Instrument Shutter and The calibration unit
In the converging beam coming from the telescope, the first element is the telescope
entrance shutter.
Then follows the Calibration Unit that allows to select a choice of flat-fielding and wavelength
calibration lamps. This unit consists of a mechanical structure with calibration lamps, an
integrating sphere, relay optics that simulate the f/13.6 telescope beam, and a mirror slide
with 3 positions that can be inserted in the telescope beam:
one free position for a direct feed from the telescope,
one mirror which reflects the light from the integrating sphere equipped with:
o Wavelength calibration Ar, Hg, Ne and Xe Penray lamps operating
simultaneously
o three flat-field halogen lamps equipped with different balancing filters to
optimize the spectral energy distribution for each arm
one mirror which reflects light from:
o a wavelength calibration hollow cathode Th-Ar lamp
o a D2 lamp for flat-fielding the bluest part of the UV-Blue spectral range
A more detailed description of the functionalities of the calibration system is given in Sect. 6.
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2.2.1.2 The Acquisition and Guiding slide
Light coming either directly from the telescope or from the Calibration Unit described above
reaches first the A&G slide. This structure allows putting into the beam either:
a flat 45˚ mirror with 3 positions mirror:
oacquisition and imaging: send the full 1.5’1.5’ field of view to the A&G
camera. This is the position used during all acquisition sequences;
ospectroscopic observations and monitoring: a slot lets the central 10”15” of
the field go through to the spectrographs while reflecting the peripheral field to
the A&G camera. This is the position used for all science observations.
oartificial star: a 0.5” pinhole used for optical alignment and engineering
purposes;
the IFU (described in Sect. 2.2.1.3);
a 50/50 pellicle beam splitter at 45˚ which is to used look down into the instrument
with the A&G camera and is exclusively used for engineering purposes.
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Figure 4: Top: view of the effect of the IFU. The central field is directly transmitted to
form the central slitlet (green) while the each lateral field (in blue and red) are reflected
toward a pair of spherical mirrors and realigned at the end of the central slice to form
the exit slit. Bottom: The field before (left) and after the IFU (right). The IFU acts such
that the lateral fields seem to rotate around a corner of their small edge. The two white
slots are not real gaps but just guides to help visualize the top and the bottom of each
slice in the drawing.
2.2.1.3 The IFU
The Integral Field Unit is an image slicer that re-images an input field of 4”x1.8” into a
pseudo slit of 12”x0.6”. The light from the central slice is directly transmitted to the
spectrographs. The two lateral sliced fields are reflected toward the two pairs of spherical
mirrors and re-aligned at both ends of the central slice in order to form the exit slit as
illustrated in Figure 4. Due to these four reflections the throughput of the two lateral fields is
reduced with respect to the directly transmitted central one. The measured overall efficiency
of the two lateral slitlets is ~85% of the direct transmission but drops to ~50% below 400 nm
due to reduced coating efficiency in the blue. An example of an IFU standard star is showed
in Figure 5.
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UVB arm
VIS arm
NIR arm
Blue orders
Red orders
Red orders
Blue orders
Blue orders
Red orders
Blue
Red
Blue
Red
Red
Blue
Below is an example of IFU observation of a telluric standard star:
Figure 5: IFU telluric standard star (B-type star). One can note the three slices in each order
of each arm. The telluric absorption lines are easily visible in the VIS and NIR arms.
One can also note the effect of the atmospheric dispersion (change of distance between the
slices between blue and red orders in UVB/VIS arms).
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U B V R I
22
22
22.5
22.5
22.5
30s
30s
20s
20s
20s
2.2.1.4 The Acquisition and Guiding Camera
The A&G camera allows to visually detecting and center objects from the U- to the z-band.
This unit consists in:
a filter wheel equipped with a full UBVRI Johnson filter set and a full Sloan Digital
Sky Survey (SDDS) filter set. Transmission curves are provided in appendix Error! Reference source not found..
a Pelletier cooled, 13 µm pixel, 512512 E2V broad band coated Technical CCD57-
10 onto which the focal plane is re-imaged at f/1.91 through a focal reducer. This
setup provides a plate scale of 0.173”/pix and a field of view of 1.47’1.47’. The QE
curve of the detector is provided in appendix Error! Reference source not found..
