Space Line of Business - Euroimpresa LoB Presentation - Oct... · Avionica are carrying out the...

Space Line of BusinesspPresentation

Galileo Avionica S.p.A and SELEX Sensors & Airborne Systems Limited - Finmeccanica Companies

FINMECCANICA

Chairman & CEO: P.F. Guarguaglini

General Manager: G. Zappa

Co-General Manager: R. PerticaCo-General Manager: A. Pansa

AERONAUTICS SPACE HELICOPTERS DEFENCE ELECTRONICS

Alenia Aeronautica

Alenia Aeronavali Telespazio

Thales Alenia Space AgustaWestland

SELEX Sistemi Integrati

SELEX GALILEO

Alenia Aeronavali

ATR Integrated

Alenia Aermacchi

Telespazio g

SELEX Communications

SELEX Service Management

DEFENCE SYSTEMS TRANSPORTATION ENERGY

Quadrics Elsag-Datamat

Elettronica

Orizzonte Sistemi Navali

Oto Melara

WASS Ansaldo STS

AnsaldoBreda Ansaldo Energia

Galileo Avionica S.p.A and SELEX Sensors & Airborne Systems Limited - Finmeccanica Companies2

MBDA Bredamenarinibus

Joint Ventures Owned Companies

FINMECCANICA - Business Overview

Consolidated data 2007Finmeccanica isRevenues 13.4 B€Backlog 39.3 B€New orders 17 9 B€

Finmeccanica isa world leading group in aerospace, defence and security and a global provider of energy and transport solutions New orders 17.9 B€

R & D 1.8 B€Employees 60,748

AERONAUTICS HELICOPTERS DEFENCE SYSTEMS

transport solutions.

15 % 22 % 10%

DEFENCE ELECTRONICSTRANSPORTATION SPACE ENERGY

15 % 22 % 10%

11 % 29 % 6% 8 %


11 % 29 % 6% 8 %

SELEX GALILEO

Operating internationally as a single OrganisationOperating internationally as a single Organisation, SELEX Sensors and Airborne Systems Ltd and Galileo Avionica SpA have adopted a common brand: SELEX GALILEO

Galileo Avionica S.p.A.

SELEXSensors and Airborne Systems Ltd

For all legal and export purposes the company names will remain Galileo Avionica S.p.A., an Italian registered company and SELEX Sensors and Airborne Systems Limited a UK registered company


SELEX Sensors and Airborne Systems Limited, a UK registered company.

SELEX GALILEO

OUR VISION

“Delivering to our Customers total awareness total protection

OUR VISION

total awareness, total protection. Help them see, keep them safe”

SELEX GALILEO is committed to developing and sustaining, throughcontinuous innovation, the most accurate and reliable systems to see,hear and feel the situation our users are facing and to enable them aneffective and timely reaction to keep themselves and those they are

t ti t f h ’protecting out of harm’s way.


SELEX GALILEO

Key data 2007SELEX GALILEO offers integrated sensor solutions and through life capability management for defence systems and

Revenues 1,755 M€Order Intake 2,429 M€

Key data 2007

homeland security applications.

SELEX GALILEO l it

Backlog 4,364 M€Employees 7,050

SELEX GALILEO leverages on its international strengths to deliver powerful, innovative solutions and by forging and

t i i l di t hisustaining leading partnerships.

SELEX GALILEO is a leader in surveillanceSELEX GALILEO is a leader in surveillance, protection, tracking, targeting, navigation & control and imaging systems.


SELEX GALILEO

SELEX GALILEO works through 6 Lines of Business:

Air Systems, Unmanned Air Systems and Simulators

Electro Optics and NavalElectro Optics and Naval

Electronic Warfare and Battlespace

Radar and Advanced TargetingRadar and Advanced Targeting

Space

Land Systems, Support and Service Solutions


MAJOR OPERATIONS


SELEX GALILEO Organisation


Space Line of Business Organisation


Space Line of Business Engineering Organisation


Completed space programs (major)

COSMO SKYMED I-II-III (ASI/MOD)• PCU (Power Control Unit)

ROSETTA (ESA)• VIRTIS - (VIS-IR Thermal Imaging Spectrometer)

