background information for users of stis charles r. proffitt

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Background information for users of STIS Charles R. Proffitt

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Page 1: Background information for users of STIS Charles R. Proffitt

Background information for users of STIS

Charles R. Proffitt

Page 2: Background information for users of STIS Charles R. Proffitt

STIS Presentation 2

Outline of Topics

More on Bright and Faint limits with STIS Calibration Lamps Wavelength Calibration Target Acquisitions CCD Operations and Characteristics MAMA Characteristics Time Resolved Observations Observing Overheads Summary of Data Products Spatial Undersampling of STIS Data A few selected data artifacts

Page 3: Background information for users of STIS Charles R. Proffitt

STIS Presentation 3

Bright Object Limits

STIS IHB gives tables of worst-case limiting magnitude as a function of grating and source spectrum.

Normalization can vary enormously, depending on grating, aperture, source SED, reddening, etc.

Cool stars especially tricky NUV flux very sensitive to all stellar parameters esp. metallicity FUV flux often dominated by chromospheric emission

Not included in Kurucz or other photospheric models Strongly affected by stellar activity

Epsilon Eri: Kurucz model vs. observed spectrum

Page 4: Background information for users of STIS Charles R. Proffitt

STIS Presentation 4

STIS Spectroscopic BOP Limits

Limit for CENWAVE with highest countrate Assumes slitless 1st order; 0.2X0.2 for echelles

Page 5: Background information for users of STIS Charles R. Proffitt

STIS Presentation 5

Bright and Faint Limits - example

Example: bright and faint limits for an A0 star Faint limit defined as S/N=10 in one hour For CCD bright limit will saturate CCD in 0.1 s

@gain=4 For MAMA bright limit determined by local or global

BOP limits

Page 6: Background information for users of STIS Charles R. Proffitt

STIS Presentation 6

Approximate Bright and Faint Limiting Mag for A0V star at a single wavelength using typical clear apertures

(don’t take exact numbers too seriously)

Grating Wavelength Mag to give S/N=10 in 1 h

Bright limit mag

delta

G750L 7000 20.8 1.1 19.7

G750M 19.0 -1.1 20.1

G430L 5500 20.8 1.5 19.3

G430M 18.4 -1.3 19.7

G230LB 3000 18.3 -1.6 19.9

G230MB 15.4 -4.4 19.8

G230L 2600 18.4 10.4 8.0

G230M 14.4 6.5 7.9

G140L 1350 16.7 8.1 8.6

G140M 13.4 5.8 7.6

E230M 2700 13.2 6.6 6.6

E230H 11.6 5.1 6.5

E140M 1400 10.7 4.5 6.2

E140H 1350 9.8 4.0 5.8

NUV-PRISM 2300 20.6 11.9 8.7

Page 7: Background information for users of STIS Charles R. Proffitt

Calibration Lamps

Page 8: Background information for users of STIS Charles R. Proffitt

STIS Presentation 8

STIS Calibration Lamps Cal Insert Platform

Flatfielding lamps Tungsten (4 lamps) Krypton (130 - 170 nm) Deuterium (165 - 310 nm)

Echelle wavelength cal PtCr/Ne (LINE)

Cal insert mechanism (CIM) blocks external light & acts as additional external shutter

Hole in the Mirror (HITM) PtCr/Ne (HITM1/2)

1st order wavecals Locate aperture during

target ACQ

Page 9: Background information for users of STIS Charles R. Proffitt

STIS Presentation 9

Flat fielding Lamps

For small scale pixel-to-pixel flat fielding Krypton for FUV Deuterium for NUV Tungsten for CCD

Also used for IR fringe flats for G750L & G750M at > 7500 Å

Page 10: Background information for users of STIS Charles R. Proffitt

STIS Presentation 10

LINE and HITM lamps spectra

Low dispersion STIS spectra of LINE and HITM1 lamps

Page 11: Background information for users of STIS Charles R. Proffitt

Wavelength Calibration

Page 12: Background information for users of STIS Charles R. Proffitt

STIS Presentation 12

Wavelength calibration

Causes of Wavelength mis-alignments MSM positioning does not repeat exactly.