This acquisition device –that can also be used to record images of the target field through
different filters– provides a good enough sampling to centroid targets to <0.1” accuracy in all
seeing conditions.
The noise of the technical CCD is currently of RON of 4.1e-.
The limiting magnitudes for a direct acquisition were measured for different filters under
relatively bad conditions (thin cirrus, full Moon, seeing about 0.7”), see Table 3.
Table 3: Limiting magnitudes for a direct acquisition
We still have to measure their limiting magnitudes under clear conditions and in dark time.
However, in case of worse weather the limiting magnitudes are smaller.
We still recommend to use blind offsets in case the object is fainter than 22-22.5, especially
if the weather constraints are selected for thin/thick transparency and seeing worse than
0.7”. In case of blind offsets, we recommend to select an acquisition star with a magnitude
about 19 or brighter to ensure a good centering before the offsets are done.
For other SDSS filters, we recommend to keep a limiting magnitude of 20 for a direct
acquisition in I’ and z’ but to go up to 21 in other SDSS filters. The exact limiting magnitudes
for those filters will be determined during P93.
Examples of recommended exposure times for the acquisition CCD:
Vmag=6 integration time=0.001s
Vmag=7 integration time=0.005s
Vmag=16-20 integration time=1 to 5s
V, R mag=23 integration time=60-120s
V,R mag>=24 integration time180s
These integration times should suffice for doing a direct acquisition in case of clear
conditions, darktime and usual seeing. However, in case of very faint objects, the blind offset
could be the best solution as it could shorten the acquisition overheads.
See Sect 4 about the imaging mode that provides updated information about the AGCCD
and the imaging mode facility.
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Figure 6: The combined efficiency of the two dichroic beam splitters. In blue: reflection
on dichroic 1; in orange: transmission through dichroic 1 and reflection on dichroic 2; in red: transmission through dichroics 1 & 2.
2.2.1.5 The dichroic box
Light is split and distributed to the three arms by two highly efficient dichroic beam splitters.
These are the first optical elements encountered by the science light. The first dichroic at an
incidence angle of 15˚ reflects more than 98% of the light between 350 and 543 nm and
transmits ~95% of the light between 600 and 2300 nm. The second dichroic, also at 15˚
incidence, has a reflectivity above 98% between 535 nm and 985 nm and transmits more
than 96% of the light between 1045 and 2300 nm. The combined efficiency of the two
dichroics is shown in Fig. 6: it is well above 90% over most of the spectral range.
2.2.1.6 The flexure compensation tip-tilt mirrors
Light reflected and/or transmitted by the two dichroics reaches, in each arm, a folding mirror
mounted on piezo tip-tilt mount. These mirrors are used to fold the beam and correct for
backbone flexure to keep the relative alignment of the three spectrograph slits within less
than 0.02” at any position of the instrument. They also compensate for shifts due to
atmospheric differential refraction between the telescope tracking wavelength (fixed at 470
nm for all SLIT X-shooter observations) and the undeviated wavelength of the two ADCs (for
UVB and VIS arms) and the middle of the atmospheric dispersion range for the NIR arm.
In case of IFU observations, one can select the telescope tracking wavelength.
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2.2.1.7 The Focal Reducer and Atmospheric Dispersion Correctors
Both UVB and VIS pre-slit arms contain a focal reducer and an ADC. These focal reducerADCs consist of two doublets cemented onto two counter rotating double prisms. The focal
reducers bring the focal ratio from f/13.41 to ~f/6.5 and provide a measured plate scale at the
entrance slit of the spectrographs of 3.91”/mm in the UVB and 3.82”/mm in the VIS.
The ADCs compensate for atmospheric dispersion in order to minimize slit losses and allow
orienting the slit to any position angle on the sky up to a zenith distance of 60˚. The zerodeviation wavelengths are 405 and 633 nm for the UVB and the VIS ADCs respectively. In
the AUTO mode, their position is updated every 60s based on information taken from the
telescope database.
Unfortunately due to some problems affecting the ADCs, they have been disabled since
August 1st, 2012. See the following section for more information about the observations
without ADCs.