GIADA (Grain Impact Analyser & Dust• PPDU (Power Protection Distrib.Unit)• CPSU (Central Payload Supply Unit)• TPSU (Tile Power Supply Unit)• XDU (X-band Driver Unit)• ASTR (Autonomous Star Tracker)• PVA (PhotoVoltaic Assembly)

• GIADA - (Grain Impact Analyser & Dust Accumulation)

• SD2 - (System)• Navigation camera• ASTR• Solar panels for Orbiter & LanderPVA (PhotoVoltaic Assembly)

• SAPS (SAR Antenna Power Supply)Status : I and II in flight, III ready for launch

CASSINI HUYGHENS (NASA/ESA/ASI)

Status : in flight

ERS2 – METOP I, II, III (ESA)• GOME / GOME 2 (Global Ozone Monitoring

Experiment)CASSINI-HUYGHENS (NASA/ESA/ASI) • HASI (Atmospheric Structure Instrument)• VIMS (Visible Mapping Spectrometer)• SRU (Stellar Reference Unit)• TX Chain (for Titan Radar Mapper)Status : in flight

DAWN (NASA)• VIR-MSStatus : in flight

p )Status : in flight, METOP II and III ready for launch

g Status : in flight

SKYNET V (4 Satellites)• UHF Solid State Power AmplifierStatus : two satellites in flight

SOLAR SYSTEM (NASA)• ASTRCustomers: JPL, JHU-APL, LMSSC, Goddard, AMESStatus : in flight/ready for launch

VENUS EXP. (ESA/ASI)• VIRTIS• ASTR

Status : two satellites in flight g y

DAWN


• ASTRStatus : in flight

METOP

METOP

Running space programs (major)

COSMO IV• Same supply as COSMO Skymed

SICRAL 1B• Power System• X-KA Band TWTA

B. COLOMBO

GALILEO CONSTELLATION• PHM (Passive Hydrogen Maser)• DC/DC Converter for SSPA (Solid State Power Amplifier)• IRES N2 (IR Earth Sensor 2nd generation)

ALADIN

X KA Band TWTA• UHF SSPA• Frequency Generator• IRES• Sun Sensor

ALADIN• IRES-N2 (IR Earth Sensor 2nd generation)

AELOUS - ALADIN (ESA)• TXA (LASER)

Automatic Transfer Vehicle (5 flights)•PhotoVoltaic Assembly•Power Control Distribution Unit•Solid State Power Amplifier

Jules Vernes first ATV flight succesfully docked

BEPI COLOMBO (SCI. ESA/ASI)• SIMBIOSYS (Cameras & Spectrometer - ASI)

ISS (INT. SPACE STATION)• FASTER: Microgravity experiment facility

( )• PVA (PhotoVoltaic Assembly)

Jules Vernes first ATV flight succesfully docked the ISS

LISA PATHFINDER (ESA)• Sun Sensor• Photo Voltaic Assembly• FEEP (Field Effect Electrical Propulsion)

SIMBIOSYS (Cameras & Spectrometer ASI)• AA-STR (ESA)

FASTER

ATVLISA PF


METOP

Running space programs (major)

AURORA EXOMARS

AURORA (EXPLORATION ESA/ASI)• Driller & Sample Preparation Distribution (ESA)• In Situ Science Instruments (ASI)

GMES (EARTH OBS. ESA)• Sentinel 3 SLSTR (Sea Land Surface

Temperature Radiometer)

EARTH CARE (EARTH OBS. ESA)• ATLID TxA (Atmospheric LIDAR Transmitter

Amplifier)• CPR HPT (Cloud Profiling Radar High Power

Transmitter)

GAIA (ESA)• RVS (Radial Velocity Spectrometer)• RBP (Red and Blue Photometer)• ASTR (Autonomous Star Tracker)• PCU (Power Converter Unit)

GAIA

JUNO (SCI. NASA/ASI)• JIRAM (IR Spectrometer- ASI)• ASTR (NASA)

PRISMA (EARTH OBS. ASI)• Hyperspectral Payload• ASTR

PVA

( )• PVA (PhotoVoltaic Assembly)

