characterization of the post-launch line spread function of cos

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Characterization of the Post- Launch Line Spread Function of COS Parviz Ghavamian A. Aloisi, C. Proffitt, D. Lennon, G. Hartig, G. Kriss, C. Oliveira, D. Massa, T. Keyes (STScI) T. Delker (Ball Aerospace) S. Osterman (Colorado)

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Characterization of the Post-Launch Line Spread Function of COS. Parviz Ghavamian A. Aloisi, C. Proffitt, D. Lennon, G. Hartig, G. Kriss, C. Oliveira, D. Massa, T. Keyes (STScI) T. Delker (Ball Aerospace) S. Osterman (Colorado). The COS LSF: Ground Tests. Gaussian 6.5 pixels FWHM. - PowerPoint PPT Presentation

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Page 1: Characterization of the Post-Launch Line Spread Function of COS

Characterization of the Post-Launch Line Spread Function of COS

Characterization of the Post-Launch Line Spread Function of COS

Parviz Ghavamian

A. Aloisi, C. Proffitt, D. Lennon, G. Hartig, G. Kriss, C. Oliveira, D. Massa, T. Keyes

(STScI)

T. Delker (Ball Aerospace)S. Osterman (Colorado)

Parviz Ghavamian

A. Aloisi, C. Proffitt, D. Lennon, G. Hartig, G. Kriss, C. Oliveira, D. Massa, T. Keyes

(STScI)

T. Delker (Ball Aerospace)S. Osterman (Colorado)

Page 2: Characterization of the Post-Launch Line Spread Function of COS

The COS LSF: Ground Tests The COS LSF: Ground Tests

• During TV03/TV06, light from PtNe lamp was passed into COS after passing through RAS/Cal stimulus, which mimicked low-frequency errors from HST OTA (spherical aberration, astigmatism, coma...)

• COS gratings correct for these LFEs, designed to produce R ~ 20,000 across 80% of bandpass in the resulting M-mode spectra (FUV and NUV)

• The LSF profile in the FUV was well described by Gaussian shape during TV03/TV06

• In NUV, LSF profile has non-Gaussian wings due to MAMA detector response; optical models give FWHM ~ 2.5 pixels

• During TV03/TV06, light from PtNe lamp was passed into COS after passing through RAS/Cal stimulus, which mimicked low-frequency errors from HST OTA (spherical aberration, astigmatism, coma...)

• COS gratings correct for these LFEs, designed to produce R ~ 20,000 across 80% of bandpass in the resulting M-mode spectra (FUV and NUV)

• The LSF profile in the FUV was well described by Gaussian shape during TV03/TV06

• In NUV, LSF profile has non-Gaussian wings due to MAMA detector response; optical models give FWHM ~ 2.5 pixels

GaussianGaussian6.5 pixels FWHM6.5 pixels FWHM

Page 3: Characterization of the Post-Launch Line Spread Function of COS

COS LSF: Effect of Mid-Frequency ErrorsCOS LSF: Effect of Mid-Frequency Errors

• During SMOV, the shape of the on-orbit COS LSF was found to differ from the profile in ground testing, due to the presence of zonal (polishing) errors on primary and secondary HST mirrors

• Zonal errors introduce mid-frequency errors (~18 nm) into beam entering COS; not included in RAS/Cal testing

• Result is a lowered, broadened core and broad non-Gaussian wings on LSF

• Mid-freq. WFEs are strongest at shortest wavelengths of COS (~1150 Å), dimin-ishing with increasing wavelength, and becoming negligible beyond ~ 2500 Å

• During SMOV, the shape of the on-orbit COS LSF was found to differ from the profile in ground testing, due to the presence of zonal (polishing) errors on primary and secondary HST mirrors

• Zonal errors introduce mid-frequency errors (~18 nm) into beam entering COS; not included in RAS/Cal testing

• Result is a lowered, broadened core and broad non-Gaussian wings on LSF

• Mid-freq. WFEs are strongest at shortest wavelengths of COS (~1150 Å), dimin-ishing with increasing wavelength, and becoming negligible beyond ~ 2500 Å

33

COS/NUV Model LSF: Mid-Frequency WFEs COS/NUV Model LSF: Mid-Frequency WFEs includedincluded

Krist & Burrows (1995)Krist & Burrows (1995)

Fraction of flux falling outside of FWHMFraction of flux falling outside of FWHM

LSF model G130M G160M G185M G225M G285M

no WFEs 24% 24% 36% 37% 39%

with WFEs (wav-avg)

41% 37% 51% 49% 47%

Page 4: Characterization of the Post-Launch Line Spread Function of COS

Example: Impact of Mid-Frequency Errors on SpectraExample: Impact of Mid-Frequency Errors on Spectra

• FUV: Sk 155 in the SMC (O9 Ib, V=12.4), observed during SMOV with G130M, G160M gratings

• E140H STIS echelle spectra exist (R ~ 114,000; E0.2x0.09) on archive and as part of Cycle 17 calibration data

• Wings on LSF cause:

1. Significant filling-in of saturated absorption features

2. Merging of narrow absorption lines into wings of nearby saturated absorption features

• Model the COS spectrum by convolving STIS E140H spectrum with model LSFs

• FUV: Sk 155 in the SMC (O9 Ib, V=12.4), observed during SMOV with G130M, G160M gratings

• E140H STIS echelle spectra exist (R ~ 114,000; E0.2x0.09) on archive and as part of Cycle 17 calibration data

• Wings on LSF cause:

1. Significant filling-in of saturated absorption features

2. Merging of narrow absorption lines into wings of nearby saturated absorption features

• Model the COS spectrum by convolving STIS E140H spectrum with model LSFs

Page 5: Characterization of the Post-Launch Line Spread Function of COS

Application of COS LSF modelsApplication of COS LSF models

Page 6: Characterization of the Post-Launch Line Spread Function of COS

Impact on COS ScienceImpact on COS Science

• Programs using full resolution of FUV G130M, G160M and NUV G185M:

1. Close together lines harder to isolate

2. Weak, narrow absorption features (b < 35 km s-1) more difficult to detect at a given S/N; lower contrast between core and wings

3. Analysis of saturated absorption lines will require full consideration of LSF

• Programs minimally affected are:

1. Those observing broad lines (b > 35 km s-1)

2. SED and continuum flux measurements

3. G140L observations, since they typically are done for SED measurements, or to observe sources with line widths larger than instrumental resolution

• Programs using full resolution of FUV G130M, G160M and NUV G185M:

1. Close together lines harder to isolate

2. Weak, narrow absorption features (b < 35 km s-1) more difficult to detect at a given S/N; lower contrast between core and wings

3. Analysis of saturated absorption lines will require full consideration of LSF

• Programs minimally affected are:

1. Those observing broad lines (b > 35 km s-1)

2. SED and continuum flux measurements

3. G140L observations, since they typically are done for SED measurements, or to observe sources with line widths larger than instrumental resolution

33σσ Limiting Equivalent Widths Limiting Equivalent Widths(assumes S/N=10 pixe(assumes S/N=10 pixell-1-1 in continuum) in continuum)

dotted: with WFEsdotted: with WFEssolid: no WFEssolid: no WFEs

Rough calculation; result may be improved Rough calculation; result may be improved with flux-weighted extraction, etc.with flux-weighted extraction, etc.

Page 7: Characterization of the Post-Launch Line Spread Function of COS

• http://www.stsci.edu/hst/cos/performance/spectral_resolution• http://www.stsci.edu/hst/cos/performance/spectral_resolution