Instrument Characteristics

Similar documents
Inverted-COR: Inverted-Occultation Coronagraph for Solar Orbiter

LYOT: LYman Orbiting Telescopes

COST Short Term Scientific Missions Report 24 July 2014

An integral eld spectrograph for the 4-m European Solar Telescope

GPI INSTRUMENT PAGES

instruments Solar Physics course lecture 3 May 4, 2010 Frans Snik BBL 415 (710)

The Field Camera Unit for WSO/UV

Observational Astronomy

BEAM HALO OBSERVATION BY CORONAGRAPH

OPAL Optical Profiling of the Atmospheric Limb

Fast Solar Polarimeter

MONS Field Monitor. System Definition Phase. Design Report

Design parameters Summary

Historical. McPherson 15 Mount

PHY 431 Homework Set #5 Due Nov. 20 at the start of class

Chapter 34 The Wave Nature of Light; Interference. Copyright 2009 Pearson Education, Inc.

The predicted performance of the ACS coronagraph

Light gathering Power: Magnification with eyepiece:

TOWARD A NEXT GENERATION SOLAR CORONAGRAPH: DIFFRACTED LIGHT SIMULATION AND TEST RESULTS FOR A CONE OCCULTER WITH TAPERED SURFACE

INAF Osservatorio astronomico di Torino Technical Report nr. 153

Optical design of Dark Matter Telescope: improving manufacturability of telescope

12.4 Alignment and Manufacturing Tolerances for Segmented Telescopes

STRAYLIGHT TESTS FOR THE HELIOSPHERIC IMAGERS OF STEREO

Lecture 7: Op,cal Design. Christoph U. Keller

Ultralight Weight Optical Systems using Nano-Layered Synthesized Materials

The Asteroid Finder Focal Plane

!!! DELIVERABLE!D60.2!

Water-Window Microscope Based on Nitrogen Plasma Capillary Discharge Source

GMT Instruments and AO. GMT Science Meeting - March

X-ray generation by femtosecond laser pulses and its application to soft X-ray imaging microscope

Southern African Large Telescope. Prime Focus Imaging Spectrograph. Polarimetric Optics Design Study

The Wide Field Imager

The Advanced Spectroscopic and Coronagraphic Explorer: science payload design concept

Spatially Resolved Backscatter Ceilometer

BAFFLES DESIGN OF THE PROBA-V WIDE FOV TMA

Optical Design of an Off-axis Five-mirror-anastigmatic Telescope for Near Infrared Remote Sensing

Experiment 1: Fraunhofer Diffraction of Light by a Single Slit

erosita mirror calibration:

Hyperspectral Imager for Coastal Ocean (HICO)

OPTICS OF SINGLE BEAM, DUAL BEAM & ARRAY RECEIVERS ON LARGE TELESCOPES J A M E S W L A M B, C A L T E C H

Starshade Technology Development Status

EE119 Introduction to Optical Engineering Spring 2003 Final Exam. Name:

Predicting the Performance of Space Coronagraphs. John Krist (JPL) 17 August st International Vortex Workshop

Will contain image distance after raytrace Will contain image height after raytrace

Simulations of the STIS CCD Clear Imaging Mode PSF

Solar Optical Telescope (SOT)

Science Detectors for E-ELT Instruments. Mark Casali

Reflectors vs. Refractors

A Possible Design of Large Angle Beamstrahlung Detector for CESR

Optical Design. Instrument concept Foreoptics and slit viewer Spectrograph Alignment plan 3/29/13

Chapter 5 Nadir looking UV measurement.

For rotationally symmetric optical

Bruce Macintosh for the GPI team Presented at the Spirit of Lyot conference June 7, 2007

Detectors that cover a dynamic range of more than 1 million in several dimensions

Phys 531 Lecture 9 30 September 2004 Ray Optics II. + 1 s i. = 1 f

October 7, Peter Cheimets Smithsonian Astrophysical Observatory 60 Garden Street, MS 5 Cambridge, MA Dear Peter:

NIRCam Optical Analysis

Gemini 8m Telescopes Instrument Science Requirements. R. McGonegal Controls Group. January 27, 1996

Physics 431 Final Exam Examples (3:00-5:00 pm 12/16/2009) TIME ALLOTTED: 120 MINUTES Name: Signature:

High Contrast Imaging

Telescopes and their configurations. Quick review at the GO level

Applications of Steady-state Multichannel Spectroscopy in the Visible and NIR Spectral Region

SPRAY DROPLET SIZE MEASUREMENT

EUV Plasma Source with IR Power Recycling

Exam 4. Name: Class: Date: Multiple Choice Identify the choice that best completes the statement or answers the question.