ASTR (NASA)• PVA• Power System

EARTH CARE ATLIDPRISMA


SPACE PRODUCTS

Spaceborne Attitude Sensors

AA-STR SSS SOLAR SENSORIRES-N2 SIREUS MEMS RATE SENSOR

Electro-Optical Instruments

VIMS[CASSINI]

GOME[ERS2,METOP]

VIRTIS[ROSETTA,VEX,DAWN]

NAVIGATION CAMERA[ROSETTA]

ALADIN LASER Tx[AEOLUS]

HYPERSPECTRAL PAYLOAD


[ ][ , ] [ , , ] [ ] [AEOLUS][PRISMA)

Space Products

Power Equipment

Main Regulator Unit Power Control UnitSolar Panels Field Emission Electronic Propulsion Power Control Unit

Robotics & AutomationRF Equipment

Power Control Unit

Robotic PayloadPassive Hydrogen MASER

Atomic ClockSolid State Power Amplifier Sampling & Drilling

S


Atomic Clock System

Space Products

Scientific Research Products(Ground Astronomy)( y)

ASTRONOMICAL TELESCOPES

LTA / LTTLTA / LTTESO & Subaru

Microgravity Equipmentg y q p

FASTMITE

E i t ll d f ilitiBDPU


Experiment cells and facilitiesExperiment cells and facilitiesExperiment cells and facilities

Solar Generators

Galileo Avionica are active in the solar array field since 1984 offering both Solar Array (fixed and body-mounted) and PVA (PhotoVoltaic Assembly) design and lay-down based on:

• GaAs bare solar cells technology from CESI (I), Azur Solar Space (D) and Emcore (USA)

Si bare solar cells technology from Azur Solar Space (D) Sharp (J)• Si bare solar cells technology from Azur Solar Space (D), Sharp (J),• Lay-down on Al/Al, CFRP/Al honeycomb panels insulated with a kapton/fiberglass layer,• Soldering and parallel gap resistance welding joining technologies using Ag, Invar/Ag,

Invar/Au and Mo/Ag interconnectors


Electrical Power Systems & Equipment

• Galileo Avionica are European Leader in Electrical Power Systems and Power Equipment forscientific, remote sensing and telecommunication satellite applications.

• The Electrical Power Systems are composed of standard, flight proven functional blocks (such asS l A P C diti i B tt Ch d Di h M i B P Di t ib ti dSolar Array Power Conditioning, Battery Charge and Discharge, Main Bus Power Distribution andProtection, ...) assembled into dedicated box(s) meeting Customer requirements.

• The Power Equipment are designed and manufactured for different applications, ranging from a fewWatt up to 6 KW (and from a few V up to 40 KV), with different topologies and power conversiontechnologies, both for Platforms and Payloads.

Multiple Output DC/DC Converters- Converters for Payload supply

Power Systems and Platform Equipment

Converters for Payload supply- EPC for SSPA / FGU- Converters for Equipment internal

auxiliary supply

Specific Application High Voltage Power Supply- EPC for TWTA


- Converters for Electric Propulsion

RF Equipment

Since mid ’60s, Galileo Avionica design,develop and manufacture severaldevelop and manufacture severalequipment types, all possibly including theirMain bus DC/DC converter and TT&Cinterface. Frequency Generators and Converters

• Frequency Generators• Modulators and Frequency Converters• Chirp Converters & Transmitters for SAR

Power AmplifiersSolid State Po er Amplifiers

MPM composed of:EPC, STWT and Champ / Lin.MPM composed of:EPC, STWT and Champ / Lin.