The NIR arm is not equipped with an ADC. The NIR arm tip-tilt mirror compensates for
atmospheric refraction between the telescope tracking wavelength (470 nm) and 1310 nm,
which corresponds to the middle of the atmospheric dispersion range for the NIR arm. This
means that this wavelength is kept at the center of the NIR slit. At a zenithal distance of 60°
the length of the spectrum dispersed by the atmosphere is 0.35”, so the extremes of the
spectrum can be displaced with respect to the center of the slit by up to 0.175”. If
measurement of absolute flux is an important issue, the slit should then be placed at
parallactic angle.
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2.2.2 ADCs problems and disabled ADCs observing mode in SLIT and IFU
During March to July 2012 the ADCs (atmospheric dispersion correctors) for the UVB and
VIS arms in X-shooter have been occasionally failing. Unfortunately recently the rate of such
failures has increased until being daily, leading sometimes to data taken in sub-optimal
instrument configuration, which needs to be taken into account when reducing and analyzing
such observations.
There is an ongoing investigation to find the cause for the ADCs' misbehavior, but it is
unlikely that the situation is back to normal for the next few months. Incorrect position of
ADCs might lead to slit losses worse than if they are not used. Consequently, the ADCs were
temporarily disabled (set at the non deviation position as in the IFU mode) on August 1st. A
major intervention to fix the problem is currently under investigation.
In the following pages, you will find useful information characterizing the observations without
working ADCs to compensate the atmospheric dispersion in UVB and VIS arms.
Measurements were performed in the various orders of the UVB/VIS arms, some
comparisons are performed and the average, the min/max values and the standard deviation
are provided. The slits used are 1.0”, 0.9”, 0.9” in the UVB, VIS, and NIR arms respectively.
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Atmospheric dispersion effect (no ADCs) on the position of the spectrum inside different orders
depending on the airmass and the arm (UVB:top, VIS: middle, NIR:bottom). The wavelength is in
Angstroms.
UVB arm
VIS arm
NIR arm
a) Atmospheric dispersion effect on the XSHOOTER spectra without ADCs
The tracking in XSHOOTER is by default 470nm, and
The dispersion effect of the atmosphere on XSHOOTER spectra depends on the tracking
wavelength used (by default 470nm).
Therefore the current effect is shown in the following plots for the UVB, VIS, and NIR arms.
ESO, Karl-Schwarzschild-Str. 2, 85748 Garching bei München, Germany
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Arm
Average
range
std
UVB
0.88
0.85-0.92
0.01
VIS
0.94
0.92-0.97
0.01
Arm, slit angle
Average
range
std
UVB parallactic
0.88
0.46-1.0
0.12
UVB perpendicular
0.46
0.10-1.0
0.33
VIS parallactic
0.92
0.86-1.0
0.03
VIS perpendicular
0.77
0.47-1.0
0.18
As consequences, in stare mode (object centered in the slit):
-if the observation is conducted at airmass 1.2 with the slit angle at parallactic angle, then the
drift between the blue and red order spectrum will be of ~1.6” in the UVB arm, ~0.6” in the
VIS arm, and ~0.2” in the NIR arm.
--if the observation is conducted at airmass 1.6 with the slit angle at parallactic angle, then
the drift between the blue and red order spectrum will be of ~3.5” in the UVB arm, ~0.8” in the VIS arm, and ~0.3” in the NIR arm.
Such kind of drifts is important to take into account in case of nodding observations to avoid
too many flux losses even with the slit at the parallactic angle.
It is again more important if the slit angle is different than the parallactic angle.
b) Comparison of ADCs efficiency at different slit angle.
The measure was performed at relatively high airmass (AM=1.8) and compares the flux
between the slit position parallactic+90 degrees and parallactic angles (ratio flux
perpendicular/flux parallactic). The average value corresponds to the average of
measurements for each order, the range gives the min/max values of the ratio and the
standard deviation (std) is given.
Stare mode, AM=1.8
With ADCs ratio perpendicular/parallactic
c) Comparison of observations with/without ADCs
There are 2 sets of measurements comparing the efficiency of observations with/without the
ADCs for the slit angle at parallactic angle or perpendicular to it:
One in stare mode at airmass =1.8 that can be compared to the subsection b.
