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vH&S SPACE RESEARCH INDUSTRY Cometary and Interstellar Dust Analyzer CIDA for the NASA Mission STARDUST H. Henkel q, J. Kissel w, J. Ryn ¨ o e, q von Hoerner & Sulger GmbH (vH&S), Schwetzingen, w emeritus, Max-Planck-Institute for Aeronomy (MPAe), Katlenburg-Lindau e Finnish Meteorological Institute (FMI), Helsinki CIDA Sensor and E-Box CIDA’s Scientific Objectives Analysis of the elementary and molecular composition of interstellar and cometary dust grains. Target: Comet Wild2 at 2 Jan. 2004 During cruise, CIDA measured 10 spectra of pos. ions, and 35 spectra of neg. ions—the first ever neg. dust spectrum! During encounter there were 27 pos. and 2 neg. spectra. CIDA Specifications Mass sensitivity 1×10 -13 g @ 6 km/s Atomic mass range 1. . . 350 Da Target area 130 cm 2 or 8 cm 2 , automatic Relative atomic mass resolution m/dm at m=100 >200 Sustained event rate >40 spectra/s CIDA instrument mass 10.4 kg Power consumption from 28V DC max. 15 W CIDA Spectrum (Encounter) The CIDA 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, and contributed mechanics. The Bergische Universit¨ at und Gesamthoch- schule Wuppertal (BUGH) participated in devel- opment of the detector amplifiers and the data ac- quisition unit FDAQ. The Finnish Meteorological Institute (FMI), Helsinki, Finland, provided the CIDA flight soft- ware, the GSE, and operational support. The Ingenieurb ¨ uro Dr. Franz Krueger, Darm- stadt, Germany, provided cleanliness analyses, sci- entific methods for spectra interpretation, and de- velopmental effort for the target. The Institut d’ Astrophysique Spatiale (IAS), Or- say, France, provided the low voltage converters. The Jet Propulsion Laboratory (JPL), Pasadena, USA, contributed electronical components. Nyle Utterback , Santa Barbara, CA, did the ion optics design. CIDA on STARDUST S/C STARDUST Launch NASA photo CIDA Timeline End 1994 Study on Large Area Dust Impact Spectrometer (LADIS) by vH&S on DLR contract. June 1996 First CIDA interface meet- ing of vH&S with Lockheed- Martin Astronautics (LMA) in Denver, CO. May 1998 vH&S delivers the CIDA flight model to LMA. 7 Feb. 1999 STARDUST launch from Cape Canaveral. 2 Jan. 2004 Comet Wild 2 encounter. 15 Jan. 2006 Return of STARDUST’s dust sampling capsule to Earth. Happy PI with CIDA CIDA Block Diagram Voltages Various Bus I/F (+15V DC) Keep Alive Line (+28V DC) Supply Power Protection Clock cidablk.fig Multiplexer LMA 21020 Electron Multiplier Isolation Transformers PAM Modulators Isolating Power Supply Supply Channel Channel +1000V Log. Amps Redundancy Sw. "MM-1" -1000V Regulators Dust Signals Various +1100V 0V High Sens. Low Sens. Target Signal 0V Electronics Box Detector Module Reflector Spacecraft Interface HV-Safe HV-Safe J1 (RS-485) Serial I/O (0V/5V) Power On/Off J2 J3 DPU CIDA Bus Latch-Up (Ampl./Pol.) HV Control Flash ADC Flash ADC Event Trigger Unit FIFO Control Boot PROM Program RAM Watch Dog EEPROM Bus I/F Backup RAM Data RAM Event FIFO Event FIFO Low Voltage Converters Serial I/F Synchronous Amp Converters High Voltage Ion Path Unit Keeping House Drift Tube Target CPU CIDA Measurement Principle CIDA is a Time-Of-Flight (TOF) mass spectrometer with impact ionization: 1 impact = 1 spectrum! Cometary or interstellar dust hits a flat silver target, which is exposed to space. The high-velocity impact leads to instantaneous decomposition and ioniza- tion of the dust particle. The generated ions (pos. or neg.) are accelerated by electrical fields (polarity selectable), and travel fixed distance through drift tube and ion reflector. A stacked dynode multiplier (MM-1) with set of logarithmic amplifiers is used to detect the ions. The arriving ion charge is digitised by a pair of fast transient recorders. The mass spectra are calculated from the time-of-flight spectra. Technical Highlights Ion detector MM-1 Electron multiplier stack of 20 dynodes. Ad- vantages: Flat surface precise end-of-flight. Excellent pulse handling due to high electrode conductivity. Access to inter- mediate dynodes. Logarithmic amplifiers Log. stage by UHF transistor arrays. Redundant de- sign, two low/high sensitive channel pairs. Integrated test pulses. Triggering Weighted integral and pulse trigger modes. Bipolar Stacked HVCs Polarity switchable for analysis of pos. or neg. ions. Software Totally and automatically relocatable software to survive memory er- rors. Hand optimized Rice compression for the spectra. The CIDA Project The PI Dr. Jochen Kissel proposed the CIDA experiment, and is leading the overall investigation. CIDA has been developed, manufactured, tested, and delivered by company vH&S as prime contractor. The CIDA Project has been funded by the DARA/DLR, and the national space agencies of the team members. CIDA Contact, Links CIDA 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/cida-stardust/press/cidaposter-a4.pdf FMI CIDA Homepage http://www.geo.fmi.fi/PLANETS/cida.html STARDUST Homepage http://stardust.jpl.nasa.gov Literature “Assignment of quinone derivatives as the main compound class composing ‘interstellar’ grains based on both polarity ions detected by the ‘Cometary and Interstellar Dust Analyser’ (CIDA) onboard the spacecraft STARDUST”, F. R. Krueger, W. Werther, J. Kissel, and E. R. Schmidt, In: Rapid Commun. Mass Spectrom. 2004; 18: 103–111. “The Probable Chemical Nature of Interstellar Dust Particles Detected by CIDA Onboard STARDUST”, J. Kissel, F. R. Krueger, J. Sil´ en, and G. Haerendel, In: Proc. COSPAR Coll. Potsdam, July 2000. (Eds.) K. Scherer et al. Vol., Pergamon Press, 351–359, 2001. “Cometary and Interstellar Dust Analyzer for comet Wild 2”, J. Kissel, A. Glasmachers, E. Gr ¨ un, H. Henkel, H. H ¨ ofner, G. Haerendel, H. von Hoerner, K. Hornung, E. K. Jessberger, F. R. Krueger, D. ohlmann, J. M. Greenberg, Y. Langevin, J. Sil´ en, D. Brownlee, B. C. Clark, M. S. Hanner, F. Hoerz, S. Sandford, Z. Sekanina, P. Tsou, N. G. Utterback, M. E. Zolensky, C. Heiss, In: Journal of Geophysical Research, Volume 108, Issue E10, pp. SRD 4–1, 10/2003. Contribution EGU04-A-07474 for the EGU – 1st General Assembly, Session PS5, Poster Area Palais des Exposition, Mo., 26 April 2004. Rev. 23 April 2004 (1.53). Poster by pdfT E X.
Transcript