Passive Hydrogen MASER

• Solid State Power Amplifiers• TWT Amplifiers

Automation & Robotics Systems

Mechanical unit

Harness

Mechanical unit

Harness

• Manipulators,Sensorised End Effectors,Control and Drive Electronics,

SERVICING SYSTEMSElectronic unit

Drill-Sampler tool

Electronic unit

Drill-Sampler tool ,High Power Density Actuators;Drill & Sample Preparation Distribution Systems,Mechanisms for Planetary Exploration;

SAMPLING SYSTEMSMechanisms for Planetary Exploration;for complex, high reliability application.MOTION CONTROL SOFTWARE


Spectral Imaging and Spectrometry

Galileo Avionica started the activity in the field of hyper-spectral spaceinstrumentation in the middle ’80s with the design and production of GOME-1,successfully flying on board of ERS-2 since 1995. For the time being, GalileoAvionica are carrying out the design of state-of-the-art optical instruments andhyper-spectral imagers devoted to both Earth and planetary / cometaryobservation; Galileo’s spectrometers are now flying on board of METOP,Cassini Rosetta and Venus Express missionsCassini, Rosetta and Venus Express missions.Leveraging on the capabilities acquired in the space field, Galileo Avionica hasdeveloped a demonstrator for airborne operations (SIMGA), which is nowpresented on the market, both for monitoring / security and militaryapplications. Demonstration flights have been performed with very attractiveresults.On the basis of all the background above, GA have started the developmentof an hyperspectral payload to be flown on a dedicated small mission, namelyPRISMA. This demonstration mission is considered as a precursor for a futuredual use mission to be agreed with National Defence authoritiesdual use mission to be agreed with National Defence authorities.


PRISMA

LASER Technology

G lil A i i i d l i h

LASER Technologies

Galileo Avionica is developing the Laser Transmitter Assembly (TXA), an all-solid-state laser source, for the Aladin instrument of ESA mission ADM/A l

ADM-AEOLUS missioncredits: ESA AOES Medialab

ADM/Aeolus.

• Laser Material:Nd-YAG

LASER CharacteristicsALADIN – credits: ESA

• Wavelength:1.06 + 0.532 + 0.355 µm• Pulse Energy:500 mJ @ 1.064 µm;

150 mJ @ 0.355 µm

• Pulse Length:15 nsg• Pulse Repetition Rate:100 Hz (burst mode)• Single Longitudinal and Transverse Mode• Frequency tunable (>15 GHz @ 1.064 µm)• Volume: 30 l Weight:28 kg


Volume: 30 l Weight:28 kg• Power: ≈ 500 W AVGALADIN PLH unit

Attitude Sensors

Star Trackers

Galileo Avionica have developedGalileo Avionica have developed more than 50 Flight models, all

working without failures

ISO STRGalileo Avionica started the production ofAttitude Sensors (AS) in the 60’s

Autonomous STR

Attitude Sensors (AS) in the 60 sThe task of the AS is to provide the attitude and /

or the spatial coordinates to the satellite; according to the mission, the reference used are

the stars the Earth or the Sun

Earth / Sun Sensors

G lil A i i h d l d

the stars, the Earth or the Sun

Galileo Avionica have developed more than 300 Flight models, all working

without failures


Earth sensor: IRESSmart Sun Sensor: SSS

Gyro sensors

Roadmap of satellite gyro Gyro

SELEX GALILEO started the activity in the field of gyro sensors in the ’70s.

All units were based on the mechanical type 125 Gyro. The first productserie was named DIRA Mk1 and was delivered to ESA, Space SystemL l d Th l Al i S It l (f Al i S i )

DIRA Mk 1

Loral and Thales Alenia Space Italy (former Alenia Spazio).

The second product serie, DIRA Mk2, was delivered to NASA and toThales Alenia Space Italy (former Alenia Spazio) for COSMO/Skymed andRadarsat-2 programmes.

Over 60 DIRA Gyros delivered to scientific

DIRA Mk 2 SELEX Galileo started in 2005 the study of a new class of gyros, the SiREUS, making use of MEMS technology for the sensor. This new generation gyro serie will fit the needs of a wide community of commercial customers, delivered to scientific,

telecomms and Earth observation missions

Si MEMS Gyro

yincluding micro and mini sat suppliers.

SiREUS will be launched on Cryosat 2.

ESA MRS development contract awarded in 2005


SiREUS

Laser Telescope Assembly (LTA/LLT)

•

LTA/LLT is an instrument specifically designed tosupport some of the biggest ground telescopes of thesupport some of the biggest ground telescopes of theworld to correct or mitigate the effects of the airturbulence on the astronomical objects, enabling theobservation of very faint astronomical objects.