Projection of target/aperture shifts by a few pixels Thermal flexure of STIS bench can also shift

projection on detector by a couple of pixels Any drift/mis-centering of target in aperture will

cause corresponding shift in wavelength scale

Page 13: Background information for users of STIS Charles R. Proffitt

STIS Presentation 13

Wavelength calibration

Wavecal observations must be adjacent to science No intervening MSM motions because of non-repeatability

Recommend repeating wavecals every 40 minutes Slit-to-slit alignment & repeatability is good

No need to use same slit for science and wavecal For best alignment do ACQ/PEAK in small aperture

G430L Wavecal with 52X0.2 Aperture- Aperture bars allow offsets in cross dispersion direction to also be determined.

E140M Echelle Wavecal

Page 14: Background information for users of STIS Charles R. Proffitt

STIS Presentation 14

Wavelength calibration

AUTO-Wavecals meet needed requirements May not always schedule at most efficient time

AUTO-WAVECALS may be turned off for visit GO-WAVECALS may then be specified by observer No automatic enforcement of timing requirements for GO-

WAVECALs

Page 15: Background information for users of STIS Charles R. Proffitt

Target Acquisitions

Page 16: Background information for users of STIS Charles R. Proffitt

STIS Presentation 16

Need for STIS Onboard Acquistions

With GSC1 typical rms pointing errors were ~ 1” GSC2 is more accurate - 0.1”-0.3” accuracy expected

Many STIS apertures smaller than this

Pointing errors along dispersion direction, translate directly to wavelength errors

Basic STIS ACQ procedure desiged to centroid to ~1/5 CCD pixel or about 0.01”

Page 17: Background information for users of STIS Charles R. Proffitt

STIS Presentation 17

Target ACQ exposures

ACQ procedure does the following:1) Images target using 5”x5” subarray1 2) For point source ACQ, use flux weighted

centroid around brightest 3x3 checkbox (extend source algorithm also available).

3) Move spacecraft to put target at reference location on CCD

4) Re-image target1 & centroid again5) Image reference aperture using HITM1

lamp & locate aperture6) Move spacecraft to put target at center

of 0.2X0.2 reference aperture

First image

Second image

Lamp image of 0.2X0.2 aperture

1Each external ACQ image is actually made from 2 subarray images dithered by 3 pixels in x and y. They are shifted into alignment and then combined by taking the minimum value at

each pixel to eliminate cosmic ray hits and hot pixels.

Page 18: Background information for users of STIS Charles R. Proffitt

STIS Presentation 18

Selecting Target ACQ parameters

For point-source ACQ exposure S/N > 40:1 suggested More is better. If 40:1 SN needs < 0.1 s minimum exposure time,

see if 0.1 s exposure is unsaturated before switching to less sensitive setting.

But don’t let ACQ saturate. Allowing central pixel to overfill and bleed along columns may affect centroid in y direction.

If there are multiple close stars, be sure which one will be brightest in chosen ACQ filter.

Point source ACQ accurate to 1/5 pixel or 0.01” Diffuse source ACQ algorithms also available

• Larger checkboxes (up to 101x101 pixels or ~ 5”x5”)• Choice of flux Weighted or geometric centering

Page 19: Background information for users of STIS Charles R. Proffitt

STIS Presentation 19

ACQ/Peak exposures

Peakups recommended for apertures ≤ 0.1” in size

Do after ACQ Always done using CCD Peakups measure flux through

small aperture and move spacecraft to maximize flux

Need to peakup in both directions for small & short apertures (0.1X0.09)

Special procedures for 0.1X0.03 peakups

Peakups can use images or dispersed light

Accuracy ~ 5% of slit width

Page 20: Background information for users of STIS Charles R. Proffitt

STIS Presentation 20

Fixing Orientation on Sky

STIS long slit can be oriented to put extended or multiple targets in aperture

Orient in APT should be (degrees east of N) + 45

Usually 180 degree alternative is just as good

Page 21: Background information for users of STIS Charles R. Proffitt

STIS CCD Operations

Page 22: Background information for users of STIS Charles R. Proffitt

STIS Presentation 22

CCD Operations

STIS CCD Format

AMP D

Bias and dark correction Daily dark and bias observations and more intensive pre-and post

anneal observations used to create weekly superbias and superdark images used for OTFR pipeline reduction.

Super-bias image subtracted from science image. Serial and parallel overscan regions used to provide 2D correction

to bias levels of image. Superdark is subtracted from science image.

For side 2 data, superdark scaled for CCD housing temperature

CCD includes physical and virtual overscan regions.

Four amps, but most science uses AMP D.

Page 23: Background information for users of STIS Charles R. Proffitt

STIS Presentation 23

CCD Operations

Science data also divided by pixel-to-pixel flat field images based on data collected in yearly campaigns.

Some models also have low order flat field images to correct for vignetting.

