FLITECAM: The first light camera for SOFIA Amanda Mainzer, I. S. McLean, T. Aliado, E. E. Becklin, G. Brims, J. Goulter, E. Kress, N. Magnone, J. Milburn,

Slides:



Advertisements
Similar presentations
MMIRS 1 MMIRS MMT and Magellan Infrared Spectrograph Brian McLeod.
Advertisements

Observational techniques meeting #7. Detectors CMOS (active pixel arrays) Arrays of pixels, each composed on a photodetector (photodiode), amplifier,
Magnet Cooldown Scheme 17 th February 2012 Roy Preece (STFC RAL)
PACS IHDR 12/13 Nov 2003 Photoconductor Detector Modules 1 IHDR ASTEQ-GmbH Germany Peter Dinges, Michael Harr, Heribert Krüger, Hilmar Richter, Bernd Zimmermann.
Test Cryostat, OGSE and MGSE PACS IHDR: MPE 12/13 Nov 2003 AIV1 PACS Test Cryostat, OGSE and MGSE Gerd Jakob MPE.
NGAO Instrumentation Overview September 2008 Updated Sean Adkins.
M2FS: Michigan/Magellan Fiber System. M2FS (Michigan/Magellan Fiber System) Fiber-fed MOS w/2 independent and identical spectrograph arms 256 total fibers.
Grism Spectroscopy with FLITECAM Erin C. Smith (UCLA) Ian S. McLean (UCLA)
IRMS Optical Subsystem Review. The Charter Confirm that the MOSFIRE design is a feasible baseline for IRMS (yes) Verify that the MOSFIRE design can achieve.
1 NLST – National Large Solar Telescope India’s Plan for a New, Large Solar Telescope D. Soltau (KIS), Th. Berkefeld (KIS), M. Süß (MTM), H. Kärcher (MTM)
NGAO NGS WFS design review Caltech Optical Observatories 31 st March 2010.
SWIFT Team University of Oxford 12 th November 2007O-SWIFT Progress Report Fraser Clarke.
PLATO kick-off meeting 09-Nov-2010 PLATO Payload overall architecture.
1.B – Solar Dynamo 1.C – Global Circulation 1.D – Irradiance Sources 1.H – Far-side Imaging 1.F – Solar Subsurface Weather 1.E – Coronal Magnetic Field.
F444W F300M F277W F356W F480M F335M F360M F460M F410M F430M LWF1 LWF2 LWF3 LWF4 LWF5 LWF6 LWF7 LWF8 LWF9 LWF10 LWF11 LWF12 F322W2 LWF F250M Imaging pupil.
The background for this poster shows a life size drawing of one NIRCam module. The other side is a mirror image. The two modules are mounted back-to-back.
Constellation Orion Visible Light Constellation Orion Infrared Light.
MMT Magellan Infrared Spectrograph ( MMIRS ) P.I. Brian McLeod Warren R. Brown SAO/CfA.
1 Aurélien Barrau LPSC-Grenoble (CNRS / UJF) A few words on the LPSC The LPSC in few words: The scientific environment : Grenoble 4 Universities.
Summer Fun with Optics Stephen Muchovej UC Berkeley CARA - REU Program.
KMOS Instrument Science Team Review Instrument overview.
SOFIA — The Observatory open cavity (door not shown) TELESCOPE pressure bulkhead scientific instrument (1 of 7) Scientist work stations, telescope and.
Integration and Alignment of Optical Subsystem Roy W. Esplin Dave McLain.
Berkeley workshop summary Redundancy : dual detector Field of view : 3”x6” Spectrograph length goal: < 400 mm Isostatic mount on the base plate with control.
1 Engineering the James Webb Space Telescope Paul Geithner JWST Deputy Project Manager - Technical March 26, 2011.
Corner Raft Test Station Kirk Arndt, Ian Shipsey Purdue University LSST Camera Workshop SLAC Sept , 2008.
Engineering: NAHUAL Ireland Acquisition Camera, Focal Plane Mechanisms and Layout Tully Peacocke, National University of Ireland Maynooth Carlos del Burgo,
STATUS REPORT OF FPC SPICA Task Force Meeting March 29, 2010 MATSUMOTO, Toshio (SNU)
1 FRIDA Engineering Status 17/05/07 Engineering Status May 17, 2007 F.J. Fuentes InFraRed Imager and Dissector for Adaptive Optics.
