LAGRANGE REMOTE SENSING INSTRUMENTS: THE EXTREME ULTRAVIOLET IMAGER (EUVI)
C. Kintziger (CSL) - Presenter S. Habraken (CSL) P. Bouchez (CSL) Matthew West (ROB) David Berghmans (ROB) Manfred Gyo (PMOD/WRC) Margit Haberreiter (PMOD/WRC) Jackie Davies (RAL Space) Martin Caldwell (RAL Space) Ian Tosh (RAL Space) Stefan Kraft (ESA)
1 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Mission overview
4 remote-sensing instruments See Poster 23 by J. Davies
2 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Mission overview
5 in-situ instruments
3 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Mission overview
• Overall Remote Sensing Instruments leader: RAL Space (UK) • EUVI study led by three institutes: – CSL (BE) – ROB (BE) – PMOD/WRC (CH)
• CSL activities • ROB activities • PMOD activities – EUVI Instrument manager: – instrument – electrical engineering • Overall management requirements – mechanisms • System study – instrument operation – mechanical engineering • Optical engineering – ground segments • Thermal engineering • AIT engineering
• Roles & Responsibilities – BPI: Pr. Dr. Serge Habraken (CSL) – Bco-I: Dr. Matthew J West (ROB) – CSL work funded by Belspo via Prodex Programme
4 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Mission overview
• EUV Imager – SSA programme (SWE) – Location: L5 – Goal: image the full solar disc – Waveband: EUV wavelength (e.g. 193 Å) – Heritage: PROBA-2 SWAP ESIO (GSTP) Solar Orbiter EUI
Parameter Requirement Spectral resolution < 1.5 푛푚 퐹푊퐻푀 Spatial resolution < 5 푎푟푐푠푒푐 Field of view 42.6′ 푥 42.6′ Mass < 8 푘푔 Size < 600 푥 150 푥 150 푚푚 Power < 10 푊
5 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Instrument overview
• Selected wavelengths
131 nm 19.5 nm 30.4 nm
Semi-Static Structures Dynamic structures Regions
Filaments/Prominences Flares Chromosphere Active Regions Eruptions Million Degree Corona Coronal Holes EUV Waves Dimmings
6 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Instrument overview
• Field of view
– Differs between selected wavebands
1. 195 Å
43 arcmin Toward Earth
62 arcmin
2. 131 + 304 Å
43 arcmin
43 arcmin
7 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Instrument overview
• Detector: EUI spare 3k by 3k, separate windowing options 1. 195 Å: 2300x1600, 1,6”/pixel, 3.2” spat. res. over 2 pixels 2. 131 + 304 Å: 2x2 binning, 800x800, 3.2”/pixel, 6.4” spat. res. over 2 pixels
• Cadence: Different for each spectral channel 1. 195 Å: 3 min 2. 131 Å: 2 min 3. 304 Å: 5 min • Schematic configuration:
Channel 1 FEE DC/DC Entrance f ilter FPA camera
Detector PE Power Optical sy stem Door
Channel 2 Entrance f ilter Filter wheel FPA camera
Detector PE
Optical sy stem Door HK, data Mechanism EUVI Optical Unit control TC
EUVI Electronic Box IPU
8 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Instrument overview
• Obtained design
– ESIO-like truss structure
• Separate avionic box
• Lightweight and stiff – SWAP-based optical design
• Improved spatial resolution and larger FOV wrt SWAP (and ESIO)
• Similar baffling system – Filter wheel
• Selects between 131 and 304 observation – One-shot opening doors
9 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Performed analyses
• Performed analyses
– Understanding of requirements
– Optical design
• Tolerancing
EUVI Electronics IPCU
Optical Unit • Straylight Heater TL 2*(1) EUVI Survival Heater RadiatorLink Radiator Thermal Link Thermistor TL 2*(1) EUVI Thermistor RadiatorLink
Camera 1 SpW 2*(1) EUVI-A CCSDS SpW 2*(1)
Heater APS(A) 2*(1) EUVI Operational Heater APS (A)
Thermistor APS(A) 2*(1) EUVI Thermistor APS (A)
Camera 2 SpW 2*(1) EUVI-B CCSDS SpW 2*(1)
Heater APS(B) 2*(1) EUVI Operational Heater APS (B) – Electrical design Thermistor APS(B) 2*(1) EUVI Thermistor APS (B) Power EB HK Control
EB HK Control
Filter Wheel Power
Electronic Box – Instrument performance model Power 2*(1) EUVI SU 2*(1)
Heater EB 2*(1) EUVI Survival Heater EB
Thermistor EB 2*(1) EUVI Thermistor EB – Thermal analysis:
• Undergoing at CSL
– Structural analysis
• Undergoing at PMOD/WRC
10 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Performed analyses
• Encountered issues:
– Coating: dual-band coating for 131 + 304 Å is not “off-the-shelf” because those two wavelengths do not fall within two successive Bragg orders (need to be factor ~2 between wavelengths)
• is feasible
• requires simulation and development
Other alternatives:
• Superpose 2 mono-band coatings on top of each other
• Implement a patterned coating on primary mirror
will lead to ~50% loss in efficiency BUT mono-band coating may be as high as 2x more efficient than dual-band.
11 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Way forward after PRR
12 ESWW 2018, 9 Nov. 2018 LGRRS-EUVI | Conclusion
13 ESWW 2018, 9 Nov. 2018