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Overview

At the time of writing, a final calibration of the throughput of NICMOS is not yet available. Observers should find the present calibration sufficient to prepare Phase I proposals but should consult the STScI NICMOS WWW pages for updated information when preparing Phase II proposals.

Instrumental Factors

Detectors

The detector properties which will affect the sensitivity are simply those familiar to ground-based optical and IR observers, namely dark current and read noise, and the detector quantum efficiency (DQE). Laboratory and preliminary on-orbit measurements have determined the read noise for the three NICMOS flight arrays to be ~35 electrons. The measured numbers are given in Table 7.1 on page 106.

Optics

NICMOS is a relatively simple instrument in layout, and thus contains a fairly small number of elements which affect the sensitivity. These are the filter transmission, the field of view (determined by the NICMOS optics external to the dewar, in combination with the HST mirrors), the reflectivities of the various external mirrors and the transmission of the dewar window.

The filter transmissions as functions of wavelength were measured in the laboratory, and the resulting curves are presented in Chapter 11. Some filters may have minor leaks outside the primary filter bandpass; the reality of these has not yet been established, and we assume here for the purposes of sensitivity calculations that the transmission is zero outside the primary bandpass.

NICMOS contains a total of seven mirrors external to the dewar, each of which reduces the signal received at the detector. The mirrors have protected silver coatings (except for the field divider assembly which has a gold coating) for maximum reflectivity, and have 98.5% reflectivity. The dewar window has a transmission of roughly 93%. Therefore, the combination of optical elements is expected to transmit ~84% of the incoming signal from the OTA.

The sensitivity will obviously be affected by the pixel field of view. The smaller the angular size of a pixel, the smaller the fraction of a given source that will illuminate the pixel. Finally, the optical efficiency will be degraded further by the reflectivities of the aluminum with MgF2 overcoated HST primary and secondary mirrors. These are given as exactly one minus the emissivities.

Background Radiation

At long wavelengths the dominant effect limiting the NICMOS sensitivity will be the thermal background emission from the telescope. How large this will be depends on the areas of the primary and secondary mirror and their optical configuration, temperatures, and emissivities. We discussed the issue of thermal background and its stability in Chapter 3.

For the purposes of sensitivity calculations, we used the values listed in Tables 6.1 and 6.2 and assumed that the effects of debris on the mirrors can be ignored.

Table 6.1: Optical Efficiency

Optical Element

Efficiency

First bending mirror

0.985

Re-imaging mirror

0.985

Pupil mirror

0.985

Image mirror

0.985

First paraboloid

0.985

Second paraboloid

0.985

Bending mirror

0.985

Dewar window

0.93

Total

0.84

Table 6.2: HST Infrared and Optical Properties

Property

Assumed Value

Primary mirror collecting area

38993 cm2

Primary mirror temperature

291 K

Primary mirror emissivity

0.048

Secondary mirror collecting area

684.4 cm2

Secondary mirror pupil clear fraction

0.76

Secondary mirror temperature

288.5 K

Secondary mirror emissivity

0.048

Focal plane image scale

35.8 arcsec/cm

Back focal distance

640.6 cm

At shorter NICMOS wavelengths, sensitivities will be affected by the zodiacal background which is given by the equation in Chapter 3; the overall expected background is shown in Figure 3.6.

Background radiation will be a slightly worse problem in the case of Multi-Object Spectroscopy (MOS) than in the case of imaging observations. Every pixel on the array will always see the entire background radiation integrated over the grism bandpass. The expected detected background rate per pixel is shown in Table 5.3.



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