Nine Years of Atmospheric Remote Sensing with SCIAMACHY – Instrument Performance Gottwald, Krieg, Lichtenberg , Slijkhuis – DLR-IMF Noël, Bramstedt, Bovensmann, von Savigny – IUP, Univ. of Bremen Snel, Krijger – SRON
Jan 29, 2018
Nine Years of Atmospheric Remote Sensing with SCIAMACHY – Instrument PerformanceGottwald, Krieg, Lichtenberg, Slijkhuis – DLR-IMFNoël, Bramstedt, Bovensmann, von Savigny – IUP, Univ. of BremenSnel, Krijger – SRON
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 2
Topics
instrument
operations
instrument status and performance
mission extension
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 3
SCIAMACHY on ENVISAT
26 m × 10 m × 5 mSatellite dimensions
8.2 tSatellite mass
10No. of instruments
100.6 minOrbit period
10 a.m. (sun-synchronous)Descending node crossing
800 kmMean altitude
98.5°Inclination
ENVISAT nominal mission profile
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 4
Instrument – Optical Assembly
Level 1:
channels 1 & 2 (UV)
entrance optics
calibration unit
pre-disperser prism
Level 2:
channels 3 & 4 (VIS)
channel 5 (NIR)
channels 6-8 (SWIR)
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 5
Viewing Geometries
scientific
nadir
limb
sun occultation
moon occultation
calibration & monitoring
sun occultation
moon occultation
subsolar
internal calibration lamps (WLS, SLS)
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 6
Instrument – Thermal SubsystemsOptical Bench Module (OBM)
cooled via RAD AT = -17.6°C to -18.2°Cactive thermal control (ATC)
detectorscooled via SCIAMACHY Radiant Cooler (SRC)
T ≈ 195 K – 230 K (channels 1-6)
T ≈ 140 K – 160 K (channels 7 & 8)open loop heater control (TC)detectors
decontaminationSRC cooling capacity may degrade because of contaminationdecontamination heaters to raise T on reflecting surface (if needed) decontamination brings T of OBM and detectors close to 0°C
→ contaminants are removed
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 7
Operationsinstrument operations are
continuous
highly autonomous
implemented in states and timelines
organised in mission scenarios
limb/nadir on dayside
sun occultation each orbit
sub-solar every 3rd day
moon occultation whenever possible
dedicated eclipse measurements
calibration&monitoring measurements on daily, weekly and monthly timescales
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 8
instrument operation related information available via
http://atmos.caf.dlr.de/projects/scops/
launch March 1, 2002
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Instrument Status - Availability
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 9
Thermal Systems: ATC and OBM Temperature
only small orbital variation of TOBM
very stable orbital mean TOBM
ATC degradation compensated by heater power adjustment
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 10
Thermal Systems: TC and Detector Temperaturestemperature control via TC heaters
TC system degrades
detectors 1-6: 0.1-0.3 K / year
detectors 7 & 8: approx. 1 K
ice layer effect
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 11
Life Limited Items
mechanical items (neutral density filter, aperture stop, nadir calibration window) and thermal item (cryogenic heatpipe) have assigned in-flight activation budgets
electrical items (WLS, SLS) have assigned in-flight switching budgets
operations concept goal is not to exceed LLI limits
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 12
Optics - Throughput optical throughput channels 1-6
reduction of 3-4% per year in UV
very stable in VIS, NIR & SWIR
solar eclipse
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 13
channels 6+, 7, 8:
6% pixel loss / year about 10-15% ‘good’ pixels by end 2013
in 7 & 8: throughput loss 1-2% / year due to ice layer (decontaminations are still an option to remove ice)
Detectors - Degradation
channel 2: detector material degradation (2% sensitivity loss / year) 25% loss by end 2013
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 14
Limb Tangent Height
pointing knowledge essential for geolocation retrieval, particularly limb tangent heights
continuos improvement over the mission lifetime: current limb tangent height accuracy about 0.002-0.003° = 120-150 m
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 15
mission in nominal ENVISAT orbit ended 22 October 2010
Mission Extension 2010-2013
since then modified drifting orbit
no inclination manoeuvres
altitude lowered by 17 km
instrument configuration successfully adapted to new orbit
SCIAMACHY continues to deliver high quality data
IGARSS2011 > G. Lichtenberg > 28 July 2011
Slide 16
SCIAMACHY – Exploring the Changing Earth’s Atmosphere
SCIAMACHY – The Need for Atmospheric Research from Space
ENVISAT – SCIAMACHY’s Host
The Instrument
Instrument Operations
Calibration and Monitoring
SCIAMACHY In-Orbit Operations and Performance
From Radiation Fields to Atmospheric Concentrations – Retrieval of Geophysical Parameters
Data Processing and Products
Validation
SCIAMACHY’s View of the Changing Earth’s Environment