RFIT 13-07 AE - Sentinel 2 -- GS2.HO.ASD.SY.000xx RFIT 2

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ASTRIUM SATELLITES Earth Observation, Navigation & Science GMES Sentinel-2 DLR - Raumfahrt-Industrietage in Friedrichshafen 13./14. Mai 2009 Projekt-Status und Möglichkeiten der Zusammenarbeit Name: Heinz Sontag

Transcript of RFIT 13-07 AE - Sentinel 2 -- GS2.HO.ASD.SY.000xx RFIT 2

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ASTRIUM SATELLITESEarth Observation, Navigation & Science

GMES Sentinel-2

DLR - Raumfahrt-Industrietage in Friedrichshafen 13./14. Mai 2009

Projekt-Status und Möglichkeiten der Zusammenarbeit

Name: Heinz Sontag

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

• GMES is an EC lead E.O. operational programme co-funded by ESA to ensure European independence for operational Earth monitoring.

• Sentinel-2 focuses at delivering operational GMES land & security services: global, systematic, medium/high resolution optical imagery with very high revisit.

• Sentinel-2 secures continuity & further enhancement of SPOT & Landsat-type multi-spectral data : land cover, land use, change detection maps and geophysical variables maps over a 15 years minimum period

• Total GMES budget currently >1 B€, covering development of 3 land and seamissions (Sentinel-1 to 3) with 2 satellites each, ground segment, and preparatory activities (S4 and S5) for atmospheric missions

GMESGlobal Monitoring for Environment and Security

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Key requirementsGlobal mapping of all land surfaces with up to 10 m spatial resolutionin 13 multispectral bands, visible to shortwave infrared spectral rangeImage size: 290 km swath, up to 29.000 pixels per lineImage data volume 800 GByte per day (compressed)Lifetime 7 years design qualification,

12 years for consumables

Spectral band settings

0

5

400 500 600 700 800 900 1000 1100 1200 1300 1400 1500 1600 1700 1800 1900 2000 2100 2200 2300 2400

[ nm ]

Sentinel-2

SPOT 5

LDCMSpat

ial R

esol

utio

n

VNIR SWIR

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Key design features

Polar Orbiting Satellite in a sun-synchronous orbitaltitude 786 km, 100 min/orbitimage acquisition over all land surfaceson daylight side of orbitside-looking capability to access any point on Earth within 1-2 days4 ground stations

Multispectral Instrument operating in pushbroom principle

filter based optical systemlow noise image compression techniques

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Sentinel-2 Satellite Key Features

Attitude and Orbit Control- Advanced APS Star Trackers for

precision attitude measurement- High Performance Fiberoptic Gyrofor precision rate measurements

- dual band GPS receiver- Low noise reaction wheels forattitude control

Power Subsystem- 6.5 m² single sided solar array- GaAs triple junction cells- 2.2 kW output power- 207 Ah battery

Data handling Subsystem- 3 Tbit Flash memory- 520 Mbps effective X-

band downlink system-- Laser Com Terminal Option

Overall Configuration- Structure Al frame/honeycomb- Mass 1.1 ton- Dimensions 3.4m x 1.8 m x 2.35 m- Fuel 117 kg Hydrazine

Monopropellant- Thermal Ctrl passive with deep

space radiators

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

The Multi-Spectral Instrument

Structure and optical elements in SiC ceramics

High performanceoptical filters

Monolithic Silicon and hybrid Mercury Cadmium Telluride

cooled detectors

High performance video and low noisecompression electronics

spectral range 0.4 – 2.4 μm data rate 490 Mbit/smass 290 kgpower 280 W

pushbroom sensoroptical FOV 20.6°15 cm effective pupildiameter

20.6°

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Sentinel-2 products - Land Cover / Land Use

Cultivated field 2

Cultivated field 1

Bare soil 2

Bare soil1

Forest 2

Forest 1

Water

Urban

Simulated Sentinel-2 images(red/green/blue bands)

and near-infrared/red/green

Example of production of land cover map

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Programme Overview

2012 Launchwith new European launcher VEGA

2008 2009 2010 2011 2012 2013

detaileddesign realisation

phase launch & commissioning

operational phase 1st satellite

preliminarydesign

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Sentinel-2 Prime Subcontractors

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Sentinel-2 Status and German SME InvolvementSatellite Prime Astrium GmbH

German SMEs involvement: star trackers (Jena-Optronik),Laser Communication Terminal (Tesat)

Multispectral Instrument Prime Astrium SASprocurement completedGerman SMEs involvement:

video-electronics (Jena-Optronik), optical filter (Jena-Optronik), power supply (ASP)

Common Procurements with EC

Reference design for Astrium Astrobus harmonisations

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Sentinel-2 Opportunities for German SMEs

Flight HWMagnetometer ITT on EMITSMagnetic Torquers ITT on EMITSReaction Wheels ITT expected May 2009

Flight SWSW Support ITT expected July 2009ISVV ITT expected July 2009

Ground SupportRF SCOE ITT expected June 2009Power SCOE ITT expected June 2009AIT Operations Support 2011 -2012

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ASTRIUM SATELLITES

GMES Sentinel-2 PDR 28 October 2008, ESTEC

Sentinel-2 Contact personsHead of Project

Dr. Heinz SontagTel: +49 7545 8 4980Email: [email protected]

System EngineerMario WelschTel: +49 7545 8 9083Email: [email protected]

ProcurementChristian StelterTel: +49 7545 8 5718Email: [email protected]