Monthly anneals warm CCD from ~-85 to ~ +5 C Heals ~80% of transient hot pixels; Increasing numbers of permanent ones accumulate.

Page 24: Background information for users of STIS Charles R. Proffitt

STIS Presentation 24

CCD Dark Current & Hot Pixels Initial dark current low: median value ~0.0015 e-/s

Extrapolation predicts 0.009 cnts/pixel/s for Cycle 17 Increased over time due to radiation damage On side-2 no closed loop T control

CCD temperature & dark current varies with T Use housing temperature to scale dark current before dark subtraction

Inexact scaling is an additional source of noise

Monthly anneal (warm from -85 C to + 5C) to heal hot pixels

Page 25: Background information for users of STIS Charles R. Proffitt

STIS Presentation 25

CCD Read Noise AMP D has always had lowest read-noise and is

used for science At Gain=1, read-noise initially ~ 4 e-

Increased to 4.5 e- after SMOV3a After switch to STIS side-2, additional 15-18 kHz electronic

noise increased read noise to ~ 5.5 e- (herring bone pattern)• careful Fourier filtering can sometimes remove this

Gain=4 showed pick-up noise even on side-1 ~7.3 e- on side 1; ~ 7.7 e- on side 2

From STIS ISR 2001-05By Tom Brown

Page 26: Background information for users of STIS Charles R. Proffitt

STIS Presentation 26

CCD Options

Gain: 1, 2, 4, or 8 Only Gains values of 1 and 4 supported for GO observations. Gain=1 has lower read-noise, but amps saturate at ~33,000 e-. Gain=4 has higher read-noise, but allows full well of CCD to be

used (144,000 e- at center, ~ 120,000 e- at edges) In saturated GAIN=4 images, electrons bleed to other pixels

(perpendicular to dispersion direction), but are not lost. Total response remains linear, allowing very high S/N with special processing techniques.

Binnng at readout by 1, 2, or 4 in either axis or both Binning data during read-out reduces read-noise and file size Increases impact of bad pixels and cosmic rays. With older, noisier detector, usually not worthwhile

Page 27: Background information for users of STIS Charles R. Proffitt

STIS Presentation 27

CCD Options - cont

CCD Sub-arrays Can save only part of image array on read-out

Reduces file size and number of buffer dumps required Decreases readout time, allowing increased cadence.

For GOs only support reducing AXIS2 size (perpindicular to dispersion direction) Discards virtual overscan in parallel direction, but retains physical overscan in serial

direction to aid in bias removal Lack of virtual overscan does make bias subraction more difficult

Reducing AXIS1 is an available-but-unsupported mode. Reducing both discards all overscan regions, greatly increasing difficulty of accurate bias

removal. Different clocking patterns used by any CCD sub-arrays may introduce artifacts,

and invalidate assumptions of empirical CTI corrections algorithms. Cosmic Ray rejection is normally done by taking multiple images.

CRREJECT=2 is default

AXIS1

AXIS2

Page 28: Background information for users of STIS Charles R. Proffitt

STIS Presentation 28

CCD Charge Transfer Inefficiency

During parallel transfers some electrons get trapped

Trapped e- be released later during read, causing extended “tail”.

Number of free traps depends on flux level that has moved through that pixel.

CTI gets worse with increasing radiation damage

No sufficient pixel based physical model, so need empirical corrections.

Loss increases with # of transfers (1-CTI)n Putting target near readout amp reduces losses E1 positions defined near row 900 Typical exposures of faint targets with the STIS

CCD in cycle 17 might experience 20-30% CTI losses when target at center of the detector, but only 5-8% if at E1 near row 900.

Page 29: Background information for users of STIS Charles R. Proffitt

STIS MAMAs

Page 30: Background information for users of STIS Charles R. Proffitt

STIS Presentation 30

FUV MAMA Dark Current

FUV MAMA initially had very low dark current (7x10-6 counts/lo-res-pixel/s), but occasionally showed enhanced glow.

Initially glow present only rarely became more frequent over time

Lower edge & lower right hand corner remains mostly dark (near original 7 x 10-6 counts/lo-res-pixel/s).

Physical basis of FUV dark current glow is unclear

Page 31: Background information for users of STIS Charles R. Proffitt

STIS Presentation 31

QuickTime™ and aTIFF (Uncompressed) decompressor

are needed to see this picture.

