Kayser-Threde GmbH Company Presentation - dlr.de · Kayser-Threde GmbH w w w . k a y s e r ... 12...

Kayser-Threde GmbH

w w w . k a y s e r – t h r e d e . c o m

Kayser-Threde GmbH


w e . c r e a t e . s p a c e .

Company PresentationSpace Industry Days, 27./28.10.2010, Munich

Dr. Eckart Wulf

Kayser-Threde

Space

Industrial Applications

09/20102 Company Presentation An OHB Technology Company

A Leading Systems House Providing High-Technology Solutions

Kayser-Threde, founded in 1967, designs, develops and manufactures instruments and systems for:

Space

Industrial Applications.

‚From Earth to Space – and Back‘

Close links with science community (technology)

Access to industrial markets

Continuous transfer of space technology into markets

Clearly-defined portfolio

Our strength is our size – High flexibility and innovation.


The Owner: OHB Technology Group

KT is member of the group since 2007


Organization


2004 2005 2006 2007 2008 2009

Total Revenues [M€]

Process Control Systems

Automotive (until 10/2009)

Space

38,934,6 33,6

39,142,4

62,4

Order Backlog: 81 M€ per 31.12.2009

Others 5%

ESA 28%

DLR 67%

Incoming Space Orders 2005-2009


Our Customers and Partners

Projects mostly funded by German Government through

DLR and ESA

Strong cooperation with research institutions (e. g. Max-Planck-

Society, Helmholtz Association) and Universities

Lang standing relations to all major industrial players in

Germany and Europe


High-Tech solutions by Kayser-Threde:

Majority of employees has an academic background

Experienced teams of technicians.

291975

1985

1995

2000

99

161

220224

Human Resources

2010

240*)

*) After sale of KT Automotive GmbH

2005


Space Business: Small Satellites and Scientific Instruments - on earth, in space and in between -

EnMAPTET 01

Studies, R&D Projects, Recurrent projects (e.g. TEXUS / MAXUS, SOFIA-operation)

ExoMars Rover MERTISWendelstein Telescope PACSPK 4 SUNRISE


Spectral “Bandwidth” of Kayser-Threde


Process Control Systems Power Supply Monitoring for German Railroad: From Control Centre to Switch – and Back

Network control (SCADA) systems

Process coupling

Small SCADA systems

Communication systemsProtocol converters

Telecontrol systems

Network and remote service security

Substation control systems

Screen control

Centralized systems

Decentralized bay controllers

K1800-40: Substation control system with screen control and field modules with integrated telecontrol, as well as control and conversion technology.


Our Competences

Absolute Customer Orientation

Process Oriented Project Management and

System Engineering

Excellence in various Engineering Disciplines

Professionalism in Design

Skills in Manufacturing

Dedicated AIT Facilities

Certified Quality Management


Management & System Engineering

Established Processes, e. g. Risk Management Project Planning & ControlSubcontractor ManagementConfiguration & Change ManagementRequirement Tracing

DOORS

Requirement Tracing

AnforderungsdokumentKunde

AnforderungsdokumentSystem

AnforderungsdokumenteSubsystem

Links: erfüllt

Links: erfüllt

TestprozedurenSystem

Links: verifiziert

TestprozedurenSubsystem

Links: verifiziert

- Anforderungsanalyse- Compliance Matrix- Abwärtsverfolgung

- Verifikationsnachweis

DOORS Views

- Compliance Matrix- Aufwärts-/Abwärtsverfolgung

- VerifikationsnachweisDOORS Views

- Compliance Matrix- Aufwärtsverfolgung

- VerifikationsnachweisDOORS Views


Mechanical Engineering

Modal Analysis Enforced Displacements Strength Analysis

Lateral excitation (y-axis)

0.01

0.10

1.00

10.00

1 10 100

Frequency [Hz]

Acc

eler

atio

n [g

]

Main platform sensor 52y

Vibration Test Prediction Measured Accelerations


Thermal Engineering

Radiator Temperature over 5 Orbits

-40

-39

-38

-37

-36

0 60 120 180 240 300 360 420

Time [min]

Tem

pera

ture

[°C

]

0

2

4

6

8

10

Exte

rnal

Hea

t Flu

x [W

]

