cosima for the esa mission rosetta - vh-s.de

1
vH&S RAUMFAHRT • FORSCHUNG • INDUSTRIE COmetary Secondary Ion Mass Analyser COSIMA for the ESA Mission ROSETTA H. Henkel q, H. H ¨ ofner w, J. Kissel e, A. Koch q, M. Hilchenbach e q von Hoerner & Sulger GmbH (vH&S), Schwetzingen, w Max-Planck-Institut f¨ ur extraterrestrische Physik (MPE), Garching, e Max-Planck-Institut f¨ ur Aeronomie (MPAe), Katlenburg-Lindau The COSIMA Instrument Electronics Box Dust Inlet Target Manip. Unit COSISCOPE Ion Source (Clean) Ion Source (Analyse) Primary Ion Optics Drift Tube Ion Reflector COSIMA’s Scientific Objectives Target: Comet 67P/Churyumov-Gerasimenko Analysis of the elemental composition (and isotopic composition of some key elements) of cometary grains. Chemical characterisation of the main organic compo- nents, present homologuous and functional groups. Mineralic and petrographic characterisation of the inor- ganic phases—all related to solar system chemistry. COSIMA Specifications Atomic mass range 1. . . 4000 Da Relative atomic mass resolution m/dm at m = 300 >2500 COSIMA instrument mass 19.8 kg Indium ion pulse duration 5 ns Indium ion energy 8 keV Power consumption from 28V DC 20.4 W The COSIMA Team vH&S The von Hoerner & Sulger GmbH is prime con- tractor and responsible for the overall design, man- agement, production, and qualification testing. The Max-Planck-Institut f¨ ur extraterrestrische Physik (MPE), Garching, Germany, then with Di- rector Prof. G. Haerendel, hosted the PI Dr. Jochen Kissel, contributed TMU and mechanical systems. The Bergische Universit¨ at und Gesamthoch- schule Wuppertal (BUGH) participated in devel- opment of the data acquisition unit TDC. The Finnish Meteorological Institute (FMI), Helsinki, Finland, provided the GSE and the COSIMA flight software. The Ingenieurb ¨ uro Dr. Franz Krueger, Darm- stadt, Germany, provided cleanliness analyses, sci- entific methods for spectra interpretation, and de- velopmental effort for collector targets. The Institut d’ Astrophysique Spatiale (IAS), Or- say, France, developed the COSISCOPE camera and the power converters. The ¨ Osterreichisches Forschungszentrum Sei- bersdorf Ges. m. b. H. (ARCS), Austria, provided the Primary Ion Sources (PIS). The Institut ur Weltraumforschung (IWF), Graz, Austria, developed the HV supply for the PIS. The Laboratoire de Physique & Chimie de l’Environnement (LPCE), Orleans, France, pro- vided the primary ion optics (PIBS). The Universit¨ at der Bundeswehr, Neubiberg, Germany, provided collector targets. Nyle Utterback, Santa Barbara, CA, did the ion optics design. The Institut f ¨ ur Planetologie,M¨ unster, Germany, performed TOF-SIMS analysis of analogs for scien- tific and instrumental comparison. The Max-Planck-Institut ur Aeronomie (MPAe), Katlenburg-Lindau, provides science operations. The ROSETTA Spacecraft ROSETTA at Comet — Artist’s view COSIMA Timeline 1992 ESA performs Pre-Study for new Cometary Mission “ROSETTA”. Dr. J. Kissel, MPK Heidelberg, presents dust mass spectrometer concept based on CoMA/CRAF (NASA mission, canceled). Sep. 1993 ESA selects ROSETTA as new “Cornerstone Mission.” June 1994 Dr. Kissel contacts insti- tutes for contributions, prepares exp. proposal “COSIMA” to ESA. Dec. 1995 ESA selects COSIMA for the ROSETTA mission. Summer 1996 vH&S starts develop- ment of COSIMA eng. model. 1998 vH&S receives contract for the COSIMA flight model. July 2002 vH&S delivers the COSIMA flight model (XM) to ESTEC. Jan. 2003 ROSETTA launch (Kourou) postponed by ESA. July 2003 COSIMA emitter mainte- nance session at GSC, Kourou. 