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The Multiband Imaging Photometer for the Space Infrared Telescope Facility

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Title: The Multiband Imaging Photometer for the Space Infrared Telescope Facility


1
The Multiband Imaging Photometer for the Space
Infrared Telescope Facility
  • William B. Latter
  • (SSC/MIPS Instrument Scientist)
  • George H. Rieke
  • (MIPS Principal Investigator)
  • and
  • The MIPS Instrument Team

The Solar System and Circumstellar Dust Disks
Prospects for SIRTF 18 - 20 August 1999 Dana
Point, CA
2
(No Transcript)
3
Outline
  • Introduction to the MIPS
  • Origin of the MIPS
  • Instrument capabilities
  • The MIPS Instrument
  • Basic Layout
  • The MIPS Detectors
  • Some MIPS Science
  • MIPS Detector Behavior
  • Calibration Plans

4
What/Who is the MIPS?
  • The Multiband Imaging Photometer for SIRTF (MIPS)
    is the long wavelength instrument on SIRTF (? 20
    to 180 mm)
  • Some of the Team
  • George H. Rieke (U. Arizona), Principal
    Investigator
  • Erick Young (U. Arizona), Deputy PI, Detector
    Lead
  • Chad Engelbracht, Arizona MIPS Scientist
  • William B. Latter, SSC/MIPS Scientist
  • Jocelyn Keene, JPL MIPS Scientist
  • Douglas Kelly, MIPS Test Scientist
  • Ball Aerospace building the instrument
  • University of Arizona GeGa focal plane arrays
  • See http//sirtf.caltech.edu/Observing/Tools/html
    /mips.html
  • and http//mips.as.arizona.edu

5
Origin of the MIPS
  • MIPS is an instrument that is based on simple
    principles.
  • Imaging at 24, 70, and 160 mm.
  • 70 ?m is longest wavelength without a strong
    confusion limit.
  • 24 mm at geometric mean between 8 mm (IRAC long
    band) and 70 mm.
  • 160 mm at geometric mean between 70 mm and 350 mm
    (accessible from ground).
  • Super resolution is an important science goal.
  • Requires pixels lt l/2.5D.
  • At 70 mm, such small pixels would be limited in
    sensitivity by cosmic ray hits.
  • Scale change at 70 mm needed to provide both
    super resolution and sensitivity.
  • Science requires ability to measure SEDs at more
    than 3 wavelengths.
  • A scan mirror was required to modulate signals to
    overcome detector 1/f noise.
  • Creative use of the scan mirror provides the
    above capabilities, plus efficient operating
    modes.

6
Multiband Imaging Photometer for SIRTF Basic
Capabilities
Array Format
Field of View (')
Pixel Size (")
F/
l/Dl
l (mm)
Band
Mode
24mm
4
20.5 26.5
7.4
5.1x5.1
2.4
128x128
70mm
5.1x5.1
60 80
3.5
Survey
32x32
9.4
18.7
Super Resolution
3.5
70mm
2.6x2.6
60 80
32x32
4.9
37.4
70mm
14 24
4.0x0.3
52 99
32x24
9.4
18.7
S.E.D.
5.1x0.5 (effective)
160mm
4
2x20
15
140 180
46
Point Extended Source Saturation Limits
(in one sample) 24 mm
8 Jy (1 Jy/Pixel) 70 mm
8 Jy (1.4 Jy/Pixel) 160 mm 8 Jy (1
Jy/Pixel)
Sensitivity (mJy) (5 s in 500 s) 24 mm
370 70 mm 1400 160 mm 22.5 mJy (160
mm is model dependent confusion limited)
See http//sirtf.caltech.edu/Observing/Tools/html
/mips.html and http//mips.as.arizona.edu
7
The MIPS MechanicalDesign and Layout
Imaging Mirrors
  • Aluminum Baseplate
  • 21 Reflective Optic Elements
  • Mirror Support Brackets
  • 3 Focal Plane Assemblies
  • 8 Filters
  • CSMM
  • Masks, Baffles, Paint
  • Cover (not shown)
  • Cables (not shown)
  • Electrical Thermal Feed Throughs