Radiator diameter: 0.5mMass: 2kgExternal heat load: transient total heat f luxDissipation: 3.25W

Temperature Variation

Temperature Distribution

Orbit Simulation

Design and Verification; Selected Typical Tasks – Thermal Analysis


CODE V, ZEMAX

ASAP

NASTRAN

CATIA V.5

Image optimization and analysis

Stray-light and advanced image analysis Mechanical design

Static, dynamic, thermal surface deformations and displacements

Zernike Polynominals

IGES

IGESIGES

IGES

Zern

ike

Poly

nom

inal

s

Integrated Design Process Interfaces


Prototyping and manufacturing of electronic units for space projects

SMD manufacturingcertified accordingECSS-Q-70-38

Machine aided PCB assembly (pick-and-place)

Reflow soldering machines

Gluing and coating activities

Harnesses for satellites

Integration of electronicSubsystems

Electrical Manufacturing and Integration

Four rooms with a total area of 185 m² (cleanroom class ISO 8):


Mechanical Workshop

About 500 m² for mechanical manufacturing assembly and integration.Various CNC milling machines, e. g. HermleC 40 U (5 axes, photo left top)Lathe and drilling machines Presetting and Measuring Devices, e. g. ZollerSmile 400, Universal (photo left bottom)


160 m² high bay area for integration of large equipment and small satellites,cleanliness class ISO 8

160 m² high bay area for integration of large equipment and small satellites,cleanliness class ISO 8

Clean Rooms

Clean Room for optical instruments50 sqm, Cleanliness ISO 5/6Temperature controlled, 0.2 K

Clean Room for optical instruments50 sqm, Cleanliness ISO 5/6Temperature controlled, 0.2 K

TV chamber-160 deg … +180 degRemotely controlled

TV chamber-160 deg … +180 degRemotely controlled


Company Sites

Wolfratshauser Str. 4881379 München

Tel.: (089) 72495-0

Fax: (089) 72495-291

[email protected]

Perchtinger Str. 581379 München

Tel.: (089) 72495-500

Fax: (089) 72495-482

[email protected]

Kayser-Threde GmbH


Kayser-Threde GmbH



KT Engineering CompetencesDr. Stefan Bedrich

Director Engineering, Kayser-Threde

DLR-Raumfahrtindustrietage, München, 27./28. Oktober 2010

Space


28/10/20102 Engineering - Raumfahrtindustrietage München An OHB Technology Company

Organisation

� 6 Abteilungen

� Alle „klassischen“ Disziplinen

� Etwa 7 bis 25 Mitarbeiter pro Abteilung

� Insgesamt etwa 90 Mitarbeiter

� Akademiker-Anteil ~90%


Selbstverständnis

■ „KT Engineering“ entwickelt, analysiert, produziert und testet Komponenten, Baugruppen

und Systeme

■ Im Team für die „internen Kunden“ Vorentwicklung (Phasen 0/A/B1) und Projekte (Phase

B2/C/D) sowie eigenverantwortlich für externe Kunden, Focus auf neue Technologien

■ Nahezu alle Geräte haben Prototyp-Charakter („Einzelstücke“), begründet durch die Natur

des – primär wissenschaftlichen – Kundenkreises

■ Kunst ist, den Innovationscharakter der Entwicklungen zu befriedigen und trotzdem

wiederkehrende Methoden, Prozesse und Erkenntnisse einzubringen

■ Entwickler (el./opt./mech.) ist in der Regel in gesamten Produktentstehungszyklus

eingebunden (bis hin zur Testunterstützung während AIT), um zu erleben, was „sein“

Design in der Praxis wirklich zu leisten vermag

■ Archivierung des Know-Hows in einer Datenbasis zur Nutzung von „recurring engineering“-

Anteilen in neuen Projekten.


