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Space Telescope Imaging Spectrograph Instrument Handbook for Cycle 22 > Chapter 3: STIS Capabilities, Design, Operations, and Observations > 3.2 Instrument Design

3.2
In this section, we provide a high-level summary of the basic design and operation of STIS, concentrating on the information most relevant to your HST observing proposal. Subsequent chapters provide more detailed information.
3.2.1 Detectors
STIS uses three large-format (1024 × 1024 pixel) detectors
(see Chapter 7 for more details), as follows:
A Scientific Image Technologies (SITe) CCD, called the STIS/CCD, with ~0.05 arcsecond square pixels, covering a nominal 52 × 52 arcsecond square field of view (FOV), operating from 1640 to 10,300 Å.
A Cs2Te Multi-Anode Microchannel Array (MAMA) detector, called the STIS/NUV-MAMA, with ~0.025 arcsecond square pixels, and a nominal 25 × 25 arcsecond square field of view (FOV), operating in the NUV from 1600 to 3100 Å.
A solar-blind CsI MAMA, the STIS/FUV-MAMA, with ~0.025 arcsecond ­pixels, and a nominal 25 × 25 arcsecond square FOV, operating in the FUV from 1150 to 1700 Å.
The CCD
The CCD provides high quantum efficiency and good dynamic range in the NUV through NIR. The CCD produces a time-integrated image in the ACCUM data-taking mode. As with all CCDs, there is noise (read noise) and time (read time) associated with reading out the detector. Time-resolved work with this detector is done by taking a series of multiple short exposures. The minimum exposure time is 0.1 second, and the minimum time between successive identical exposures is 45 seconds for full-frame, but can be reduced to 20 seconds for subarray readouts. CCD detectors are capable of high dynamic range observations. The dynamic range for a single exposure ultimately is limited by the depth of the CCD full well (144,000 electrons), which determines the total amount of charge (or counts) that can accumulate in any one pixel during any one exposure without causing saturation. For GAIN=1, it is further limited (to 33,000 electrons) by saturation in the gain amplifier. Cosmic rays will affect all CCD exposures. CCD observations should be broken into multiple exposures (called CR-SPLITs) of no more than 1000 seconds each, whenever possible, to allow removal of cosmic rays in post-observation data processing; during Phase II you can specify the CR-SPLIT optional parameter to do this (see Chapter 11).
The MAMAs
The two MAMAs are photon-counting detectors which provide a two-dimensional UV capability. They can be operated either in ACCUM mode, to produce a time-integrated image, or in TIME-TAG mode to produce an event stream with high (125 microseconds) time resolution. Doppler correction for the spacecraft motion is applied automatically onboard for data taken in ACCUM high-spectral-resolution modes.
The STIS MAMA detectors are subject to both scientific and absolute brightness limits. At high local (≥50 counts/s/pix) and global (285,000 counts/s) illumination rates, counting becomes nonlinear in a way that is not correctable. At only slightly higher illumination rates, the MAMA detectors are subject to damage. We have therefore defined absolute local and global count rate limits, which translate to a set of configuration-dependent bright object screening limits. Sources which violate the absolute count rate limits in a given configuration cannot be observed in that configuration, as discussed in Section 7.7.
Early concerns about the signal-to-noise attainable with the MAMAs have been alleviated by experience in orbit. Values of 50:1 per spectral resolution element in extracted spectra are routinely obtained for point sources with sufficient counting statistics when integrated over the extraction aperture. Higher signal-to-noise values of 100–300 can be obtained by stepping the target along the slit in the first-order modes, or by use of special multiple slits with the echelles (see Chapter 12). Current information indicates that the flat fields are stable to ±1–2%. See also Section 16.1.
3.2.2 STIS Physical Configuration
The STIS optical design includes corrective optics to compensate for HST’s spherical aberration, a telescope focal plane slit-wheel assembly, collimating optics, a grating selection mechanism, fixed optics, and camera focal plane detectors. An independent calibration lamp assembly can illuminate the focal plane with a range of continuum and emission line lamps. A simplified schematic showing major mechanisms and detectors, and a medium-resolution echelle mode light path is shown in Figure 3.1.
Figure 3.1: Simplified STIS Optical Design
Slit and Grating Wheels
The slit wheel contains apertures and slits for spectroscopic use and the clear, filtered, and coronagraphic apertures for imaging. The slit wheel positioning is repeatable to very high precision: ±7.5 and ±2.5 milliarcseconds in the spatial and spectral directions, respectively.
The grating wheel, or so-called Mode Selection Mechanism (MSM), contains the first-order gratings, the cross-disperser gratings used with the echelles, the prism, and the mirrors used for imaging. The MSM is a nutating wheel which can orient optical elements in three dimensions. It permits the selection of one of its 21 optical elements as well as adjustment of the tip and tilt angles of the selected grating or mirror. As described in “Routine Wavecals” below, the grating wheel exhibits non-repeatability which is corrected for in post-observation data processing using contemporaneously obtained comparison-lamp exposures.
For some gratings, only a portion of the spectral range of the grating falls on the detector in any one exposure. These gratings can be scanned (tilted by the MSM) so that different segments of the spectral format are moved onto the detector for different exposures. For these gratings a set of pre-specified central wavelengths, corresponding to specific MSM positions, i.e., grating tilts, has been defined (see Chapter 4).
Calibration Lamp Systems
STIS has two independent calibration subsystems, the so-called Hole in the Mirror (HITM) system and the Insert Mechanism (IM) system. The HITM system contains two Pt-Cr/Ne line lamps used to obtain wavelength comparison exposures and to illuminate the slit during target acquisitions. Light from the HITM lamps is projected through a hole in the second correction mirror (CM2). In some very early STIS data, the STIS external shutter was left open during the HITM wavecal exposure and the spectra of the lamp and the sky were recorded simultaneously. However, this is no longer an available option. Now the external shutter is always closed during the HITM lamp exposures. The IM system contains flat-fielding lamps (a tungsten lamp for CCD flats, a deuterium lamp for NUV-MAMA flats, and a krypton lamp for FUV-MAMA flats) and a single Pt-Cr/Ne line comparison lamp. When the IM lamps are used, the Calibration Insert Mechanism (CIM) is inserted into the light path and all external light is blocked. Observers will be relieved to know that the ground system will automatically choose the right subsystem (see Section 3.3) and provide the necessary wavelength calibration exposures.

Space Telescope Imaging Spectrograph Instrument Handbook for Cycle 22 > Chapter 3: STIS Capabilities, Design, Operations, and Observations > 3.2 Instrument Design

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