The LTA/LLT is a beam expander telescope used toproject an artificial image of a star on the higherlayers of the atmosphere; the 500 mm telescopeworks at the wavelenght of 589 15 nmworks at the wavelenght of 589.15 nm.•Telescopes with LTA/LLT• Very Large Telescope (VLT) – ESO

S b / NAOJ H• Subaru / NAOJ – Haway• LTA / Keck Observatory - Hawaii


Micro-gravity

G lil A i i h li d i t d f iliti f

FAST

Galileo Avionica have realized many experiments and facilities formicro-gravity; the development of these instruments required strongeffort in hydraulics / vacuum technologies, in optics, electronics &precision mechanics.A li ti t i f h i f fl id lif i d iApplications cover topics of physics of fluids, life science and micro-gravity effects on humans; the experiments have used as carriersounding rockets, airplanes (parabolic flights), Shuttle flights and theISS.

ESS EMEC

TEXUS sounding rocket (credits: ESA)


TEXUS

Space Solar Generatorsp

Space Solar Generators

• Photovoltaic Assembly (PVA) network for a id li ti d (f t lwide application spread (from nano to large

space crafts)• Turnkey solar generators for nano, micro and

small space craftsp• Body mounted • Deployable for small application only

Technologies:• Technologies:• Si and GaAs (single and multi-junctions) solar cells with

state-of-the-art efficiency:- Si: 17% AM0, Beginning Of Life;- GaAs Triple junction: 28% AM0 Beginning Of Life;GaAs Triple junction: 28% AM0, Beginning Of Life;

• Lay-down on different material as: CFRP, Al and fibreglass;

• PVA processing capability up to 9 m2 panels;• welding and soldering joining technology;

Galileo Avionica have participated to themost important and recent ESA programs• welding and soldering joining technology;

• protection against atomic oxygen erosion (ATOX), available as option;

• immunity to electrostatic discharges (ESD cleanliness) using conductive glasses available as option

p p gsuch as Rosetta, ATV, PROBA, Herscheland Plank, ADM Aeolus, GSTB-V2,PROBA 2, LISA PathFinder, GAIA and tothe LEO constellations COSMO SkyMed

17/11/2008 2

using conductive glasses, available as option. yand Pleiades

Space Automation & Robotics

Sampling Systems

Drill systems:y• Single rod• Multi-rod• Sampling depth: up to some metersSampling depth: up to some meters• Sample dimensions: from some tens of mm3

to some cm3• Soil type: from not cohesive to rocksSoil type: from not cohesive to rocks

Sample distribution/preparation mechanisms:

• Based on single carousel or more complex• Based on single carousel or more complexDrill deployment devices:

• Articulations with 2 - 4 degrees of freedomE i t l diti d t Drills main physical characteristicsEnvironmental conditions: down to -160°C in vacuum/low pressure Application: sampling of Moon, Mars,

Drills main physical characteristics• Dimensions: 150x200x600-800 mm• Mass: 4-8 kg• Power in operation: 5 to 50 W• Power in St-by: 1 to 5 W

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Comets, Asteroids • Power in St-by: 1 to 5 W

Servicing Systems

Dextrous Robot Arm:• 7 degrees of freedom• joints equipped with high performance three-

phase brushless motor redundant positionphase brushless motor, redundant position sensor, brake, torque sensor

• servo control electronics embedded in each jointjoint

• arm P/L capability: some kg in 1g condition• arm size: 1.3 meter

Joint main characteristics• arm mass: 26 kg

Control SW:• multi arm coordination control SW

Joint main characteristics• torque: 100 - 200 Nm sustained• accuracy: 0.0004 rad• repeatability: 0.00004 rad• speed: 0 3 rad/s• multi arm coordination control SW

• position, force, torque, hybrid control• speed: 0.3 rad/s• diameter: 112-130 mm• length: 175 – 185 mm• mass: 2.9 to 3.5 kg• Power: 20 W at 100Nm stall condition

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• Power: 20 W at 100Nm stall condition

Space Line of Business - Euroimpresa LoB Presentation - Oct... · Avionica are carrying out the...

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