70 mm FPA
160 mm FPA
Pick-off Mirrors
24 mm FPA
CSMM
8
Where the Light Goes
70mm Pupil Imaging Mirror
160 mm Fold Mirror
160 mm Pupil Mirror
Slit Mirror
160 mm FPA
24mm Pupil Imaging Mirror
70mm FPA
Flat Field Relay Mirror 2
24mm Camera Mirror 1
160mm Camera Mirror
Narrow Field Fold Mirror
24mm Camera Mirror 2
Periscope Mirror 1 (above) Periscope Mirror 2
(below)
24mm FPA
Flat Field Relay Mirror 1
Grating
24mm Fold/Pupil Mirror
24mm Band Scan Mirror
70mm Band Scan Mirror
Narrow Field Camera Mirror
24mm Pick-off Mirror
70mm Pick-off Mirror
9
The MIPS is Real!
10
And very black inside, too.
11
MIPS Focal Plane Arrays
  • 24 mm Band
  • 128 x 128 pixel SiAs BIB detector array
  • Developed by Boeing-North American
  • IRS Team has lead development responsibility
  • 70 mm Band
  • 32 x 32 pixel GeGa photoconductor array
  • Developed and constructed at the Steward
    Observatory
  • Detector material from Lawrence Berkeley
    Laboratory
  • Custom cryogenic readouts ( CRC-696 )
  • 160 mm Band
  • 2 x 20 pixel stressed GeGa photoconductor array
  • Developed and constructed at the Steward
    Observatory
  • Detector material from Lawrence Berkeley
    Laboratory
  • Custom cryogenic readouts ( CRC-696 )

12
70 mm Qualification Array with Filter Holder
13
2 x 20 GeGa Stressed Array
MIPS 160 micron band
Stressed array footprint
14
The MIPS Flight CryogenicScan Mirror Mechanism
15

MIPS in the SIRTF Focal Plane
16
MIPS ScienceThe Potential
The MIPS 70 micron sky These are
logarithmically scaled versions of comparison
images generated for MIPS, SOFIA, ISO, and IRAS.
A test field was "observed" with with each
instrument for 24 hours, taking into account
sensitivity, image scale, and field of view. The
IRAS image has very large pixels and is really
only capable of detecting the infrared cirrus in
this field. The ISO image has better spatial
resolution but is limited by the small
field-of-view and low sensitivity of the arrays.
SOFIA has excellent spatial resolution but a
correspondingly small field-of-view and is
limited in sensitivity because it uses warm
optics. Courtesy of Chad Engelbracht
17
Simulated 24 and 70 micron Observations of
Circumstellar Disks
Below are simulated 70 mm observations convolved
with a model of the SIRTF Point Spread Function.
Left to Right Vega, 1/10 as much dust as Vega, a
point source. All are on a logarithmic brightness
scale.
Left are simulated 24 mm observations convolved
with a model of the SIRTF PSF on a logarithmic
brightness scale. The left image is Vega. On the
right is the difference of a Vega-like star with
1/100 times less dust and a point source of the
same total flux.
Simulations by Ned Wright (UCLA)
18
MIPS ScienceThe Possibilities
  • MIPS provides the last opportunity in the
    foreseeable future to observe at far infrared
    wavelengths from space. Even with a 5 year
    mission, MIPS time will likely be in strong
    demand. Examples of potential science programs
    include
  • Extragalactic
  • Detailed IR maps of galaxies such as M33
    structure, star formation, cirrus.
  • Cosmology and the early universe with large area
    mapping.
  • Far-IR properties of quasars and ultraluminous
    galaxies.
  • Galactic
  • Survey star formation sites, and examine the
    earliest stages of stellar birth.
  • Examine the temperature, structure, and dust
    composition of the ISM surrounding sites of
    massive star formation.
  • Structure and frequency of proto-planetary debris
    disks.
  • Solar System
  • Cometary debris, structure, and composition.
  • Counts and colors of Kuiper Belt objects.
  • Detailed studies of the Zodiacal dust.
  • You make up you own!