vH&SSPACE • RESEARCH • INDUSTRY

Cometary and Interstellar Dust AnalyzerCIDA for the NASA Mission STARDUSTH. Henkel q, J. Kissel w, J. Ryno e, q von Hoerner & Sulger GmbH (vH&S), Schwetzingen,

w emeritus, Max-Planck-Institute for Aeronomy (MPAe), Katlenburg-Lindau e Finnish Meteorological Institute (FMI), Helsinki

CIDA Sensor and E-Box

CIDA’s Scientific ObjectivesAnalysis of the elementary and molecular composition ofinterstellar and cometary dust grains.

Target: Comet Wild2 at 2 Jan. 2004

During cruise, CIDA measured 10 spectra of pos. ions, and35 spectra of neg. ions—the first ever neg. dust spectrum!During encounter there were 27 pos. and 2 neg. spectra.

CIDA SpecificationsMass sensitivity 1×10−13g @ 6km/sAtomic mass range 1. . . 350DaTarget area 130 cm2 or 8 cm2, automaticRelative atomic mass resolution m/dm at m=100 >200Sustained event rate >40 spectra/sCIDA instrument mass 10.4 kgPower consumption from 28V DC max. 15W

CIDA Spectrum (Encounter)

The CIDA 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, and contributed mechanics.

The Bergische Universitat und Gesamthoch-schule Wuppertal (BUGH) participated in devel-opment of the detector amplifiers and the data ac-quisition unit FDAQ.

The Finnish Meteorological Institute (FMI),Helsinki, Finland, provided the CIDA flight soft-ware, the GSE, and operational support.

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

The Institut d’ Astrophysique Spatiale (IAS), Or-say, France, provided the low voltage converters.

The Jet Propulsion Laboratory (JPL), Pasadena,USA, contributed electronical components.

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

CIDA on STARDUST S/C

STARDUST Launch

NASA photo

CIDA Timeline

End 1994 Study on Large Area DustImpact Spectrometer (LADIS) byvH&S on DLR contract.

June 1996 First CIDA interface meet-ing of vH&S with Lockheed-Martin Astronautics (LMA) inDenver, CO.

May 1998 vH&S delivers the CIDAflight model to LMA.