One in nodding mode at airmass=1.35.
Stare mode, AM=1.8
Ratios no ADCs/with ADCs
ESO, Karl-Schwarzschild-Str. 2, 85748 Garching bei München, Germany
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Arm, slit angle
Average
range
std
UVB parallactic
0.87
0.87-0.9
0.01
UVB perpendicular
0.82
0.56-1.0
0.15
VIS parallactic
0.88
0.82-0.9
0.02
VIS perpendicular
0.81
0.66-0.99
0.11
Arm
airmass
Ratio 45/parall
Ratio 90/parall
UVB
1.10
0.98
0.83
UVB
1.51
0.84
0.63
UVB
2.20
0.31
0.18
VIS
1.10
0.87
0.80
VIS
1.51
0.92
0.72
VIS
2.20
0.63
0.31
On those plots for observations at 90 degrees of the parallactic angle, slits of 0.4” in the UVBarm (top), 0.5” in the VISarm (bottom) and a seeing of 0.8” have been considered.
Nodding mode, AM=1.35
Ratios no ADCs/with ADCs
The measurements were performed on short integration times and if possible in stable
conditions of the seeing.
d) Efficiency of observations without ADCs at different given slit angles
and airmasses
In this subsection a summary is presented first, a modeling for narrower slits is shown in
second, and finally the detailed measurements corresponding to the first part are provided.
We consider here the ratios of the observation at 45 degrees or 90 degrees of the parallactic
angle to the parallactic angle for different airmasses.
Summary:
The similar information was computed theoretically and is shown in the following plots.
ESO, Karl-Schwarzschild-Str. 2, 85748 Garching bei München, Germany
Doc:
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Date
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VLT-MAN-ESO-14650-4942
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30.06.2014
30 of 156
Arm
airmass
Type of ratio
average
range
std
UVB
1.10
45/parall
0.98
0.84-1.0
0.19
UVB
1.10
90/parall
0.83
0.74-1.0
0.15
UVB
1.51
45/parall
0.84
0.56-1.0
0.13
UVB
1.51
90/parall
0.63
0.25-1.0
0.26
UVB
2.20
45/parall
0.31
0.05-0.64
0.20
UVB
2.20
90/parall
0.18
0.04-0.23
0.06
VIS
1.10
45/parall
0.87
0.83-0.94
0.03
VIS
1.10
90/parall
0.80
0.75-0.92
0.04
VIS
1.51
45/parall
0.92
0.87-1.0
0.04
VIS
1.51
90/parall
0.72
0.47-1.0
0.17
VIS
2.20
45/parall
0.63
0.37-0.83
0.16
VIS
2.20
90/parall
0.31
0.28-0.34
0.02
Arm
Average
range
std
UVB
0.96
0.66-1.47
0.25
VIS
0.85
0.74-1.00
0.09
Arm
Average
range
std
UVB
1.04
0.54-1.89
0.45
VIS
0.79
0.62-1.08
0.14
e) Efficiency of observations without ADCs at given airmass and slit angle
but with different tracking wavelength
Up to now only in IFU mode, the user can choose the tracking wavelength. This option will be
considered for the SLIT mode as well. In the following tables we compare the flux ratios other
the orders for the observations at 470nm (default tracking wavelength) with respect to the
observation at another wavelength. The observations were performed without ADCs, in
nodding mode at AM=1.35.
If the user chooses the tracking wavelength equals to 600nm instead of 470nm
For the UVB arm, the ratio is higher in blue orders (~1.4) with the 470nm tracking wavelength
and lower in the red orders (~0.7) compared to the 600nm tracking wavelength. This is the
same evolution for the VIS arm.
Same measurements but with the tracking wavelength at 850nm instead of 470nm
For the UVB arm, the ratio is higher in blue orders (~1.9) with the 470nm tracking wavelength
and lower in the red orders (~0.6) compared to the 850nm tracking wavelength. This is the
same evolution for the VIS arm.
ESO, Karl-Schwarzschild-Str. 2, 85748 Garching bei München, Germany
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