131 darksApr 1997Aug 1998178809 s

Mean 0.21Glow 0.37D.C. 0.161x 10-5 c/p/s

(hi-res-pixel)2048 x 2048

126 darksAug 1998Nov 1999173880 s

Mean 0.45Glow 1.08D.C. 0.165x 10-5 c/p/s

141 darksDec 1999May 2001194580 s

Mean 0.56Glow 1.24D.C. 0.161x 10-5 c/p/s

125 darksMay 2003Aug 2004172500 s

Mean 0.65Glow 1.65D.C. 0.154x 10-5 c/p/s

Dark Corner

Glow region

Page 32: Background information for users of STIS Charles R. Proffitt

STIS Presentation 32

FUV MAMA Dark Current FUV MAMA dark current increases

~ linearly with time since HV turn-on

Increases faster at higher T Rate of increase has gone up over

the years Hot pixels also increasing

Page 33: Background information for users of STIS Charles R. Proffitt

STIS Presentation 33

FUV MAMA Dark Current

Mitigation strategies Use only first orbit of each SAA free period for observations that

need low dark current. (only 1 orbit per day). Keep FUV HVPS off when detector not in use (ops change). Cool detector (NUV MAMA off). Place target on darker part of detector.

New D1 aperture position defined near bottom edge of detector

The count rate summed in each column over a seven pixel high region of the mean dark image covering the period between May 2003 and August 2004. The dotted line gives the results for a region near the standard 1st order spectral location, and the solid line gives the results at the new D1 position

located near the bottom edge of the detector.

Page 34: Background information for users of STIS Charles R. Proffitt

STIS Presentation 34

NUV MAMA Dark Current

NUV MAMA dark current dominated by a different physical mechanism than the FUV MAMA

Meta-stable states with lifetimes of days to weeks are populated by high-energy particle impacts, leading to a phosphorescent window glow.

Long term trend depends on low-earth orbit radiation environment

Page 35: Background information for users of STIS Charles R. Proffitt

STIS Presentation 35

NUV MAMA Dark Current Effect of temperature changes on dark current is complex Short term changes lead to a large increase in the dexcitation rate,

leading to a large, but temporary, increase in the dark current, including daily cycling as MAMA warms up.

Over the long term, a smaller equilibrium number of populated states partially balances the higher excitation rate caused by higher average T.

If detector cold for long time, large but temporary increase until a new equilibrium is reached.

Page 36: Background information for users of STIS Charles R. Proffitt

STIS Presentation 36

MAMA Pipeline Dark Images

Low dark rates require averaging hundreds of images to make useful dark image.

NUV darks semi-empirically scaled for time and temperature changes and subtracted in pipeline.

Secular changes are seen in shape of NUV dark current over time.

Unpredictable nature of FUV glow makes subtracting it in OTFR pipeline impractical

Only base dark current and hot pixels subtracted by pipeline - users need to to custom extraction of glow.

In background limited observations, FUV hot pixels should just be masked out because poor statistics makes subtraction difficult.

Page 37: Background information for users of STIS Charles R. Proffitt

STIS Presentation 37

MAMA Flat Fields

On-orbit lamp images used to provide MAMA pixel-to-pixel flats collected during occasional campaigns. MAMA flats very stable once data binned to lo-res

(1024x1024) Can use same pixel-to-pixel flats for essentially all

data. Flat fielding of unbinned 2048x2048 hi-res images not

repeatable - significant structure remains hi res mostly useful for filtering out hot pixels.

Low order MAMA flatfields provided for selected modes (mostly FUV modes).

Page 38: Background information for users of STIS Charles R. Proffitt

STIS Presentation 38

MAMA Observation Modes

ACCUM mode Keeps track of how many events fall on each pixel. For medium and high dispersion modes, the pixel

locations are corrected for spacecraft doppler motion as image is accumulated.

STIS data buffer can hold 1 hires (2048x2048) image or up to 7 lowres MAMA + CCD full frame images or 1 hires image + 3 lowres or CCD full frame images

Hires format default for MAMA science, lores for wavecals

Page 39: Background information for users of STIS Charles R. Proffitt

STIS Presentation 39

MAMA Observation Modes

TIME-TAG mode Records x-y location and time of each event with 125 micro-

second resolution. Corrections for spacecraft Doppler motion done on ground, not on

spacecraft STIS buffer divided into two sections for time-tag

Each half of buffer can hold 2 x 106 events. One half of buffer can be dumped while other half is recording. User must predict rate and specify buffer time so that buffer is

dumped before one half fills, otherwise gaps will appear in sequence. If global rate < 20,000 counts / s, continuous observations can be

sustained for extended periods (up to 30 buffer dumps). For some projects needing time resolved data, a series of

ACCUM observations may be better than time-tag mode. For CCD observations, the use of subarrays may increase

cadence.

