SPACE TELESCOPE SCIENCE INSTITUTE Operated for NASA by AURA The On-Orbit Performance of the Cosmic Origins Spectrograph Alessandra Aloisi (for the COS STScI team and the COS IDT) 21 July 2010
Mar 22, 2016
SPACETELESCOPESCIENCEINSTITUTE
Operated for NASA by AURA
The On-Orbit Performance of the Cosmic Origins Spectrograph
Alessandra Aloisi(for the COS STScI team and the COS IDT)
21 July 2010
Aloisi – 21 July 2010 Slide 1 of 15
Highlights
Quick Overview of the Instrument Sensitivities and their Time Dependence Gain Sag of FUV Detector On-orbit Line Spread Function Darks and their Evolution Flat Fields Wavelength Calibration COS-to-FGS Alignment COS Documentation
Instrument Overview
Aloisi – 21 July 2010 Slide 2 of 15
FUV spectroscopy: R = 3,000 - 20,000 [1150 - 2050 Å] NUV spectroscopy: R = 2,000 - 20,000 [1700 - 3200 Å] Some NUV imaging capabilities (mostly used for TA)
Aloisi – 21 July 2010 Slide 3 of 15
COS Sensitivity
Superb in FUV Comparable to STIS in NUV NUV sensitivity in G225M & G285M is as expected at launch from grating degradation Within 20% of ground values
New COS & STIS on-orbit sensitivities
Aloisi – 21 July 2010 Slide 4 of 15
COS has Sensitivity down to the Lyman Limit
McCandliss et al. 2009 ApJL, submitted
G140L ModeR ~ 2,500
McCandliss et al. 2010, ApJ, 709, L183 Mode currently
supported in Cycle 18 (G140L @ 1280 Å Segment B)
Additional F & characterization in Cycle 17 Calibration program 12081
Two new G130M settings at R ~ 5,000 (1055 Å & 1096 Å)
S. Osterman’s talk
COS sensitivity is regularly monitored as part of Cycle 17 & 18 Calibration Programs
NUV Sensitivities - gratings keep following pre-launch trends Bare-Al gratings G225M and G285M continue to show grating-dependent
but wavelength-independent decline on orbit at a rate similar or higher than pre-launch rates (up to ~ 10% per year )
MgF2-coated gratings G185M and G230L continue to be stable FUV Sensitivities – non localized wavelength-dependent decline up to
~ 12% per year at longer λ similar for all gratings suggestive of CsI photocathode aging (with each segment of the XDL detector having different rates)
COS TDS trends already included in ETC (v18.2) and in CALCOS
See R. Osten’s talk fore more details Aloisi – 21 July 2010
Slide 5 of 15
Time Dependence of COS Sensitivity
Gain Sag of COS FUV Detector
FUV cumulative images and maps of pulse height distributions as a function of time now available (fully implemented into pipeline for OPUS build 2010.4)
Evidence of detector gain sag (localized effect) Gain after launch higher than on the ground
HV lowered during SMOV Evolution of gain sag faster than expected
Consistent with on-orbit gas contamination around launch time
We are probably re-scrubbing the detector on-orbit Gain sag is already slowing down in most heavily
exposed areas Very localized loss up to a few % in most heavily
affected areas (geocoronal Lyα) In the process to identify mitigative actions
See D. Sahnow’s poster C2Aloisi – 21 July 2010
Slide 6 of 15
Aloisi – 21 July 2010 Slide 7 of 15
COS On-Orbit FUV LSF
FUV spectral resolution not quite as expected due to MFWFEs
See P. Ghavamian’s poster C5
LSF power is distributed from core to wings
Effect is wavelength dependent,
being most extreme in the FUV
R ~ 16,000 vs 20,000 @ 1300 Å
— 1150 Å (G130M)— 1450 Å (G130M)— 1750 Å (G160M)— Gaussian 6.5 pixel FWHM (no MFWFEs)
Aloisi – 21 July 2010 Slide 8 of 15
COS On-Orbit NUV LSF
Contribution of MFWFE
present also in NUV
Almost negligible longward of 2500 Å
NUV spectral resolution at > 2500 Å as expected
Aloisi – 21 July 2010 Slide 9 of 15
COS FUV Darks
FUV dark rate away from SAA measured during SMOV was as expected from pre-launch estimates, i.e. ~ 1.5-2 x 10-6 cts/sec/pixel, when pulse-height filtering (4-30) is applied
FUV dark rate up to ~ 30 times higher close to the SAA boundary (before SAA model adjustment in May 2010)
Several weak features found for Segment B (Segment A is featureless)
TIME-TAG: most of the features removed by pulse-height filtering (4-30) during ground processing (already implemented into CALCOS)
ACCUM: suspect regions flagged; features too weak to affect very bright objects observed in this mode
FUV dark rate monitored weekly No evolution with time
See D. Sahnow’s poster C2
G130M @ 1309 Å (Segment B)