26 Feb. 2004 Planned launch date. Aug. 2014 Arrival (prelim.) at comet 67P/Churyumov-Gerasimenko. COSIMA Functional Principle Target Target Target Indium Camera (Camera Pos.) Ion Optics Ion Source Ion Reflector Ion Detector Electronics Robotic Arm with Target (Spectrometer Pos.) (Collect Position) Cometary Dust Target Store (Chemistry Station) Tungsten Needle Secondary Ion Beam Primary Ion Beam cosima-func-en.fig ROSETTA Spacecraft Drift Tube COSIMA Block Diagram Divider Chain Power Data KAL Data Amp. Sensors Motors Start Point to Target PIBS Camera GND COSISCOPE TMU PIS Control PIBS Control Deflection Cntl. Interface Control Deflection Cntl. Control HK-Unit S/C-Interface Casc. Supply HVC Cascade Cascade Chain (DET-CASC) (PA-CASC) (TOF1/2-HVC) (D-, A-CNTL) (D-CNTL, A-CNTL) (D-CNTL, A-CNTL) (Board Names in Brackets) Chop. HVC Bunch. HVC Generator PIBS Timing PIBS Camera TMU Primary Ion Divider Detector Post-Accel. (SERIF) Low-Voltage TOF-HVC TOF Secondary Ion Reflector (D-, A-CNTL) (D-, A-CNTL) (HK1, HK2) Switch Unit (LVS) (D-CNTL) (SERIF) (TMUC, TMUD-A, -B) Boot PROM SRAM Program Watch Dog Latch- Up-Cntl. CPU 21020 Data SRAM EEPROM Program Bus I/F LVC (LVC) (TDC-TDC) COSIMA Experiment Bus Camera TMU TDC PIS, PIBS, TOF Statuses Temperatures Currents Voltages Start COSIMA Experiment Bus CCD (DET-NW) Ion Path Extr. Lens Reflector Ion Detector Target Emitter A Chopper 3-Stage Buncher Emitter C LC1 LA1 Analyze Beam Clean Beam HVC U_px U_pe HVC Beam Switch Drift Tube $Revision: 1.15 $ HVC HVC Dual-HVC Deflection Unit Deflection Unit TOF-HVC PA-HVC (PA/DET-HVC) (PA/DET-HVC) (PIBS/TOF-DU) (TOF3-HVC) (PIBS/TOF-DU) (L1/2-HVC) (L1/2-HVC) (CB-HVC) (CB-HVC) Lenses 2 Lenses 1 Beam Switch TDC (TDC-TDC, -DAC, -PTC, -TRIG) (CPU) DET-HVC (BS-HVC) Heater Supply cosimablk.fig LA2 LC2 COSIMA Measurement Principle Cometary dust is collected on targets, which are stored in Target Manipulation Unit (TMU). The dust grains are located by microscopic camera COSISCOPE. A pulsed primary Indium ion beam partially ionises the dust grains. The secondary ions (pos. or neg., selectable) are accelerated by electrical fields, and travel well-defined distance through drift tube and ion reflector. A multisphere plate with dedicated amplifier is used to detect the ions. The arrival times of the ions are digitised and accumulated into 2ns bins. The mass spectra are calculated from the time-of-flight spectra. The COSIMA Investigation COSIMA has been proposed, developed, and delivered by an international team of 39 investigators. The PI Jochen Kissel (MPAe) and 4 CoPIs Yves Langevin (IAS), Rita Schulz (ESTEC), Johan Sil ´ en (FMI), and Hanna von Hoerner (vH&S) are leading the investigation. Funding comes from DARA/DLR and the respective other national agencies. The special support by ESTEC in a critical situation before delivery is gratefully acknowledged. COSIMA Contact, Links COSIMA Info von Hoerner & Sulger GmbH, Schlossplatz 8, D-68723 Schwet- zingen, Germany, http://www.vh-s.de, Tel.: (+49) 62 02 / 57 56-16, E-mail: [email protected]. This poster is available at: http://www.vh-s.de/projects/cosima/press/a4poster.pdf MPAe Homepage http://www.linmpi.mpg.de MPE Homepage http://www.mpe.mpg.de FMI COSIMA Homepage http://www.geo.fmi.fi/PLANETS/Cosima.html ROSETTA Homepage http://rosetta.esa.int Poster first presented at EGS-AGU-EUG joint assembly, Nice, France, 10 April 2003. Revised and extended 22 April 2004, Rev. 1.106. Poster by pdfT E X.