Expertise:

� Optisches Engineering und

Design

� Optische Analysen: Ray

Tracing, Streulicht, Radiometrie

� Performance-Verifikation und

Kalibration des analytischen

Modells

Tools:

� ZEMAX

� CODE V

� ASAP

� Matlab

Optik

CODE V, ZEMAX

Interferogram Measurement

Image optimisation and analysis

Zernike or Interferometer-File

Verified End-to-End Image Performance

NASTRANStatic, dynamic, thermal surface

deformations and displacements

Defined S

tatic L

oads


Expertise:

� Konstruktion

� Strukturberechnung

� Thermalberechnung

� Verifikation

Tools:

� Catia V5, Inventor

� NASTRAN/Hyperworks

� Femap

� Esarad/Esatan

� Matlab

Beispiel: Sunrise Teleskop

EigenfrequenzberechnungCAD-Design

Thermalmodell (inkl. Gondel)

Temperaturverteilung

am Hauptspiegel

Mechanik


Elektronik

Schwerpunkte:

� Front End Electronics

• ICU

• Signal Conditioning

• Power Supply

� Telecom Components

Tools:

� CAD Mentor

� ADS Agilent

� VHDL & Modelsim

� PSpice

� LabVIEW

� Div. Mess-Equipment

(Network Analyzer,

Logic Analyzer, …)SiGe RF MMICs: (5GHz to 20 GHz) Synthesizer

Nutzlast Versorgungssysteme

Signal-Konditionierung,

ICUs, Stromversorgungen


Software

Schwerpunkte:

� Onboard-S/W für

eingebettete (Echtzeit-)

Systeme; spezialisierte

Hardware

� Bodenbetriebs-S/W mit

spezif. GUI (Test und

operationeller Betrieb der

Onboard-Einheit)

Tools:

� Objekt-Orientierung,

autom. Codegenerierung

aus Software-Modellen

� DOORS, Rhapsody,

LabVIEW, PolySpace,

CTC++

Software Struktur- und Verhaltens-Modelle für onboard/Ground:

Grafische Oberflächen:


� About 185m² for manufacturing/

integration of electronic units

� SMD manufacturing, certified

according ECSS-Q-70-38

� About 500 m² for mechanical

manufacturing, assembly and

integration

� Various CNC milling machines,

e. g. Hermle C 40 U (5 axes)

� Machine aided PCB assembly

(“pick-and-place”)

� Reflow soldering machines

� Gluing and coating activities

� Production of harnesses for

satellites (routing, worst case

analysis, mock-ups, brackets)

� EGSE/OGSE/MGSE for

integration and test of complete

subsystems

Manufacturing, Assembly & Integration


160 m² high bay area for integration

of large equipment and small satellites,

cleanliness class ISO 8

160 m² high bay area for integration

of large equipment and small satellites,

cleanliness class ISO 8

Testing & Clean Rooms

Clean Room for optical instruments

50 sqm, Cleanliness ISO 5/6

Temperature controlled, 0.2 K

Clean Room for optical instruments

50 sqm, Cleanliness ISO 5/6

Temperature controlled, 0.2 K

TV chamber

-160 deg … +180 deg

Remotely controlled

TV chamber

-160 deg … +180 deg

Remotely controlled


� Wir können nicht alles

� Wir machen nicht alles selbst

� Aber: wir möchten (fast) alles verstehen

� Wir brauchen Partner, die notwendige Technologien für neue Applikationen mitbringen und weiterentwickeln

bzw. für Raumfahrt-Anwendungen einsetzen wollen:

� Focal Plane Assemblies: Detektoren, FEE, schnelle Wandler + Rechner, …

� Mechanismen für optische und robotische Baugruppen

� Neue thermostabile und/oder hochfeste Materialien

� Hochpräzise Fertigungs- und Fügeverfahren

� Engineering Support (Konstruktion, Analyse, S/W-Entwicklung, AIT, …)

� …

Zusammenarbeit und Partner


For further questions please contact


Kayser-Threde GmbH

Wolfratshauser Str. 48

81379 München

Tel.: +49 (89) 72495-0

Fax: +49 (89) 72495-291

[email protected]

Kayser-Threde GmbH

Perchtinger Str. 5

81379 München

Tel.: +49 (89) 72495-500

Fax: +49 (89) 72495-482

[email protected]

Kayser-Threde GmbH


Kayser-Threde GmbH



MTG – KT Share & ProcurementsDr. Christoph BartscherKayser-Threde, München

Raumfahrt

Industrielle Anwendungen

28.10.20102 Raumfahrt Industrie Tage 2010 Ein Unternehmen der OHB Technology AG

Main Content

MTG Program Overview (Space Segment)MTG Core Team Structure and Responsibilities

– Kayser-Threde Work Packages– Best Practice Items under KT Responsibility


MTG Program Overview (Space Segment)4 MTG-I Satellites:

Flexible Combined Imager (FCI)Full Disc High Spectral resolution Imagery (FDHSI), 10min, 16 Channels, 1-2kmHigh spatial Resolution Fast Imagery (HRFI), ¼ Earth, 2.5min, 4 Channels, twice better resolution

Lightening Imager (LI), 10kmSearch and Rescue (S&R) Relay Service from GEOData Collection System (DCS) mission

2 MTG-S SatellitesInfrared Sounding Mission (IRS)

Hyperspectral sounding information, Long & Mid Wave Infrared, Info about water vapor distribution and movement

Ultraviolett, Visible & Near-Infrared (UVN, Sentinel-4), O3, NO2,SO2, HCHO


Mission RequirementsESA / EUMETSAT

MTG-I Mission PrimeMTG-I Satellite Prime

TAS

MTG-S Mission PrimeMTG-S Satellite Prime

OHB-System

MTG-S IRSInstrument Prime

KT

DEA & Interferometer Assembly

TAS

MTG-I FCIInstrument Prime

TAS

Telescope AssemblyKT

MTG Common Platform

OHB-System

MTG Core Team and Responsibilities


Main Components - IRS Instrument

IRS Instrument Data:Volume: 1.436 x 1.15 x 1.25 m3

Mass (nom/max): 295/353 kgPower (nom/max): 519/643 WData Rate: 153 Mbps

Interferometer

Imager (IBI)

Solar Baffle

I/F Panel

Cryostat

Back Telescope

Optical Bench

M3 Refocalization

Mechanism

Black Body

Interferometer

Imager (IBI)

Solar Baffle

I/F Panel

Cryostat

Back Telescope

Optical Bench

M3 Refocalization

Mechanism

Black Body

High Modularity!


IRS Procurements under KT12100 Optical Sounder Assembly:

12111. OBA: Optical Bench Assembly*12112. Telescope Optics*12113. Calibration & Obturation Mechanism*12114. Refocusing System/Mechanism*12120. IRS Scan Assembly*12140. Structure and Thermal Control

incl baffle mechanism*12150. In-Built Imager12161. Optical Bench Assembly (BT)12162. Telescope Optics (BT)ICU & Instrument SWGSE (OGSE, EGSE, MGSE)Harness, Engineering Support, Test Facilities

* Combined procurement with the common FCI-TA items.


Volume: 1.6 x 1.1 x 1.4 m3

Mass (max): 250 kgPower (max): 300 WData Rate: 55 Mbps

Main Components – FCI Telescope Assembly

High Modularity!


FCI-TA Procurements under KT

The Flexible Combined Imager (FCI) is composed of:The telescope assembly (12100)The spectral Separation & Detection AssemblyThe FCI Electronics

KT is responsible for the procurement of the Telescope Assembly (FCI-TA):

12110: MOA. Main Optical Assembly:12111* OBA. Optical Bench Assembly12112* Telescope Optics12113* Calibration & Obturation Mechanism12114* Refocusing Mechanism

12130* FCI Scan Assembly12120* Structure and Thermal ControlGSE (EGSE, MGSE, OGSE)Harness, Engineering SupportTest Facilities.

* items that shall be procured in combination with the common IRS items.


Planned ITT Process

The procurement follows the ESA Best Practice, all ITTs will be issued on EMITs. ESA, OHB-S and TAS review and approve all ITTs. Announcements in EMITs are made at least 2 weeks before ITT issue.Expected Subco minimum response time to ITTs is 6 weeks. An acknowledgment of intention to respond will be requested.The majority of the TEBs and TSBs are expected in 2nd and 3rd quarter 2011.Negotiations with the selected subcontractors will follow.Finalisation of the negotiations (80-90%) and contract signature before the end of phase B2.

Preparation of ITTs will start right after the KO of Phase B2For procurements directly under KT responsibility start of ITTs release approx KO + 4M. Some ITTs for very critical components will be released at KO + 1M (e.g. detectors) by TAS.

KT will ensure that each ITT will be in competition, i.e. there will be several bidders.

Key objective is to maximise the commonalities between FCI and IRS for combined or parallel procurements.