7 Feb. 1999 STARDUST launch fromCape Canaveral.

2 Jan. 2004 Comet Wild 2 encounter.

15 Jan. 2006 Return of STARDUST’sdust sampling capsule to Earth.

Happy PI with CIDA

CIDA Block Diagram

VoltagesVarious

Bus I/F

(+15

V D

C)

Kee

p A

live

Line

(+28

V D

C)

Sup

ply

Pow

er

Protection

Clock

cidablk.fig

Mul

tiple

xer

LMA 21020

ElectronMultiplier

Isol

atio

nT

rans

form

ers

PA

MM

odul

ator

s

Isolating Power Supply

Supply

Channel

Channel

+1000V

Log.

Am

ps

Red

unda

ncy

Sw

.

"MM−1"

−1000V

Regulators

Dust

SignalsVarious

+1100V 0V

High Sens.

Low Sens.

Target

Signal0V

Electronics BoxDetectorModule

Reflector

Spacecraft Interface

HV

−S

afe

HV−Safe

J1 (RS

−48

5)S

eria

l I/O

(0V

/5V

)P

ower

On/

Off

J2 J3

DPU

CID

A B

us

Latch−Up

(Ampl./Pol.)HV Control

Flash ADC

Flash ADC

EventTrigger

UnitFIFO Control

Boot PROM

Program RAM

Watch Dog

EEPROM

Bus I/F

Backup RAM

Data RAM

Event FIFO

Event FIFO

Low VoltageConverters

Serial I/FSynchronous

Amp

ConvertersHigh Voltage

Ion Path

UnitKeepingHouse

Drift Tube

TargetCPU

CIDA Measurement PrincipleCIDA is a Time-Of-Flight (TOF) mass spectrometer with impact ionization:

1 impact =⇒ 1 spectrum!

• Cometary or interstellar dust hits a flat silver target, which is exposed to space.

• The high-velocity impact leads to instantaneous decomposition and ioniza-tion of the dust particle.

• The generated ions (pos. or neg.) are accelerated by electrical fields (polarityselectable), and travel fixed distance through drift tube and ion reflector.

• A stacked dynode multiplier (MM-1) with set of logarithmic amplifiers is usedto detect the ions.

• The arriving ion charge is digitised by a pair of fast transient recorders.

• The mass spectra are calculated from the time-of-flight spectra.

Technical Highlights

Ion detector MM-1 Electron multiplier stack of 20 dynodes. Ad-vantages: Flat surface → precise end-of-flight. Excellent pulsehandling due to high electrode conductivity. Access to inter-mediate dynodes.

Logarithmic amplifiers Log. stage by UHF transistor arrays. Redundant de-sign, two low/high sensitive channel pairs. Integrated test pulses.

Triggering Weighted integral and pulse trigger modes.

Bipolar Stacked HVCs Polarity switchable for analysis of pos. or neg. ions.

Software Totally and automatically relocatable software to survive memory er-rors. Hand optimized Rice compression for the spectra.

The CIDA ProjectThe PI Dr. Jochen Kissel proposed theCIDA experiment, and is leading theoverall investigation. CIDA has beendeveloped, manufactured, tested, anddelivered by company vH&S as primecontractor.The CIDA Project has been fundedby the DARA/DLR, and the nationalspace agencies of the team members.

CIDA Contact, Links

CIDA 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/cida-stardust/press/cidaposter-a4.pdf

FMI CIDA Homepage http://www.geo.fmi.fi/PLANETS/cida.html

STARDUST Homepage http://stardust.jpl.nasa.gov

Literature“Assignment of quinone derivatives as the main compound class composing ‘interstellar’grains based on both polarity ions detected by the ‘Cometary and Interstellar Dust Analyser’(CIDA) onboard the spacecraft STARDUST”, F. R. Krueger, W. Werther, J. Kissel, and E. R. Schmidt,In: Rapid Commun. Mass Spectrom. 2004; 18: 103–111.“The Probable Chemical Nature of Interstellar Dust Particles Detected by CIDA Onboard

STARDUST”, J. Kissel, F. R. Krueger, J. Silen, and G. Haerendel, In: Proc. COSPAR Coll. Potsdam, July2000. (Eds.) K. Scherer et al. Vol., Pergamon Press, 351–359, 2001.“Cometary and Interstellar Dust Analyzer for comet Wild 2”, J. Kissel, A. Glasmachers, E. Grun,H. Henkel, H. Hofner, G. Haerendel, H. von Hoerner, K. Hornung, E. K. Jessberger, F. R. Krueger, D.Mohlmann, J. M. Greenberg, Y. Langevin, J. Silen, D. Brownlee, B. C. Clark, M. S. Hanner, F. Hoerz, S.Sandford, Z. Sekanina, P. Tsou, N. G. Utterback, M. E. Zolensky, C. Heiss, In: Journal of GeophysicalResearch, Volume 108, Issue E10, pp. SRD 4–1, 10/2003.

Contribution EGU04-A-07474 for the EGU – 1st General Assembly, Session PS5, Poster Area Palais des Exposition, Mo., 26 April 2004. Rev. 23 April 2004 (1.53). Poster by pdfTEX.

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