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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
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NineYearsofAtmosphericRemoteSensingwithSCIAMACHY-InstrumentPerformance.ppt

Jan 29, 2018

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Page 1: NineYearsofAtmosphericRemoteSensingwithSCIAMACHY-InstrumentPerformance.ppt

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

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Slide 2

Topics

instrument

operations

instrument status and performance

mission extension

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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

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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)

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Slide 5

Viewing Geometries

scientific

nadir

limb

sun occultation

moon occultation

calibration & monitoring

sun occultation

moon occultation

subsolar

internal calibration lamps (WLS, SLS)

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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

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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

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Slide 8

instrument operation related information available via

http://atmos.caf.dlr.de/projects/scops/

launch March 1, 2002

end

no

min

al m

issi

on

ph

ase

M

arc

h 1

, 20

07

Instrument Status - Availability

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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

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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

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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

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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

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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

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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

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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

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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