Main Commonalities for IRS and FCITAMain Optical Assembly consisting of:

Optical Bench AssemblyTelescope OpticsRefocusing Mechanism (M2)Calibration Mechanism

Scan Assembly: to ensure the complete Earth coverageElectronics unitMechanical unit

Structure and Thermal Control consisting of:Entrance and Baffle Assembly (incl. mechanism)Supporting StructuresThermal Control ItemsRadiator Assembly

Harness, GSE, Test Facilities, Eng. Support


Planned ITTs


Table of planned ITTs (KT & TASF)

Approx. 60% of MTG Budget available for Best Practice ItemsOpportunities for German companies also in TAS ITTsNo further break down planned Teaming building with European companies


GEO Return


MTG Master Schedule – Key MilestonesAssumed Kick-off in mid November 2010 und linear shift to original schedule (TBC by ESA)

Milestone Phase Date Relative Date AbsoluteKO B2 B2 T0 Nov 10SRR B2 T0+3M Feb 10PDR B2 T0+12M Nov 11Instrument PDR (IRS & FCI) C/D T0+15M Feb 12FCI & LI CDR C/D T0+38M Jan 14CDR-I C/D T0+44M Jul 14IRS CDR C/D T0+50M Jan 15CDR-S C/D T0+56M Jul 15QR-I C/D FAR-I -12M May 16QR-S C/D FAR-S -12M Oct 17FAR-I (MTG-I-1) C/D T0+78M (max) May 17FAR-S (MTG-S-1) C/D T0+96M (max) Oct 18

Com

mon

ality

!


MTG Program Manager: Dr. Christoph Bartscher [email protected]

MTG Procurement Manager: Manfred Leipold [email protected] Eduardo Bellido [email protected]

IRS Project Manager: Rupert Feckl [email protected]

FCITA Project Manager: Dr. Christoph Bartscher

MTG Contacts at KT

mailto:[email protected]





The End

Kayser-Threde GmbH


Kayser-Threde GmbH



Selected Space Projects

Missions, Science & Exploration, A&R, µg

Dr. Clemens Kaiser

Raumfahrtindustrietage München

28. Oktober 2010

Space


28/10/20102 Selected Space Projects - Raumfahrtindustrietage München An OHB Technology Company

EnMAP – Environmental Mapping and Analysis ProgramHyperspectral Sensor Development

Future German hyperspectral Earth observation mission

DLR and Kayser-Threde signedPhase C/D contract in November 2008, satellite to be launched in 2013

Kayser-Threde as industrial prime cooperates with GeoForschungsZentrumPotsdam (GFZ) as Prime Investigator

EnMAP will be the first full range HSI sensor with sufficient Signal to Noise performance which supports most relevant future tasks related to Global Earth Management in the areas:

Earth Dynamics and Risks ● Climate Change ● Water Availability and Quality ● Biodiversity and Ecological Stability ● Natural Resources ● Socio-political Aspects of Global Change


On-Orbit Verification TETTechnologie-Erprobungs-Träger • Technology Experiment Carrier

■ OOV-Program of the DLR serves to bridge the gap between the product tested and qualified on ground and the utilization of the product in space.

■ Kayser-Threde serves as Prime contractor for Phase C/D of the TET-1 mission including piggy-back launch.

■ The Technology Experiment Carrier (TET) comprises the core element of the OOV-Program.

■ TET satellite bus based on heritage of BIRD satellite bus.

■ Modular Payload Supply System newly developed.

■ Open satellite structure allows for flexible payload accommodation.

■ Designed for mission durations up to one year.

■ For Low-Earth-Orbits from 450 to 850 km.


