HIPO
| Name of Instrument: |
HIPO -
High Speed Imaging Photometer for Occultation |
| Instrument type: |
High-speed Imaging Photometer
0.3 - 1.1 microns |
| Principal Investigator: |
Dr. Edward W. Dunham; dunham@lowell.edu
Lowell Observatory
1400 West Mars Hill Road
Flagstaff, AZ 86001 |
| Co-Investigator: |
Dr. James L. Elliot
Massachusetts Institute of Technology
77 Massachusetts Avenue, Bldg. 54-422
Cambridge, MA 02139 |
|
Contact the SOFIA help-desk |
Scientific/Technical Abstract:
HIPO is a special-purpose science instrument for SOFIA that is designed
to provide simultaneous high-speed time resolved imaging photometry at two optical
wavelengths. It will be possible to mount HIPO and FLITECAM on the SOFIA telescope
simultaneously to allow data acquisition at two optical wavelengths and one near-IR
wavelength. HIPO has a flexible optical system and numerous readout modes,
allowing many specialized observations to be made. The instrument characteristics
required for our proposed scientific pursuits are closely aligned to those needed for
critical tests of the completed SOFIA Observatory, and HIPO will be used heavily for
these tests. The general design and performance goals of the instrument are described
in the 2004 paper in the references below.
Our main scientific interest is in the use of HIPO for observing
stellar occultations. In a stellar occultation, a star serves as a small probe of the
atmospheric structure of a solar system object or the surface density structure of a
planetary ring or comet. Such observations provide information at high spatial
resolution that would otherwise require a space mission to obtain. This work makes use
of SOFIA's mobility, freedom from clouds, and near-absence of scintillation noise to
provide the best possible occultation data.
The low atmospheric scintillation in airborne photometry gives HIPO the
potential to detect P-mode stellar oscillations in sunlike stars and will provide
excellent photometry of stellar transits by extrasolar planets. HIPO will be available
for Guest Investigator use on a collaborative basis, and potential Guest Investigators
should contact the PI prior to proposing to insure that the proposed observations are
feasible and make the best use of HIPO 's capabilities.
HIPO Performance Summary:
The instrument sensitivity and resolution summaries are provided to
permit estimating feasibility of scientific investigations. The HIPO performance
summaries show the expected system performance for Full Operational Capability, which
may differ from that during commissioning.
HIPO Optical Design:
The HIPO optical system is reconfigurable to meet its varied
requirements. It incorporates two dichroic beamsplitters, one to divert the
infrared beam to FLITECAM (if mounted) and one to split the red and blue sides of
the HIPO optical paths. Either or both of these may be removed if desired. It is
also possible to move either CCD so it is placed directly at the optimal SOFIA focal
plane for highest spatial resolution and throughput. The optical design is
described in detail in the 2003 paper in the references
below.
The 8-position filter wheels are located near the pupil image formed
by the collimator optics. Two positions in the red CCD's filter wheel are normally
used for Shack-Hartmann lenslet arrays, but these may be replaced if necessary for a
particular observation. We have contemplated adding grism capability to HIPO but
have not yet carried this out.
The region between the mounting flange and the gate valve on the
telescope can be evacuated to reduce image degradation due to density fluctuations
in this region of the optical path.
HIPO provides a number of CCD readout modes as described in the 2008
paper in the references below. The most commonly used are
the single frame mode and a frame transfer time series (basic occultation) mode with
readout frequency up to 50 Hz. A variety of readout rates are available allowing the
observer to optimize the subframe size, speed, noise, full well, and linearity
tradeoff for a particular event.
HIPO Angular Resolution
The primary HIPO detectors are e2v CCD47-20 1024 x 1024 pixel frame
transfer CCDs with plate scales of 0.33" x 0.33" pixels at low resolution
and 0.05" x 0.05" pixels at high resolution. The HIPO field of view (FOV)
is a 5.6' square, the 8' diagonal of which corresponds to the 8' diameter SOFIA FOV.
Pixels will normally be binned to best match the seeing blur size and to reduce the
effect of read noise. The high resolution mode includes no reimaging optics. (It is
possible to replace one or both of the CCD47's with CCD67's having half the field of
view, twice the pixel size, and much faster imaging operation.
