Characterization of the Post-Launch Line Spread Function of COS - PowerPoint PPT Presentation

1 / 7
About This Presentation
Title:

Characterization of the Post-Launch Line Spread Function of COS

Description:

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) – PowerPoint PPT presentation

Number of Views:40
Avg rating:3.0/5.0
Slides: 8
Provided by: sts57
Learn more at: https://www.stsci.edu
Category:

less

Transcript and Presenter's Notes

Title: Characterization of the Post-Launch Line Spread Function of COS


1
(No Transcript)
2
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

Gaussian 6.5 pixels FWHM
3
COS 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

LSF model G130M G160M G185M G225M G285M
no WFEs 24 24 36 37 39
with WFEs (wav-avg) 41 37 51 49 47
4
Example Impact of Mid-Frequency Errors on Spectra
  • FUV Sk 155 in the SMC (O9 Ib, V12.4), 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
  • Significant filling-in of saturated absorption
    features
  • Merging of narrow absorption lines into wings of
    nearby saturated absorption features
  • Model the COS spectrum by convolving STIS E140H
    spectrum with model LSFs

5
Application of COS LSF models
6
Impact on COS Science
  • Programs using full resolution of FUV G130M,
    G160M and NUV G185M
  • Close together lines harder to isolate
  • Weak, narrow absorption features (b lt 35 km s-1)
    more difficult to detect at a given S/N
    lower contrast between core and wings
  • Analysis of saturated absorption lines will
    require full consideration of LSF
  • Programs minimally affected are
  • Those observing broad lines (b gt 35 km s-1)
  • SED and continuum flux measurements
  • G140L observations, since they typically are done
    for SED measurements, or to observe sources with
    line widths larger than instrumental resolution

3s Limiting Equivalent Widths (assumes S/N10
pixel-1 in continuum)
Rough calculation result may be improved with
flux-weighted extraction, etc.
7
  • http//www.stsci.edu/hst/cos/performanc
    e/spectral_resolution
Write a Comment
User Comments (0)
About PowerShow.com