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MIPS : AOT Description


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The MIPS AOT inputs are relatively few, and designing a typical MIPS observation is not complicated. However, the design of all MIPS observations should be based on a careful examination of the far-infrared properties of the particular region of the sky to be observed, and a good understanding of MIPS operation, capabilities, and limitations. In addition, the orientation and rotation of the Spitzer focal plane can be a factor, as can the three-hour limit of a MIPS AOR (e.g., for large scan maps).

There are four major operational modes (or Astronomical Observing Templates; AOTs) of the MIPS instrument:

  • Scan Map (includes slow, medium and fast scan rates, where incomplete coverage at 160 microns is obtained at the fast scan rate).
  • Photometry and Super Resolution (includes super-resolution, large source, and small source options, and can be used to obtain multiple images through the cluster and raster-map options).
  • Spectral Energy Distribution (SED; can be used for a single spectrum or step and stare spectral mapping).
  • Total Power Mode (used to obtain absolute brightness measurements for highly extended sources).
Observing in any of these modes involves the acquisition of multiple data frames, not just a single frame. The multiplicity of frames provides for rejection of cosmic rays, calibration of the Ge:Ga focal plane array data in the light of the two time-constant behavior of those detectors, adequate sampling of the point spread function (PSF; especially for super resolution observations), and, in the case of the 160 micron array, for building up a filled image using multiple offset exposures of that 2x20 pixel array. The total number of images obtained depends on the total integration time needed, the observational mode, and the array. The multiplicity of frames is prescribed within the Astronomical Observing Templates (AOTs), and the observer selects the number of times to repeat the basic pattern of a template in order to build up the desired integration time. The exposure times for each frame are also limited by the AOTs, with the result that the total integration times that can be specified are quantized. The details of this are described in the Spitzer Observer's Manual.

Scan Map Mode

The scan map mode is designed to provide efficient mapping of large areas on the sky. A ramp motion of the scan mirror compensates for continuous telescope scanning motion, freezing the images on the arrays. The scan map mode avoids having to repoint and stabilize the telescope between exposures.

Scan rate24 microns (sec) 70 microns (sec) 160 microns (sec) Overscan time (min)
slow (2.6 arcsec/sec)100 sec 100 sec10 sec1.2 min
medium (6.5 arcsec/sec)40 sec 40 sec4 sec3.2 min
fast (17 arcsec/sec)15 sec 15 sec3 sec(a)7.9 min
Note: Each source appears in 10 consecutive frames for slow and medium scans at 24 and 70 microns, each source appears in 5 consecutive frames for fast scans at 24 and 70 microns, and each source appears in one frame at slow and medium scans at 160 microns.
(a) Only 1/2 of map region covered by 160 micron pixels at the fast scan rate in one scan leg.

Scan leg offset lookup table - how wide is half the array? What are the rest of the available offsets in units of array widths?

Observers should step by at most 2.5 arcmin (1/2 array) cross-scan steps to ensure full coverage at 70 microns. Depending on the scan rate, observers might want to step by at most 1.3 arcmin (1/4 array) steps to ensure full coverage at 160. Use Spot to visualize your observations to be sure that it is doing what you think it should be doing.

Photometry and Super-Res Summary

Mode Band Frames / Obs. Cycle (a) Approximate Integration Time per Pixel per Cycle (b)
Compact Source Photometry 24 microns 14 (c) 42, 140, 420 sec (d)

70 microns 10 30, 100 sec
160 microns 14 (e) 6, 20 sec
Large Source Photometry

24 microns 10 / 10(f) 30, 100, 300 sec (d)
70 microns 6 / 6 18, 60 sec
160 microns 10 / 10 (f) 3, 10 sec
Compact Source Super Resolution 24 microns 14 (c) 42, 140, 420 sec (d)
70 microns 8 / 8 24, 80 sec
160 microns 42 (g) 18, 60 sec
Large Source Super Resolution 24 microns 10 / 10 (c) 30, 100, 300 sec (d)
70 microns 32 / 32 24, 80 sec
160 microns N/A N/A

(a) Two values indicate # of frames on-source/off-source
(b) For 3 and 10 second exposure times (and 30 seconds at 24 microns) respectively. Times are per pixel on a given sky position in MIPS seconds. Actual exposure times are 1.05 times longer.
(c) At 24 microns, 2 additional frames are taken per AOR, so total integration time will be longer than shown here by (2 times the exposure time). See also next note.
(d) For the first cycle in an observation at 24 microns, exposure time is 1 second shorter than shown in this table. See also previous note.
(e) The 10 160 micron frames combine to provide a 2' x >5' filled field of view containing 2 images of the source.
(f) The 10 160 micron frames combine to provide a 4' x 5' filled field of view containing a single image of the source.
(g) The 3 x 10 160 micron frames combine to provide a 2' x >5' filled field of view containing 6 images of the source sampled at sub-pixel shifts.
Experienced MIPS observers might note that the 70 and 160 micron portions of the PH/SR AOT were changed with respect to our pre-launch plans to keep the source on only one side of the respective arrays. Additional images were included in the 160 micron AOT to ensure full coverage. Always use Spot to visualize your observations to be sure that it is doing what you think it should be doing.

Spectral Energy Distribution Mode

The Spectral Energy Distribution (SED) mode applies only to the 70 micron Ge:Ga array, since it requires an offset of the scan mirror that deflects light away from the optical trains for the other arrays. This operating mode provides low-resolution (R ~ 20) spectral information from about 55-96 microns. The SED optical train illuminates a slit approximately 24 pixels long on the array by 2 pixels wide, with dispersion via a reflection grating.

Total Power Mode

MIPS is optimized to provide calibrated images of sources that are small enough that they can be chopped on and off of the arrays, particularly at 70 and 160 microns. The Total Power mode AOT provides a way to accurately measure extended emission as well, by chopping between an internal dark position and the sky.

Examples of MIPS AOTs

See also the Observation Planning Cookbook.


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This file was last modified on Thu Sep 28 12:39:07 2006.

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