Aloisi – 21 July 2010 Slide 10 of 15
COS NUV Darks
NUV dark rate away from SAA measured during SMOV was 6x10-5 cts/sec/pixel, significantly below prelaunch predictions (~ 20x10-5 cts/sec/pixel)
NUV dark rate up to ~ 15 times higher close to the SAA boundary until SAA model adjustment in May 2010 (no long-term phosphorescence in MAMA window after SAA passage)
NUV dark exposures relatively featureless NUV dark rate monitored weekly
Approximately linear increase with time, once temperature fluctuations are taken into account
Currently slightly higher than prelaunch estimates, i.e. ~ 35x10-5 cts/sec/pixel
Still several times lower than current STIS NUV MAMA values
See W. Zheng’s poster S1
Aloisi – 21 July 2010 Slide 11 of 15
COS NUV Flat
NUV on-orbit flat (internal lamp) confirmed consistency with ground flat at higher S/N (alignment better than 1 pixel)
NUV flat field currently used Combination of ground and on-orbit flats Includes on-orbit vignetting (depression up to 15-
20%) in first ~ 200 pixels Vignetting currently implemented separately for
M (G185M, G225M, G285M) and L (G230L) gratings
NUV flat field correction currently applied in CALCOS
NUV flat allows to achieve S/N > 100 per resel when combined with 4 different FP-POS positions with high S/N data
NUV ground flat
NUV flat for on-orbit data
Aloisi – 21 July 2010 Slide 12 of 15
COS FUV Flat
Vallerga et al. 2001, SPIE 4498, 141
Sum of the 8 rows indicated above
“Berkeley” Flat of Segment A (whole detector, no grid wires)
2D ground flats (Berkeley + TV03) still to be validated with on-orbit data
No 2D on-orbit flat with adequate S/N currently available
FUV flat field correction currently not applied in CALCOS
CALCOS currently omits grid wires and other defects when creating x1dsum files
1D iterative technique combined with 4 different FP-POS positions looks promising and allows to achieve S/N > 100 per resel with high S/N data
Implementation of 1D flats on extracted spectra underway
New 1D flats for all FUV gratings to be obtained in Cycle 17 Calibration program 12086
See T. Ake’s talk for more details on 1D flats
Aloisi – 21 July 2010 Slide 13 of 15
COS On-Orbit Wavelength Calibration
TV03 demonstrated that dispersion solutions of PSA and WCA differ from each other
PSA/WCA wavelength dispersion solutions obtained in TV03 TV06 demonstrated that dispersion solution difference between
WCA and PSA depends on optical alignment SMOV data used to:
infer new on-orbit wavecal templates measure on-orbit zeropoints compared to ground calibration
New CALCOS reference files that update wavelength calibration for most settings delivered in January 2010 (G185M still to be completed)
On-orbit wavelength scales for most settings meet requirements 15 km/s for the M gratings 150 km/s (175 km/s) for G140L (G230L) gratings In a few cases, extra offsets of up to 10 pixels in FUV appear in
part of the spectrum (nature & frequency of such localized distortions still under investigation)
Cycle 17 monitoring indicates that PSA to WCA on-orbit offsets are stable with time
See C. Oliveira’s poster C4
Aloisi – 21 July 2010 Slide 14 of 15
COS-to-FGS Alignment and TA COS-to-FGS alignment optimized during
SMOV and Cycle 17; SIAF tables updated Figure includes centering slews in all TA
sequences of GTO/GO programs since update of SIAF table in March 2010
Alignment now appears to be accurate to within ~ 0.1”– Initial pointing now limited by accuracy of
GSC2 catalogue (~ 0.2”) Reconsidered the need for an ACQ/Search at
start of each visit for Cycle 18 Phase II– Change will save time, especially for
acquisitions of very faint targets– For faint targets, ACQ/Search can have
problems with variable background– Coordinates need to be accurate within 0.4”
COS Documentation
On-orbit COS performance summarized in 10 published ISRs and 6 soon-to-be-published ISRs:
http://www.stsci.edu/hst/cos/documents/isrs
Preliminary SMOV updates included into the Instrument Handbook for Cycle 18 (published in January 2010): http://www.stsci.edu/hst/cos/documents/handbooks/current/cos_cover.html
SMOV and Cycle 17 Calibration updates currently implemented into the Instrument Handbook for Cycle 19 (for publication in December 2010)
Visit our web pages at: http://www.stsci.edu/hst/cos
Aloisi – 21 July 2010 Slide 15 of 15