Upload: others

Post on 18-Dec-2021

6 views

Category:

Documents


0 download

TRANSCRIPT

Page 1: COSIMA for the ESA Mission ROSETTA - vh-s.de

vH&SRAUMFAHRT • FORSCHUNG • INDUSTRIE

COmetary Secondary Ion Mass AnalyserCOSIMA for the ESA Mission ROSETTAH. Henkel q, H. Hofner w, J. Kissel e, A. Koch q, M. Hilchenbach e— q von Hoerner & Sulger GmbH (vH&S), Schwetzingen,

w Max-Planck-Institut fur extraterrestrische Physik (MPE), Garching, e Max-Planck-Institut fur Aeronomie (MPAe), Katlenburg-Lindau

The COSIMA Instrument

Electronics Box

Dust Inlet

Target Manip. Unit

COSISCOPE

Ion Source (Clean)

Ion Source (Analyse)

Primary Ion Optics

Drift Tube

Ion Reflector

COSIMA’s Scientific ObjectivesTarget: Comet 67P/Churyumov-Gerasimenko

• Analysis of the elemental composition (and isotopiccomposition of some key elements) of cometary grains.

• Chemical characterisation of the main organic compo-nents, present homologuous and functional groups.

• Mineralic and petrographic characterisation of the inor-ganic phases—all related to solar system chemistry.

COSIMA SpecificationsAtomic mass range 1. . . 4000DaRelative atomic mass resolution m/dm at m=300 >2500COSIMA instrument mass 19.8 kgIndium ion pulse duration ≈5nsIndium ion energy 8 keVPower consumption from 28V DC 20.4W

The COSIMA Team

vH&S The von Hoerner & Sulger GmbH is prime con-tractor and responsible for the overall design, man-agement, production, and qualification testing.

The Max-Planck-Institut fur extraterrestrischePhysik (MPE), Garching, Germany, then with Di-rector Prof. G. Haerendel, hosted the PI Dr. JochenKissel, contributed TMU and mechanical systems.

The Bergische Universitat und Gesamthoch-schule Wuppertal (BUGH) participated in devel-opment of the data acquisition unit TDC.

The Finnish Meteorological Institute (FMI),Helsinki, Finland, provided the GSE and theCOSIMA flight software.

The Ingenieurburo Dr. Franz Krueger, Darm-stadt, Germany, provided cleanliness analyses, sci-entific methods for spectra interpretation, and de-velopmental effort for collector targets.

The Institut d’ Astrophysique Spatiale (IAS), Or-say, France, developed the COSISCOPE cameraand the power converters.

The Osterreichisches Forschungszentrum Sei-bersdorf Ges.m.b.H. (ARCS), Austria, providedthe Primary Ion Sources (PIS).

The Institut fur Weltraumforschung (IWF),Graz, Austria, developed the HV supply for the PIS.

The Laboratoire de Physique & Chimie del’Environnement (LPCE), Orleans, France, pro-vided the primary ion optics (PIBS).

The Universitat der Bundeswehr, Neubiberg,Germany, provided collector targets.

Nyle Utterback, Santa Barbara, CA, did the ionoptics design.

The Institut fur Planetologie, Munster, Germany,performed TOF-SIMS analysis of analogs for scien-tific and instrumental comparison.

The Max-Planck-Institut fur Aeronomie(MPAe), Katlenburg-Lindau, provides scienceoperations.

The ROSETTA Spacecraft

ROSETTA at Comet

—Artist’s view

COSIMA Timeline

1992 ESA performs Pre-Study for newCometary Mission “ROSETTA”.

Dr. J. Kissel, MPK Heidelberg,presents dust mass spectrometerconcept based on CoMA/CRAF(NASA mission, canceled).

Sep. 1993 ESA selects ROSETTA asnew “Cornerstone Mission.”

June 1994 Dr. Kissel contacts insti-tutes for contributions, preparesexp. proposal “COSIMA” to ESA.

Dec. 1995 ESA selects COSIMA forthe ROSETTA mission.

Summer 1996 vH&S starts develop-ment of COSIMA eng. model.

1998 vH&S receives contract for theCOSIMA flight model.

July 2002 vH&S delivers the COSIMAflight model (XM) to ESTEC.

Jan. 2003 ROSETTA launch (Kourou)postponed by ESA.

July 2003 COSIMA emitter mainte-nance session at GSC, Kourou.

26 Feb. 2004 Planned launch date.

Aug. 2014 Arrival (prelim.) at comet67P/Churyumov-Gerasimenko.

COSIMA Functional Principle

Target

Target

Target

Indium

Camera(Camera Pos.)

Ion Optics Ion Source

Ion Reflector

Ion Detector

Electronics

Robotic Arm with Target(Spectrometer Pos.)

