Techniques d'observation spectroscopique d'astéroïdes

Techniques d'observation spectroscopique d'astéroïdes Techniques d'observation spectroscopique d'astéroïdes

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46 CHAPTER 2. WHY SPECTROSCOPY? tel-00785991, version 1 - 7 Feb 2013 Figure 2.2: The atmospheric transmission above Mauna Kea for the wavelength ranges 0.9 - 2.7 µm with a water vapor column of 1.6 mm and an air mass of 1 (Source: http://www.gemini.edu/?q=node/10789). several other components into the instrument called spectrometer. Usually, the designs of spectrometers incorporate the following basic components: an entrance slit to reduce the overlap between adjacent wavelengths and to reduce the background noise, collimators to produce parallel beams of light, a dispersive element, a focusing element to produce focused images of the slit for different wavelengths of the spectrum, and a detector. 2.2 Spectroscopy and atmospheric transparency The observation of celestial bodies using different types of ground-based telescopes is possible in the regions of electromagnetic spectrum for which the atmosphere is transparent. There are two spectral windows which allow the observation: the optical (V) up to the mid-infrared(the near-infrared 0.8 - 2.5 µm interval is denoted as NIR) and the radio one. The X-rays and ultraviolet wavelengths are blocked due to absorption by ozone and oxygen, while the far infrared radiation is blocked mainly due to absorption by water and carbon dioxide. While in the optical wavelength region the atmosphere is almost completely transparent, in the near-infrared there are absorption bands of water vapors making some regions like 1.4-1.5 µm and 1.8-2.0 µm poorly transparent (Fig. 2.2). Because of the effects of the atmosphere, observations with space telescopes, such as the Hubble and Spitzer telescopes, are very valuable. Another important difference between the V and NIR spectral intervals is the fact that the sky is brighter in the NIR region. For example in the J, H, K filters 1 the estimated sky background has 15.7, 13.6, respectively 13 mag/arcsec 2 . Additional, important variations of the sky background could be observed in the intervals of tens of arc minutes of the sky. 1 Wide band filters centered on 1.25 µm (J), 1.65 µm (H), 2.2 µm (K)

CHAPTER 2. WHY SPECTROSCOPY? 47 These issues in the NIR part require additional observing techniques and processing methods (described in Chapter 4) comparing to observation in the V part of the spectrum. 2.3 A simple application tel-00785991, version 1 - 7 Feb 2013 Bellow is described a simple application to exemplify the basic method for obtaining spectra of celestial bodies. It concerns an emission spectrum studied in the V region using a small telescope. Additional details regarding this spectral observation can be found in Popescu et al. [2012a]. An easy way to obtain spectra of celestial bodies is to use a prism or a transmission grating in front of a telescope objective. Depending on the equipment used, the sky quality on the observing moment and data reduction procedures, the limiting magnitude could be pushed up to V = 15 in low resolution mode, with a small telescope (principal mirror diameter below 50 cm). Together with my colleagues, I carried out observations with telescopes having the diameter of principal mirror between 200-300 mm and a diffraction grating having 100 lines/mm [Popescu et al., 2012a]. Since promising results were obtained both for stars and for the quasar 3C273 we took the challenge to observe the quasar PG1634+706 that has and apparent magnitude V=14.7. The purpose was to identify the emission lines in its spectrum and to calculate their redshift. For this run we used a Celestron C8-NGT telescope, which is a Newtonian type having the primary mirror of 200 mm and a focal length of 1,000 mm, which means a focal ratio f/5. It is used on a AS-GT (CG-5 GoTo) equatorial mount allowing automated tracking of the object. For image recording we used An ATIK 314L+ CCD (charge coupled device) camera having 1.45 Megapixels (a matrix of 1391x1039 pixels), each pixel being a square - 6.45 x 6.45 µm (chip size - 8.98 x 6.71mm). This camera has a resolution of 16 bits. The spectrum of PG1634+706 was obtained using a Star Analyser 100 - a high efficiency 100 lines/mm transmission diffraction grating, blazed in the first order. It was mounted in a standard 1.25 inch diameter threaded cell which is compatible with the telescope and CCD camera. A rough calibration of the system can be estimated according to the designer formula adapted to our system (Eq. 2.6): Dispersion estim [ nm 6.45 ]= (2.6) pixel d[cm] where d is the distance between grating and CCD. The optical design allowed a resolution around 1.5nm. A precise calibration was made using known lines identified in the spectrum of a bright star. The software used for data acquisition was Artemis Capture. The observations were carried out at 2011-08-05.089 (UT) in a low light pollution area (Vălenii de Munte - România). The object has the equatorial coordinates RA = 16 h 34 m 29 s and DEC = +70 o 31 ′ 32”. At the observing moment the object had an air mass of 1.17. The final

