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IGRINS Immersion GRating INfrared Spectrograph: Current Design. Sungho Lee Korea Astronomy and Space Science Institute ( KASI ) / Univ. of Texas at Austin ( UT )
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IGRINSImmersion GRating INfrared Spectrograph:Current Design Sungho Lee Korea Astronomy and Space Science Institute (KASI) / Univ. of Texas at Austin (UT) In-Soo Yuk (KASI), Moo-Young Chun (KASI), Soojong Pak (KHU), Hanshin Lee (UT), Chan Park (KASI), Joseph Strubhar (UT), Weisong Wang (UT), Casey Deen (UT), Michael Gully-Santiago (UT), Jared Rand (UT), Jung-Hoon Kim (SET), Won-Kee Park (SNU/KHU), Haingja Seo (KHU), Kang-Min Kim (KASI), Heeyoung Oh (KASI), Sang-On Lee (KASI), Marc Rafal (UT), Stuart Barnes (Univ. of Canterbury/UT), John Goertz (UT), John Lacy (UT), Tae-Soo Pyo (Subaru), Daniel T. Jaffe (UT)
IGRINS • High resolution IR spectrograph which can cover a broad wavelength range in a single exposure • IGRINS will be commissioned at the McDonald 2.7-m telescope, and also designed to be compatible with 4-8 m telescopes. • Spectral resolution • R=40,000 (3.66 pixel sampling) • Wavelength coverage • H-band : 1.49~1.80 µm (25 orders) • K-band : 1.96~2.46 µm (22 orders) • Slit dimension
Design Concept Model of IGRINS on 2.7m • Cross-dispersed echelle spectrograph • Main disperser : silicon immersion grating (R3, 36.5 l/mm) • Cross disperser : VPH gratings (H: 650 l/mm, K: 400 l/mm) • High sensitivity • Silicon immersion grating • VPH gratings • HAWAII-2RG (2048x2048) detectors • Compact (0.9 x 0.6 x 0.4 m) • Silicon immersion grating • VPH gratings • White pupil optical design • Simple and reliable operation • No cold moving parts in the spectrograph • Only switching mechanism for the calibration sources
Optical Design Layout • Collimated beam size = 25 mm • Slit size = 0.13 mm x 1.94 mm
Spectrograph Optical Performance H-band K-band • Geometric spot diagram across the spectra • Squares: 2 x 2 pixels (36 x 36 micron) • Circles: Airy disk size • Optical quality does not degrade spectral resolution
Input Relay Optics Circle: Airy disk size • 1 arcsec seeing disk image through the input optics at the slit mirror • 4.4 arcsec per size • Left: Center of the slit • Middle: One edge of the slit • Right: One corner of the 2 x 2 arcmin field Convert a telescope f-ratio (f/9-f/16) to f/10 Provide a cold stop to prevent thermal radiation Deliver 2 x 2 arcmin FOV to the slit-viewing/guiding camera
Slit-Viewing Camera • 1 arcsec seeing disk image through the input optics • and slit viewer • 4.4 arcsec per size • Left: Center of the slit • Middle: One edge of the slit • Right: One corner of the 2 arcmin x 2 arcmin field Target acquisition and slit monitoring Offset guiding in a 2 x 2 arcmin FOV at the 2.7-m telescope Use 1024 x 1024 clean area of an Engineering Grade H2RG Ks-band filter
Immersion Grating • Outstanding capability of IGRINS in the compact design comes from the silicon immersion gratings. • The high refractive index (n=3.4)of silicon keep the high spectral resolution with a much smaller beam size. • Silicon lithography can make a very coarse grating which enables continuous spectral coverage.
IGRINS Immersion Grating • Silicon R3 grating (10 cm) • Spectral ghost < 0.3% (~5 nm periodic error) • Spectral grass ~10-5 (scattering at groove surfaces) • Will make another grating • Choose and cut into the shape
VPH Gratings • Volume Phase Holographic grating • Cross-dispersers in each H and K band spectrograph • Advantages of VPH gratings over conventional gratings • Higher efficiency by less scatters • Enabling compact optical systems by transmission configuration • High durability and easy handling • Has been used in optical and NIR (H-band) spectrographs • We have purchased H-VPHGs which show good performances.