19
The MIPS AstronomicalObserving Templates
  • MIPS Photometry Super Resolution Imaging
  • Imaging photometry and high resolution imaging at
    24, 70, and 160 ?m.
  • MIPS Freeze-frame Scan-mapping
  • Telescope scanning at 24, 70, and 160 ?m for
    large field maps
  • MIPS Spectro-Photometry or Spectral Energy
    Distribution (SED)
  • ?/?? 14 - 25 covering 52 - 99 ?m.
  • MIPS Total Power Measurement
  • Zero level reference observations for absolute
    brightness of very extended sources.
  • Because of the expected science demands and
    pointing limitations for SED, the
    Photometry/Super Resolution and Scan AOTs have
    been selected to be available for Cycle 1
    observing. The other two AOTs will be available
    for Cycle 2.
  • Important Operational Features
  • Array operation is identical for all modes, as
    is data grouping.
  • Commanding, stimulator, and scan mirror
    operation is very similar for all modes.
  • Solar System tracking is currently supported for
    all MIPS AOTs.

20
How the GeGa Detector Arrays Behave
  • Bulk photoconductors have multiple time constant
    response.
  • Infrared-active and high impedance regions are
    identical.
  • Changes in illumination result in changes in
    space charge that occur
  • at roughly the RC time constant of this high
    impedance region.
  • At the same time, simple generation-recombination
    of charge carriers
  • occurs quickly.
  • Consequently
  • Initial background plays a key role in behavior,
    since it sets initial R in RC.
  • Transient for light on is slower than for
    light off.
  • Space charge adjustments near contacts can
    overshoot, resulting in hook.
  • In addition, CR hits compensate the material,
    changing the detector
  • response characteristics (and eventually
    increasing noise).
  • The MIPS implementation is robust
  • MIPS uses a DC-stable readout process that gives
    good recovery from transients.
  • Neither detectors nor readouts are subject to
    damage at SIRTF CR dose levels.

21
Mitigation for Photoconductor Misbehavior
  • Stimulator flashes included in normal
    data-taking at 1/( 2 min).
  • Will allow calibration to be tracked and fitted.
  • Extensive modeling of basic physics is underway
    to understand the details
  • For example, the effects of a stimulator flash
    on the calibration it is measuring.
  • Extensive ground testing of fight detectors
    under typical observing conditions.
  • Scan mirror allows rapid modulation of signals
    so all measurements rely
  • as much as possible on the fast response.
  • Pure fast response has excellent photometric
    characteristics.
  • Strategies included to anneal detectors to
    remove CR effects periodically all
  • work by flooding detector with charge carriers to
    restore equilibrium.
  • Thermal anneal raises detector temperature
    briefly.
  • Bias boost causes the detector to break down
    electrically.
  • Photon flood illuminates it with a bright
    source.
  • Raw data frames sent to ground to permit further
    optimization of reduction.
  • Coadds of adjacent frames can be used to reduce
    data rate.

22
Calibration ofMIPS Data
  • Requirement MIPS shall be able to repeat
    photometric measurements of bright sources to
    better than 4, with 5 absolute flux
    calibration.
  • The instrument allows measurement of dark
    current, flat field, responsivity, etc.
  • Scan mirror can be used to put arrays in the dark
    as well as select flat field projector for
    spectral energy distribution mode.
  • Scan mirror moves sources around on array.
  • Improves sampling
  • Robust behavior in the presence of bad pixels
  • Keeps detectors in fast response regime
  • The scan mirror and stimulator operation are
    closely synchronized with the observing modes.
  • Track responsivity changes
  • Measure flat field
  • Maintain flux calibration
  • The definition of a few standard observing modes
    aids in calibration repeatability.

23
Summary
  • MIPS is a powerful, versatile, and operationally
    simple instrument.
  • The four MIPS AOTs provide accurate photometric
    and super resolution observations of compact
    objects, sensitive and efficient large area
    mapping, low resolution spectroscopy, and the
    ability to make absolute flux measurements of
    very diffuse material.
  • Photometry/Super Resolution and Scan AOTs
    available at launch. The remaining two will be
    available for Cycle 2.
  • Instrument operation and carefully planned
    observing and calibration strategies are designed
    to mitigate difficulties inherent to germanium
    detectors.
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