Transcript Document

IRTF POETS (Orange)
Preship review
Anticipated shipment date 22 APR 2008
Anticipated mounting 30 APR – 05 MAY 2008
18 April 2008, aasg
Outline
• Overview of POETS IRTF Project
• Lab testing results
• Packing plan
• Shipping Plan
• Mounting Plan
POETS IRTF team
MIT, Boston
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Amanda Gulbis (P.I.)
Jim Elliot (Co-I.)
Folkers Rojas (mechanical design and fabrication)
Mike Person & Matt Lockhart (instrument consultation & observers)
IfA, Hawaii
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Bobby Bus (observing and long term support)
John Rayner (optical design, SpeX interface)
Vern Stahlberger (mechanical design)
Lars Bergknut (mounting & work at summit)
Alan Tokunaga (IRTF division chief)
POETS IRTF Summary
• Our goal is to mount a high-speed, visible wavelength camera
system on the IRTF (NASA’s 3-m Infrared Telescope Facility)
• The instrument is based on existing MIT-Williams College POETS
(Portable Occultation, Eclipse, and Transit Systems)
• The instrument will be mounted on the side-facing exit window
of SpeX – a dichroic allows entry for light < 8000 Å or 9500 Å
• Fore-optics box uses 3:1 reducing optics to ret
f/9.32 beam and 60” FOV
POETS IRTF Overview
• Schematic of full setup
POETS IRTF Overview
• Schematic of full setup
• Optical path
POETS IRTF Components
• Fore-optics box (28 pieces, 1 mirror, 3 lenses, 1 filter wheel, 1
filter wheel motor, and assorted dowel pins and screws)
• Camera (Andor Ixon, 512 x 512 frame transfer BI E2V CCD with
16 m pixels; including power cable & computer cable)
• Computer (Shuttle; including power cord, PCI card, keyboard, &
mouse)
• GPS (Spectrum Inst.; including power supply, 25-m cable, control
cable, and antenna)
• Fore-optics box
• Camera
• Computer
Two computers are shown here -the top is a current POETS
machine. The bottom is the
IRTF machine, which we have
yet to get functioning properly
with the camera. We have
ordered a new computer, as
similar to the top machine as
we possible. If that machine
does not work, we will ship a
current POETS computer and
swap at a later date.
• GPS
Lab Testing
• Setup:
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All components assemble and disassemble as planned
Dowel pins are used for accurate alignment during assembly
No play in components once assembled
Light tightness can’t be tested until mounted – all components overlap
• Remaining issues:
• attachment to SpeX (was tested onsite)
• Manual shutter (functions, but attachment not tested)
• Instrument Computer (original system won’t work with the camera. new
system ordered, ETA at MIT 18 April 2008)
• Filter wheel (parts are in place, no filters or driving mechanism)
• Replacement lenses (lens 1 chipped at edges during initial fitting - doesn’t
seem to effect images, but spare lenses have been ordered)
Lab Testing
• Calibrations
• Cooling: TE cooler run for hours at -70º C at room temp
• Read Noise and Gain
• Were measured in lab prior to fore-optics box setup, are consistent
with spec. sheet
• Difficulties in obtaining accurate flatfields while camera is attached to
fore optics
Lab Testing
Lab Testing
• Vignetting
• Illuminated frames show slight vignetting at corners
• Vignetting pattern changes with adjustment of lens 2 & 3 positions, but
cannot be eliminated
Lab Testing
• As evenly illuminated as possible: note
vignetting (spots are dust on lenses)
Lab Testing
• Images
• Test charts placed at approximate TFP (0.3” in front of lens 1) can be made
to come into a clear focus
• Camera can be adjusted greater than 1” in z-extension for focusing
adjustment – threaded at 32 threads per inch to allow fine tuning
• No distortions are apparent across the image, centering looks OK – can’t
confirm without higher accuracy of TFP
Lab Testing
 Test charts placed at TFP 
 Images 
Packing Plan
• F. Rojas to be in charge of packing fore-optics box
• Preassembled, with lens mounts removed
• shipped in hard, ex-PCCD container
• All associated box hardware and camera cables can fit in this package
• Packages to ship
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Fore-optics box
GPS (packaged as shipped to us)
Computer (packaged as shipped to us)
Some possibility for consolidation (i.e. GPS may fit in fore-optics box)
Shipping Plan
• Online quote for DHL 2-day shipping from zip codes 02139 to
96720 is ~ $500 (100 lb. box with rough dimensions of our fore
optics box)
• Plan to ship no later than 23 April (Wed.) for mounting one week
later (30 April)
• If computer testing takes longer, can ship as late as the 25th
• Hand-carried components
• Camera
• Optics
Mounting Plan
B. Bus (observing, long term support), J. Rayner (SpeX
interfacing, testing), L. Bergknut (mounting, summit work),
A. Tokunaga (big problems)
Engineering Run Preparation
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Submitted plan to A. Tokunaga
Verified plan is reasonable with B. Bus
Completed ORF - requested lodging at PH and IRTF vehicle
Faxed Driver’s Clearance form
Contacted George Koenig re: instrument delivery
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• Confirmed DHL 2-day shipping will work
• Confirmed shipping address
Working on night plans for observations with C. Zuluaga
Engineering Run Preparation
Immediate to do
• Telecon with Hawaii to ensure we’re all on the same page
• Contact Miranda Hawarden-Ogata re: network interface
• Confirm engineering observing times
Longer term to do
• Compile documentation
• Engineering diagrams
• Setup and usage manual
Basic version for observers and more advanced for supporters
• Maintenance manual
The End
Slides on possible observing targets to follow
POETS IRTF Engineering Observations
• Calibrations
• On-telescope biases
• On-telescope flats (sky and dome)
• Focus
• standard star target?
• ensure co-focal with SpeX
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Image variations due to pointing
• Check variations with telescope pointing
• Check variations at different airmass
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Throughput & exp. times
• standard star target grid – range of stars from ~ 8 to
20 mag., B & R stars, versus range of exposure times
in conv.and EM modes
Engineering Observations II
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Possible science targets
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KBO and star for 06 May 2008 appulse
Other KBOs
Occultation candidate stars