CHAPTER 2. WHY SPECTROSCOPY? 47<br />

These issues in the NIR part require additional observing techniques and processing methods<br />

(described in Chapter 4) comparing to observation in the V part of the spectrum.<br />

2.3 A simple application<br />

tel-00785991, version 1 - 7 Feb 2013<br />

Bellow is described a simple application to exemplify the basic method for obtaining spectra<br />

of celestial bodies. It concerns an emission spectrum studied in the V region using a small<br />

telescope. Additional details regarding this spectral observation can be found in Popescu et al.<br />

[2012a].<br />

An easy way to obtain spectra of celestial bodies is to use a prism or a transmission grating<br />

in front of a telescope objective. Depending on the equipment used, the sky quality on the<br />

observing moment and data reduction procedures, the limiting magnitude could be pushed up<br />

to V = 15 in low resolution mode, with a small telescope (principal mirror diameter below 50<br />

cm).<br />

Together with my colleagues, I carried out observations with telescopes having the diameter<br />

of principal mirror between 200-300 mm and a diffraction grating having 100 lines/mm<br />

[Popescu et al., 2012a]. Since promising results were obtained both for stars and for the quasar<br />

3C273 we took the challenge to observe the quasar PG1634+706 that has and apparent magnitude<br />

V=14.7. The purpose was to identify the emission lines in its spectrum and to calculate<br />

their redshift. For this run we used a Celestron C8-NGT telescope, which is a Newtonian type<br />

having the primary mirror of 200 mm and a focal length of 1,000 mm, which means a focal<br />

ratio f/5. It is used on a AS-GT (CG-5 GoTo) equatorial mount allowing automated tracking<br />

of the object. For image recording we used An ATIK 314L+ CCD (charge coupled device)<br />

camera having 1.45 Megapixels (a matrix of 1391x1039 pixels), each pixel being a square -<br />

6.45 x 6.45 µm (chip size - 8.98 x 6.71mm). This camera has a resolution of 16 bits.<br />

The spectrum of PG1634+706 was obtained using a Star Analyser 100 - a high efficiency<br />

100 lines/mm transmission diffraction grating, blazed in the first order. It was mounted in a<br />

standard 1.25 inch diameter threaded cell which is compatible with the telescope and CCD<br />

camera. A rough calibration of the system can be estimated according to the designer formula<br />

adapted to our system (Eq. 2.6):<br />

Dispersion estim [ nm 6.45<br />

]= (2.6)<br />

pixel d[cm]<br />

where d is the distance between grating and CCD. The optical design allowed a resolution<br />

around 1.5nm. A precise calibration was made using known lines identified in the spectrum of<br />

a bright star. The software used for data acquisition was Artemis Capture.<br />

The observations were carried out at 2011-08-05.089 (UT) in a low light pollution area<br />

(Vălenii de Munte - România). The object has the equatorial coordinates RA = 16 h 34 m 29 s and<br />

DEC = +70 o 31 ′ 32”. At the observing moment the object had an air mass of 1.17. The final

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