IR VPH Grating Test Performance verification K-band grating development in collaboration with KOSI Thermal cycling tests
Mechanics – Cyrostat Input relay optics Slit-viewing camera Size of the cryostat : 900 x 600 x 400 mm Total mass : 210 kg Compactness minimizes the flexure issue All access from the bottom of the cryostat Optical bench is mounted on the bottom plate and thermally isolated by G10 supports
Cyrostat – Structual Analysis • Mostly looking upward to the straight Cassegrain focus • Deflection is < 10 um at the G10 supports • Corrected out by focussing and guiding
Mechanics – Camera Barrels Radial spring 3 Baffle Plates Axial spring Radial spring Radial Spring Built in Baffle Axial spring Axial Spring M3 screws with helicoil Precision Pin Bent Holes • Camera is the most sensitive • Design it first to minimize risk • 3+1 baffle vanes • 3-point kinematic mount • Springs for thermal expansion
Mechanics – Detector Mounts Thermal insulation Cryo ASIC Board Flex Cable Cold Strap from ASIC board • Flex cable to the outside electronics • H2RG & ASIC thermally isolated from the optical bench Cold Strap from H2RG H2RG
Mechanics – Telescope Mount • 4-point structure • Only translation on the FP • Same mount for 2.7 m and Gemini
Cryogenics 2 rubber springs Metal bellows Vibration isolation design • Operating temperature • Optical bench and optics : 130 K • Detectors : 77 K • Temperature stability control • Silicon immersion grating : ±0.06 K • Detector : ±0.1 K • Optical bench : ±1 K • The temperature will be monitored at least at six positions • Cold head, optical bench, radiation shield, input optics, two spectrograph cameras
Detector Testing • Collaboration with WIFIS at Univ. of Toronto • ROIC functional test is ongoing • Cryogenic EG detector test in this year • Test at KASI • Test dewar design • Cryogenic test at KASI next year
Electronics Architecture • IP based control system (each device has an IP address) • Standard SW protocols and HW devices • System can evolve as needed.
Software Architecture • Standard observing scenarios • Software Requirements Document • Software Specification Document: working for each SW package
Calibration Unit • Line Calibration : • Th-Ar lamp or Uranium lamp • OH emission lines • Telluric absorption lines • Continuum Calibration : • Tungsten-halogen lamp • Compatible with f/8 ~ f/16 telescopes • Considering an absorption gas cell for future RV programs
Integration and Test – Lab Setup and Handling Plan • Clean room, optical bench, interface • Multi-purpose cart • Storage and transportation • Telescope installation
Overall Alignment Procedure Module Alignments (Warm) [M1] Input-relay lens module [M3] H & K camera lens module [M2] Slit-viewer lens module [M5] Optical bench assembly Warm Test [Sb1] Input-relay optics [Sb2] Slit-viewer optics [Sb3] Spectrograph reflective optics Cold Test [Sb4] Slit-viewer system [Sb5] Input+Slitviewersystem [Sb6] Spectrograph system [M4] Calibration optics System Alignments (Cold) [S1] Instrument alignment [S2] Telescope alignment
Fabrication & Alignment Plan Fabricate and test H & K camera lenses Fabricate and test dispersion part components Correct positions of H & K cameras + detectors Correct design of M2 mirror mount Correct design of H & K camera barrels Fabricate H & K camera barrels Fabricate dispersion part mounts Assemble and align H & K camera barrels Assemble and align dispersion part (compensator: M2 mirror) Assemble and align dispersion part + camera barrels + detectors (compensator: detector assembly)
Future Work • Overall timeline • PDR : 2009. 12 • Camera CDR : 2010. 11 • Main CDR : 2011 (TBD) • Commissioning : 2012. 11 (TBD) • Tasks for the Camera CDR • Camera lens barrel design • Scattered light and ghost analysis • Revise engineering requirements: OCDD, FPRD, error budget • Revise I/T plan, acceptance test plan, alignment plan