AMICA Antarctic Multiband Infrared CAmera Favio Bortoletto INAF – Osservatorio Astronomico di Padova on behalf of the AMICA collaboration Telescope and.
NIRCam ETU Testing at LMATC, Palo Alto Kailash C. Sahu.
SCI (SPICA coronagraph instrument) Keigo Enya & SCI team.
NORDFORSK Summer School, La Palma, June-July 2006 NOT: Telescope and Instrumentation Michal I. Andersen & Heidi Korhonen Astrophysikalisches Institut Potsdam.
SPS Synchrotron Light Monitor -BSR- Status G. TRAD E. Bravin, A. Goldblatt, F. Roncarolo.
MIRI Optical System CDR, 6 th & 7 th December 2006 Mid InfraRed Instrument 07-1 Optical System Critical Design Review (CDR) TIPS Presentation: Margaret.
The FMOS Facility for the SUBARU telescope Gavin Dalton Oxford/RAL.
The Prime Focus Imaging Spectrograph Design and Capabilities
Calibration of the LSST Camera Andy Scacco. LSST Basics Ground based 8.4m triple mirror design Mountaintop in N. Chile Wide 3.5 degree field survey telescope.
Test Readiness Review 23 October 2003 CRAL - LYON.
SPACE TELESCOPE SCIENCE INSTITUTE Operated for NASA by AURA MIRI VM2 Testing Scott Friedman and the MIRI Test Team (special thanks to Paul Eccleston, Alistair.
A Modular K-Band Focal Plane Array for the Green Bank Telescope Matt Morgan National Radio Astronomy Observatory 9/28/2007.
Binospec - Next Generation Optical Spectrograph for the MMT
Preliminary Foreoptics Design for FASOT of 2nd Generation L. Chang, X.M Cheng
System Performance Metrics and Current Performance Status George Angeli.
Astronomical Observational Techniques and Instrumentation
Extended Detector Cutoff Considerations WFIRST Project Office May
1 FLITECAM December 11, 2008 Ian McLean (Principal Investigator) UCLA Infrared Laboratory University of California, Los Angeles.
1 FLITECAM April 28, 2009 Ian McLean (Principal Investigator) UCLA Infrared Laboratory University of California, Los Angeles.
Introduction NICMOS (Near-Infrared Camera and Multi-Object Spectroscopy) was installed on the Hubble Space Telescope during SM2 in 1997 and has been the.
FourStar Status SAC Meeting 13mar2010 Persson, Murphy, Birk, Monson, Kelson, Uomoto.
PACS IBDR MPE 27/28 Feb 2002 AIV 1 PACS IBDR Test Cryostat and OGSE Gerd Jakob MPE.
1 Harvard-Smithsonian Center for Astrophysics Magellan SAC 9/04 MMIRS Status Report Brian McLeod.
N A S A G O D D A R D S P A C E F L I G H T C E N T E R I n s t r u m e n t S y n t h e s i s a n d A n a l y s i s L a b o r a t o r y APS Formation Sensor.
MPI Semiconductor Laboratory, The XEUS Instrument Working Group, PNSensor The X-ray Evolving-Universe Spectroscopy (XEUS) mission is under study by the.
MMIRS 1 Harvard-Smithsonian Center for Astrophysics Magellan SAC 9/05 MMIRS Status Upate Presented by A. Szentgyorgyi P.I. B. McLeod.
Date 2007/Sept./12-14 EDR kick-off-meeting Global Design Effort 1 Cryomodule Interface definition N. Ohuchi.
Astronomical Spectroscopic Techniques. Contents 1.Optics (1): Stops, Pupils, Field Optics and Cameras 2.Basic Electromagnetics –Math –Maxwell's equations.
MagIC Upgrade for High-Speed Photometry Jim Elliot, MIT Magellan SAC
S A Griffiths CM42 June 2015 Electrical & Control.
Teleconf ACS – FREIA 28th March 2017
Telescope Assembly, Integration and Verification (AIV) WBS 04C. 14 J
Astronomical Spectroscopic Techniques
SOFIA — The Observatory
Single Object & Time Series Spectroscopy with JWST NIRCam
David Montanari / Johan Bremer Jun 11, 2015 Rev. 1
When to use them, why you should use them, and how they work!
Launch and On-orbit Checkout
FourStar 4K x 4K JHK imager
Optics Alan Title, HMI-LMSAL Lead,
Instrument Overview Larry Springer HMI Program Manager
Presentation transcript:

FLITECAM: The first light camera for SOFIA Amanda Mainzer, I. S. McLean, T. Aliado, E. E. Becklin, G. Brims, J. Goulter, E. Kress, N. Magnone, J. Milburn, G. Skulason, M. Spencer UCLA SPIE 27 August 2002

AKM 2 SPIE 27 Aug FLITECAM Team Dr. Ian McLean, Principal Investigator Amanda Mainzer, Instrument Scientist Ted Aliado, Mechanical/Fabrication Dr. Eric Becklin, SOFIA Project Scientist George Brims, Systems Engineering John Goulter, Mechanical/Regulatory Evan Kress, Mechanical Nick Magnone, Mechanical/Fabrication John Milburn, Software Gunnar Skulason, Electronics Michael Spencer, Electronics UCLA:

AKM 3 SPIE 27 Aug FLITECAM Summary First Light Test/Experiment CAMera/ for SOFIA Features: –1- 5 µm with InSb 1024 x 1024 array –FOV: 8´ diameter (inscribed on detector) –Scale: 0.47´´ per pixel –LHe/LN 2 system –Grism Spectroscopy (R~2000) –Co-mounts with HIPO First light: ~Q (ground based) Delivery to SOFIA: Q Must be fully FAA certified Y(side) X(aft) Z(up)

AKM 4 SPIE 27 Aug FLITECAM’s Field of View Originally going to use 512x512 array Between PDR and CDR, switched to 1024x1024 array to image the entire 8 arcmin SOFIA field of view

AKM 5 SPIE 27 Aug Optics Modes: - Imaging - Grism (R~2000) - Pupil viewing Optical design: - Collimator triplet - F/5 imaging camera - 4 fold mirrors - Dual filter wheel - 3 pupil viewing lenses - Filters: ZJHKK’LM + selected narrow band

AKM 6 SPIE 27 Aug Image Quality SOFIA seeing ~2-3 arcsec FLITECAM PSF: arcsec across entire 8 arcmin field of view FLITECAM designed to fully evaluate SOFIA image quality Box = 2x2 pixels 1 pixel = 0.47 arcsec

AKM 7 SPIE 27 Aug Thermomechanical Optical Design Large crystal lenses have to be cooled in controlled fashion to avoid thermomechanical shock Collimator: LiF, BaF 2, ZnS all with diameter ~165 mm Spring-loaded “finger” mounts isolate lenses and prevent thermomechanical shock Lenses manufactured by Brad Picirillo of Optical Solutions Inc. of New Hampshire LiF lens Spring-loaded “fingers”

AKM 8 SPIE 27 Aug Thermomechanical Performance Large LiF and BaF2 lenses particularly susceptible to thermal & mechanical shock Spares difficult & expensive to obtain - 9 month lead time! To verify success of our mounting/thermal isolation scheme, we constructed a dummy collimator

AKM 9 SPIE 27 Aug Dummy Collimator 77 K end Thermometers: front center, front edge, back edge LiF spare lens Glass blanks ~165 mm Brad Picirillo of OSI provided spare unpolished LiF lens for dummy collimator Put in two additional glass blanks to simulate thermal characteristics of BaF 2 and ZnS lenses Epoxied thermometers to spare LiF: front/back center, and front edge Additional thermometers on collimator housing and optical baseplate This allowed us to monitor gradients vs. cooldown rate

AKM 10 SPIE 27 Aug Thermomechanical Optical Design cont’d. Cooldown rates controlled by isolating selected components with G10 Time constants calculated and measured to determine safe rates Thanks to Brad Picirillo of OSI for providing spare LiF! Will eventually test spare LiF to destruction Results show that cooldown rates of up to 13 K/hr are safe! Edge to center gradient Front center to back center gradient

AKM 11 SPIE 27 Aug Warm First Light To avoid long iterative cryogenic cycles, found focus warm Confirmed warm focus with warm Zemax optical model Warm best focus location agreed with warm focus model to within depth of focus Set focus to predicted cold focus location

AKM 12 SPIE 27 Aug Completed Software Java  platform- independent Software controls temperature sensors, vacuum gauge, helium level sensor, detector heater, and mechanisms Astronomical Observation Requests (AORs) will be written using a modified version of SPOT (SIRTF Planning and Observation Tool)

AKM 13 SPIE 27 Aug Electronics Detector head and electronics purchased from Mauna Kea Infrared These systems are being packaged into 19” racks for ground-based operations: – Data acquisition system – Mechanism controllers – Temperature controllers – Pressure monitors – LHe level monitor – Power controller Multiplexer CW Rack SHARC Processor On-Cryostat Electronics

AKM 14 SPIE 27 Aug Cryogenics LN2/LHe cryostat manufactured by Precision Cryogenics of Indianapolis, IN 20 L of LN2, 20 L of LHe FAA regulations: cryostat can only be filled when plane is on the ground Will fill before each night’s observing Cylindrical design dictated by SOFIA volume allocation Cryostat can either look up or horizontal - can be used on ground

AKM 15 SPIE 27 Aug DAR witnessed testing at PCI on 28 March 2002 LN 2 Container Pressure Test measuring the deformation of container under pressure checking conformance with drawings FLITECAM FAA Cryogen Container Testing

AKM 16 SPIE 27 Aug FLITECAM Assembly

AKM 17 SPIE 27 Aug Milestones

AKM 18 SPIE 27 Aug Commissioning Three fall observing runs scheduled at 3-m Shane Telescope at Lick Observatory Shane telescope’s F/17 optics well-matched to SOFIA’s F/19.6 First run starts Sept. 13! Will observe a variety of star forming regions Observations will constitute part of A. Mainzer’s Ph.D. thesis