On-line spectrometer for FEL radiation at

New Optics for Astronomical Polarimetry

Electromagnetic Radiation

System/Prescription Data

Radiometric Solar Telescope (RaST) The case for a Radiometric Solar Imager,

Corner Rafts LSST Camera Workshop SLAC Sept 19, 2008

CHARA Collaboration Review New York 2007 CHARA Telescope Alignment

ECEN. Spectroscopy. Lab 8. copy. constituents HOMEWORK PR. Figure. 1. Layout of. of the

Chapter Ray and Wave Optics

Optical Components for Laser Applications. Günter Toesko - Laserseminar BLZ im Dezember

Commissioning of Thomson Scattering on the Pegasus Toroidal Experiment

Ground-based Solar Optical Observations

Oriel MS260i TM 1/4 m Imaging Spectrograph

A LATERAL SENSOR FOR THE ALIGNMENT OF TWO FORMATION-FLYING SATELLITES

The below identified patent application is available for licensing. Requests for information should be addressed to:

1/8 m GRATING MONOCHROMATOR

INTRODUCTION THIN LENSES. Introduction. given by the paraxial refraction equation derived last lecture: Thin lenses (19.1) = 1. Double-lens systems

ZIMPOL-3: a powerful solar polarimeter

3.0 Alignment Equipment and Diagnostic Tools:

Optics for the 90 GHz GBT array

Final Feed Selection Study For the Multi Beam Array System

UltraGraph Optics Design

Lecture 2: Geometrical Optics. Geometrical Approximation. Lenses. Mirrors. Optical Systems. Images and Pupils. Aberrations.

MIRI The Mid-Infrared Instrument for the JWST. ESO, Garching 13 th April 2010 Alistair Glasse (MIRI Instrument Scientist)

Coronal and heliospheric imaging instrumentation development at RAL Space

Optical basics for machine vision systems. Lars Fermum Chief instructor STEMMER IMAGING GmbH

ADVANCED OPTICS LAB -ECEN Basic Skills Lab

UNIVERSITY OF HAWAII Institute for Astronomy. f/31 High Angular Resolution Imaging Spectrograph HARIS USER MANUAL update June 10, 1997

Use of Computer Generated Holograms for Testing Aspheric Optics

ADVANCED OPTICS LAB -ECEN 5606

Southern African Large Telescope. Prime Focus Imaging Spectrograph. Optics Design

Southern African Large Telescope. Prime Focus Imaging Spectrograph. Instrument Acceptance Testing Plan

Exercise 8: Interference and diffraction

Selecting an image sensor for the EJSM VIS/NIR camera systems

NGAO NGS WFS design review

Transcription:

II Workshop Instrument Characteristics Marco Romoli Torino, 12-13 dicembre 2012

In order to meet the requirements: Coronal Imaging Wavelength range Spatial Resolution Field-of-view VL: 580-640 nm UV: 121.6 10.0 nm 20 arcsec 1.5-2.9 annular, off-limb corona Instrumental Stray Light (Bcor/B ) VL <10 9 UV <10 7 instrument is an externally occulted coronagraph (with inverted occultation) with imaging capabilities.

consists of two units: Optical Unit (MOU) Processing & Power Unit (MPPU)

de-scoping from PDR (April 2012) to fulfill mass, cost requirements ant to reduce complexity: External Re-pointing Mechanism (ERM) Internal Door Mechanism (IDM) EUV imaging channel Filter Insertion Mechanism (FIM) Spectroscopic channel Filter Insertion Mechanism (FIM) UVD door mechanism Grating Slit assembly (Sun-sensor) (Internal Occulter Mechanism (IOM))

Optical Unit (MOU) Boom Occulter Assembly (BOA) On-axis Gregorian Telescope for for UV, VL imaging (with Al/MgF 2 coated mirrors) S*

MOU sub-systems Optics Mechanisms Detectors M0 Sun sensor Lyot M2 Stop Internal Occulter Mechanism M1 UVD VLD VL Polarimeter

Optical Design: IMAGING optical design: IMAGING

Mechanisms: IOM Internal Occulter Mechanism (IOM) IO stops diffraction from IEO edge IEO IO re-alignment If IOM is descoped IO will change size (smaller radius) increasing the lower edge of FOV by 0.15 R @ 0.28 AU

Polarimeter assembly The polarimeter consists of: Polarimetric Optical System (POS) The POS electro-optically modulates the intensity of the linearly polarized K-corona. The POS is a polarization optics in Senarmont configuration : Bandpass (BP) filter (580-640 nm); Fixed Quarter-Wave (QW) retarder; Polarization Modulation Package (PMP) with a LCVR cell (Liquid Crystal Variable Retarder); Linear Polarizer (LP). Relay-Optics System (ROS) The ROS gives a 1:1.2 magnification ratio to match the telescope plate scale with the APS pixel size.