Page 40: Background information for users of STIS Charles R. Proffitt

STIS Presentation 40

Time resolved STIS Observing

Detector Mode Minimum Sample time (texp)

Time between samples (dt)

Max time for uninterrupted time series

MAMAs Time-tag 125 s 0 6e7/R s for R < 20,000 cnts/s

4e6/R s for R > 20,000 cnts/s (R=global count rate)

MAMAs Hi-res ACCUMs

0.1 s 30s if texp > 3 m

2 m if texp < 3 mNo limit

MAMAs Lo-res ACCUMs

0.1 s 30s if texp > 3 m

1 m if texp < 3 m

No Limit

7

CCD Full Frame ACCUMs

0.1 s 45 s No limit for texp > 3 m

(texp + dt) x 7

CCD 1060x32 subarray ACCUMs

0.1 s 20 s No limit for texp > 3 m

(texp + dt) x 256

Page 41: Background information for users of STIS Charles R. Proffitt

STIS Presentation 41

Other MAMA Constraints

STIS MAMAs cannot be used in any SAA impacted orbit Optical isolators scintillate from cosmic rays and can

cause random bit flips in MAMA electronics STIS low & high voltage turned off during deepest SAA

passages; not practical to turn on MAMA for only part of individual orbits.

Allows use during only one ~ 5 - 6 orbit block per day Observers required to separate CCD and MAMA

science observations into separate visits when practical

Page 42: Background information for users of STIS Charles R. Proffitt

STIS Presentation 42

Summary of Overheads

Page 43: Background information for users of STIS Charles R. Proffitt

STIS Presentation 43

STIS Data Products

Selected STIS data file types:

opppvvnnd_tag.fits - table of time tag events opppvvnnd_raw.fits - 2d image of unproccesed data opppvvnnd_flt.fits - flat fielded image opppvvnnd_crj.fits - cosmic ray rejected image (CCD) opppvvnnd_x1d.fits - fits table with 1D extracted spectra opppvvnnd_sx1.fits - 1D spectra from summed images opppvvnnd_x2d.fits - 2D spectral image (rectified and flux

calibrated) opppvvnnd_sx2.fits - 2D spectral image (rectified and flux

calibrated) from summed images

Page 44: Background information for users of STIS Charles R. Proffitt

STIS Presentation 44

1D spectral extraction

In 1D spectral extraction, an extraction box is centered on spectrum, and summed over cross dispersion direction at each pixel in dispersion direction.

Extracted spectrum is then background subtracted and flux calibrated

Corrections for aperture throughputs, time-dependant sensitivity changes and CTI losses (CCD only) are applied.

Geometry for extraction of 1st order STIS spectra

Page 45: Background information for users of STIS Charles R. Proffitt

STIS Presentation 45

1D spectral extraction - cont

For echelle modes, a separate 1D extraction is done for each spectra order

Background subtraction is done using a special algorithm that models the scattered light (see STIS ISR 2002-001 by Valenti et al

Page 46: Background information for users of STIS Charles R. Proffitt

STIS Presentation 46

2D spectral extraction

Image rectified so that wavelength and spatial scales are linear and aligned with x and y coordinates.

X2d image is flux calibrated (science images only) Corrections for aperture width and time-dependant

sensitivity changes are applied (no CTI correction).

Page 47: Background information for users of STIS Charles R. Proffitt

STIS Presentation 47

Spatial Undersampling of STIS

Critical sampling of PSF requires about 2 pixels per PSF FWHM

STIS CCD spatial scale of ~0.051”/pixel undersampled by ~2x @ 5000 Å.

STIS MAMA spatial scale ~0.0245”/pixel undersampled by ~2x @ 2500 Å.

Undersampling can produce artifacts when extracting spectra at small spatial scales (affected by tilt of spectrum on detector)

Dithering along long slit to sub-sample spatial scale recommended if spatial structure is significant.

Page 48: Background information for users of STIS Charles R. Proffitt

STIS Presentation 48

Selected Data Artifacts

CCD window reflections.Brightest ring about 1% of flux

Some MAMA modes also show imaging ghosts.

Airy rings produce spectroscopic fringes

IR fringing due to multiple reflections in CCD. Need contemporaneous tungsten fringe flats to correct properly.