(Collect Position)

Cometary Dust

Target Store

(Chemistry Station)

Tungsten Needle

Secondary Ion Beam

Primary Ion Beam

cosima−func−en.fig

ROSETTASpacecraft

Drift Tube

COSIMA Block Diagram

Divider Chain

Power

Data

KAL

Data

Amp.

Sensors

Motors

Start

Poi

nt to

Tar

get

PIBS

Camera

GND

COSISCOPE

TMU

PIS ControlPIBS ControlDeflection Cntl.InterfaceControl

Deflection Cntl. ControlHK−Unit

S/C−Interface

Casc.Supply HVC

Cascade Cascade

Chain

(DET−CASC)(PA−CASC)

(TOF1/2−HVC)

(D−, A−CNTL)(D−CNTL, A−CNTL)(D−CNTL, A−CNTL)

(Board Names in Brackets)

Chop. HVCBunch. HVC

GeneratorPIBS TimingPIBSCameraTMU

Primary Ion

Divider

DetectorPost−Accel.

(SERIF)

Low−VoltageTOF−HVCTOF

Secondary Ion Reflector

(D−, A−CNTL) (D−, A−CNTL)(HK1, HK2)

Switch Unit(LVS)(D−CNTL)

(SERIF)(TMUC, TMUD−A, −B)

BootPROM SRAM

Program WatchDog

Latch−Up−Cntl.

CPU21020

DataSRAMEEPROM

ProgramBusI/F LVC

(LVC)

(TDC−TDC)

CO

SIM

A E

xper

imen

t Bus

Cam

era

TM

U

TD

C

PIS

, PIB

S, T

OF

Sta

tuse

s

Tem

pera

ture

s

Cur

rent

s

Vol

tage

s

Sta

rt

COSIMA Experiment Bus

CC

D

(DET−NW)

Ion Path

Extr. Lens

Reflector

Ion Detector

Target

Emitter AChopper

3−Stage Buncher

Emitter CLC1

LA1

Analyze Beam

Clean Beam

HVCU_px

U_peHVC

Beam Switch

Drift Tube

$Revision: 1.15 $

HVCHVC Dual−HVCDeflection Unit

Deflection UnitTOF−HVC

PA−HVC(PA/DET−HVC) (PA/DET−HVC)

(PIBS/TOF−DU)(TOF3−HVC)

(PIBS/TOF−DU) (L1/2−HVC) (L1/2−HVC)(CB−HVC)(CB−HVC)

Lenses 2 Lenses 1Beam Switch

TDC(TDC−TDC, −DAC,

−PTC, −TRIG) (CPU)

DET−HVC

(BS−HVC)

Hea

ter

Sup

ply

cosimablk.fig

LA2

LC2

COSIMA Measurement Principle

• Cometary dust is collected on targets, which are stored in Target ManipulationUnit (TMU).

• The dust grains are located by microscopic camera COSISCOPE.• A pulsed primary Indium ion beam partially ionises the dust grains.• The secondary ions (pos. or neg., selectable) are accelerated by electrical fields,and travel well-defined distance through drift tube and ion reflector.

• A multisphere plate with dedicated amplifier is used to detect the ions.• The arrival times of the ions are digitised and accumulated into 2ns bins.• The mass spectra are calculated from the time-of-flight spectra.

The COSIMA InvestigationCOSIMA has been proposed, developed, and delivered by an international teamof 39 investigators. The PI Jochen Kissel (MPAe) and 4 CoPIs Yves Langevin (IAS),Rita Schulz (ESTEC), Johan Silen (FMI), and Hanna von Hoerner (vH&S) areleading the investigation. Funding comes from DARA/DLR and the respectiveother national agencies. The special support by ESTEC in a critical situationbefore delivery is gratefully acknowledged.

COSIMA Contact, Links

COSIMA Info von Hoerner & Sulger GmbH, Schlossplatz 8, D-68723 Schwet-zingen, Germany, http://www.vh-s.de, Tel.: (+49) 6202 / 5756-16,E-mail: [email protected]. This poster is available at:http://www.vh-s.de/projects/cosima/press/a4poster.pdf

MPAe Homepage http://www.linmpi.mpg.de

MPE Homepage http://www.mpe.mpg.de

FMI COSIMA Homepage http://www.geo.fmi.fi/PLANETS/Cosima.html

ROSETTA Homepage http://rosetta.esa.int

Poster first presented at EGS-AGU-EUG joint assembly, Nice, France, 10 April 2003. Revised and extended 22 April 2004, Rev. 1.106. Poster by pdfTEX.