Detectors The visible detector (VLD)will be a 2kx2k hybrid Active Pixel Sensor (APS) H2RG ROIC+HyViSI PIN array produced by Teledyne with 18 μm pixel size The UV detector (UVD) will be a photon counting Intensified Active Pixel Sensor (IAPS) with a 2k 2k format, 15 μm pixel size, with the capability of working also in integration/analog mode under high flux though with a reduced spatial resolution (30 μm pixel size, 1kx1k)

stray light rejection Sources of stray light: 1. Disk light entering IEO: Reflected back through IEO by M0 2. Disk light diffracted by IEO: Blocked by IO and by LS

Effects of ERM descoping Loss of repointing capabilities consequences: in unsafe conditions when offset pointing > 9 arcmin (= 0.15 R @0.28 AU) (= 0.2 R @0.35 AU) (= 0.28 R @0.5 AU) Total APE requirement (S/C + ) : < 4.5 arcmin Non-symmetric vignetting function + non-symmetric stray light pattern Decrease of S/N in pb measurements Need of pointing knowledge to be characterized (better than 1 arcmin TBD)

Effects of ERM descoping Effects of offset pointing or offset error on stray light: Figure shows a ratio of 3 between lateral lobes of stray light pattern at 2.7arcmin offpointing L=70mm a=0,604deg 8,00E-05 7,00E-05 6,00E-05 5,00E-05 4,00E-05 3,00E-05 6,78mm 6,92mm 6,34mm 6,30mm 6,26mm 2,00E-05 1,00E-05 0,00E+00-1,00E+02-8,00E+01-6,00E+01-4,00E+01-2,00E+010,00E+002,00E+014,00E+016,00E+018,00E+011,00E+02

Imaging performances No change of imaging performances in UV and VL channel after descoping

Sunsensor descoping Sunsensor has two functions: Provide pointing information Safety If sunsensor is descoped: Pointing information given by S/C and stray light pattern (TBD) Safety given by UVD MCP current monitoring

Cleanliness Particle contamination open issue cleanliness budget can be met with the exception of the IEO cleanliness. IDM descoping brings in also a molecular contamination issue The IEO cleanliness effort is based on comparison with UVCS, LASCO, and SECCHI. All three instruments had a sealed door. The accommodation of the current instrument design on Solar Orbiter will not satisfy the critical particle cleanliness requirement during launch. Mitigation of the launch environment will be achieved with a one-shot door that seals the feedthrough aperture combined with the recloseable heat shield door. The two doors bring both particulate and molecular contamination under control

Cleanliness

Cleanliness

Summary of optical specifications Field of view Annular Sun-centered: 1.5-2.9 1.6 3.1 R @ 0.28 AU 2 4 R @ 0.35 AU Telescope type Effective focal length Externally occulter on-axis telescope 296mm UV 360 mm VL Inverted External Occulter (IEO) Stop aperture at heat shield Sun-light Rejection Mirror (M0) Circular hole (Diam.): 40 mm Spherical (Diam.): 71 mm; Curv. Radius: 1600 mm Primary mirror (M1) Secondary mirror (M2) Lyot stop Spatial resolution Wavelength band-pass Detectors On axis ellipsoidal: outer (Diam.): 160 mm, inner (Diam.): 88mm Curvature radius: 272 mm, conic: -0.662 On axis ellipsoidal: outer (Diam.): 216 mm, inner (Diam.): 125 mm Curvature radius: 312.385 mm, conic: -0.216 Circular obscuration (Diam.): 46 mm VL: 20 arcsec UV: 20 arcsec < 2.5 R ; > 20 arcsec at > 2.5 R VL: 580-640 nm; UV HI (121 ± 10) nm UV: APS Scale factor 10.1 arcsec/pxl Image size: 30.7 mm (2048x2048) with 15 μm pixel size VL: APS Scale factor 10.7 arcsec/pxl Image size: 36.7 mm (2048x2048) with 18 μm pixel size