Thomas Reiter with ETD onboard the space station (July 2006)

EyeTracking Device (ETD),life sciences

PK-3 Plus, complex plasmaphysics

Oil Emulsion Experiment (OEE), education

SKIN, dermatology

MELFI (-80°C freezer) for biological samples

Research with PK-3 Plus: T. Reiter workingwith the telescience unit (ISS, August 2006)

OEE SKIN MELFI

Thomas Reiter`s Long-Duration Mission Onboard Space Station ISS Instruments & Experiments with Kayser-Threde`s Contribution


P K EP K E28 VDC28 VDC

RS 422RS 422

Utilization of ISS Plasma Crystal Instruments

Telescience LaptopTelescience Laptop

PKE Launch: February 2001

13 PKE Scientific Missions from 2001 to 2005

PK 3 Plus Missions: since 2006

PK 4: Prime Responsibilityfor a complete new unitinside the EPM-Rack(under development)

Future facility: Plasma Lab


MERTIS: MERcury Thermal Infrared Spectrometer

Measuring the spectral emittancein the spectral range from 7-14 µm

Cartographic mapping of theMercury surface mineralogywith a high spatial resolution

Investigation of the surfacecomposition of Mercury

Global measurement of thesurface temperature (radiometricmeasurements in the spectralrange from 7-40 µm)

7 8 9 10 11 12 13 140.8

0.9

1.0

CF - Christiansen featureRB - Reststrahlen bands (Si-O absorptions)TF - Transparency feature

CF

RB

TF

Feldspars <25 µm

Anorthite Albite Orthoclase

Emis

sivi

ty

Wavelength (microns)


Fraunhofer Telescope WendelsteinOptical system key data:

Primary Mirror M1 Ø: 2m (F# 2,0)3 Mirror Ritchey Chrétien System F#Sys: 7,8 Field of View: 0,7° (optional 0,9°)

more that the full moon in one shot!2 Nasmyth Ports for science instrumentation(Wide Field Imager and Spectroscopy )Wide field camera port is equipped with a3 lens Field corrector, which optimizes the performance for the 4x4k CCD Mosaic (64 MPixel !!!) wide field camera

new 8,5m Ø Dome

primary M1

tertiary M3

secondary M2


DEOS Servicer- & Targetsatellite

KT responsible for:Docking, Berthing,Servicing (Lot 4)

H/W: Robotic Arm, ICU,Navigation Cameras,Docking Tool, ORUs

Docking & BerthingVerification usingEPOS

Docking & Berthingoperations & operationcontrol unit for GCC

Collaboration withGerman sub-contractors

Collaboration with GSOC and DLR Institute forRobotics & Mechatronics

On-Orbit Servicing - DEOS


WSO-UV Mission Overview

Word Space Observatory – UVHigh resolution UV astronomy with un-matched performance featuresin image, spectral and spatial resolution, magnitude and wavelength range

Customer: Lavochkin AssociationKey features:

Wavelenght range 104 – 310 nmDiameter M1: 1,7 m3 UV spectrographs

KT responsibilityInstrument prime for UV Spectrographs (WUVS)

UV Spectrographs

External InstrumentationPlatform (Electronics)

M1

Thermal StabilizedProtectiv Cover

UV Imagers


KT CONTRIBUTIONS to the EXOMARS ROVER

Sample Preparation & Distribution System KT: SPDS Mechanisms (level 1 subcontractor)

Rover

Raman/RLS(DLR funded)

High-resolution Camera (HRC)(DLR funded)

Sample Preparation & Distribution System incl. Crushing Station (SPDS) and Analytical Laboratory Drawer (ALD) (ESA funded)


EXOMARS SPDS

Core Sample Handling System

Crushing Station (stone crusher)

Powdered Sample Dosing and Distribution System

Powdered Sample Handling System


Potential Fields of Cooperation for Suppliers & Subcontractors

Engineering Support in all DisciplinesOptical Subsystems / Equipments / ElementsMechanismsStructuresThermal Control System and EquipmentElectronic Subsystems, E-BoardsHarnessSoftwareMGSE / OGSE / EGSE


For further questions please contact


Project ResponsiblesScience & Exploration: Dr. Thomas Zeh

µg: Ralf von Heise-Rotenburg

Orbital Services & Robotics / TET: Stefan Föckersperger

EO: Dr. Clemens Kaiser

ENMAP: Kai Lenfert

Subcontractor Management:Dr. Manfred Leipold, Sven Müncheberg, Eduardo Bellido, Werner Wilden

Business Development:Dr. Timo Stuffler / Dr. Peter Hofmann

Kayser-Threde GmbH Company Presentation - dlr.de · Kayser-Threde GmbH w w w . k a y s e r ... 12...

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Transcript of Kayser-Threde GmbH Company Presentation - dlr.de · Kayser-Threde GmbH w w w . k a y s e r ... 12...