The figure below shows the expected instrument FWHM beam diameter as
a function of wavelength. It is expected to be dominated by seeing and image motion
effects. The red curve in this figure is the nominal image quality expected at first
light for SOFIA, based on the expected shear layer seeing, the as-built optical
performance, and 2" rms image motion. The blue curve represents the ultimate
combined optical quality and image motion requirement (80% encircled energy in a
1.6" diameter circle) convolved with the expected shear layer seeing. Also
plotted are representative photometry aperture diameters likely to be used for
processing occultation frames under both conditions described above. The image
motion assumed is larger than will be experienced when observing at high frame
rates. Occultation photometry will be extracted from data frames using effective
aperture sizes comparable to the 80% enclosed light diameter plotted here.
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HIPO Spectral Passbands and Filter Characteristics
Wavelength range: 0.3 - 1.1 µm. HIPO currently includes standard
Johnson UBVRI filters that will be used primarily for facility performance testing.
Occultation observations will normally be unfiltered for events involving faint
stars or will use specialized filters such as the narrow-band methane filter
(λc ~ 0.89 µm) for events with bright stars. Additional
custom filters will be added for specific events.
HIPO uses a dichroic reflector to separate its blue and red
channels. Two dichroics are currently available with transition wavelengths of
0.575 and 0.675 µm respectively. Other dichroics will be added as necessary
for specific events.
Below is a plot of the HIPO total system throughput for each of the
available bandpasses. The dichroic response in the figures shown below is only an
example, assuming a transition wavelength of 0.62 µm. This figure assumes that
the FLITECAM dichroic beamsplitter is not installed.
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HIPO Sensitivities
Below are shown HIPO first-light sensitivities for several
representative cases. These figures assume that the FLITECAM dichroic beamsplitter
is not installed. The upper figures correspond to occultations by Pluto or Triton
while the lower two are for the case of a very faint occulting object. The left and
right figures are for 0.5 sec and 50 ms integrations, respectively. Each figure
shows S/N for no filter (dichroic only) and for the dichroic plus standard Johnson
filters. The dichroic transition is assumed to occur from 0.57 and 0.67 µm.
The deviation of S/N from a square root dependence is mostly due to
shot noise on the occulting object in the top two figures, mostly to shot noise on
the sky in the bottom left figure, and mostly to read noise in the bottom right
figure. The improved final SOFIA pointing stability will increase sensitivity for
sky-limited events and improve discrimination from nearby bright objects (e.g.
Neptune for a Triton occultation).
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HIPO Observation Preparation and Data Handling
Once the observatory has been fully commissioned, additional
information will be provided, including a full accounting of overheads associated
with particular instrument set-ups and observing strategies; information on
preparing observations using the SPT; and details regarding data formatting,
calibration, and reduction.
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Disclaimer
All sensitivity and resolution data are preliminary,
and based on anticipated performance of the observatory and the
instrument. Actual performance of the SOFIA telescope and
instrument combination will be established after flight operations
begin. Telescope performance is expected to be upgraded during
the first two years, and instrument performance may be upgraded,
or additional modes or capabilities may be added.
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Additional References:
Dunham et al., "HIPO data products," Ground-based and Airborne Instrumentation for
Astronomy II, Ian S. McLean, Editor, Proc. SPIE 7014, 70144Z (2008),
DOI: 10.1117/12.788040 [pdf]
Dunham et al., "HIPO: a high-speed imaging photometer for occultations,"
Ground-based Instrumentation for Astronomy, Alan F. M. Moorwood & Masanori Iye, Editors,
Proc. SPIE 5492, 592 (2004),
DOI: 10.1117/12.552152 [pdf]
E. W. Dunham, "The optical design of HIPO: a high-speed imaging photometer for
occultations," Airborne Telescope Systems II, Ramsey K. Melugin & Hans-Peter Roeser,
Editors, Proc. SPIE 4857, 62 (2003),
DOI: 10.1117/12.458819 [pdf]
Dunham, et al., "SOFIA image motion compensation," Ground-based and Airborne Instrumentation for Astronomy III, Ian S. McLean, Suzanne K. Ramsay, & Hideki Takami, Editors, Proc. SPIE 7735, 77355X (2010), DOI: 10.1117/12.857731 [pdf]
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