pf_ohb-system ag_final [kompatibilit¤tsmodus]
TRANSCRIPT
SMALL GEOA Product for the Market
5th Capital Market Day, Bremen, February 11, 2009
Prof. Dr. Manfred FuchsCEO OHB-System AG
OHB-System AG | Bremen, February 11, 2009
Our Space
SPACE SYSTEMS + SECURITY
Page 2OHB-System AG | Bremen, February 11, 2009
MARKET REQUIREMENTS FOR SGEO
Geostationary communications satellites have been g etting bigger, but there is a market demand for Small GEO:Larger operators� Quick reaction to market needs� Short-term replacement� Careful testing of new markets
Small operators
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Small operators� Capacity of larger satellite not required� Minimization of financial and operational risk� Tailored to individual business� Avoidance of hybrid solutions � National satellite to serve the public needs
Replacement demand peaking in 2012The estimated market size is 7 satellites per year
BENEFITS OF SGEO COMPARING WITH A BIG SATELLITE
� Lower capital investment, thus lower risks and fast schedule
� Ideal for new market exploration and new services / technologies / verifications
� Better investment return through matching capacity uptake in a new market
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� Better investment return through matching capacity uptake in a new market
� Ideal for the desires from military to have an independent and highly secured space asset
� Cluster of SGEO provides redundancy and avoids total failure
Ideal for its niche with better investment return a nd lower risks
RESPONDING TO THE MARKET DEMAND
ESA established ARTES-11 program to develop the SGE O
� OHB-System signed the platform prime contract with ESA in November 2008 at the contract value of EUR 115 million
� OHB leads the European industrial consortium:
� Sweden
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The first commercial satellite mission contract wit h Hispasat was signed in November 2008 by ESA
Sweden
� Switzerland
� Luxemburg
LUXOR SATELLITE KEY FEATURES
� Up to 15 years lifetime
� Fast recurring delivery time
less than 24 months
� Launch Flexibility
LUXOR product: 3000 kg (GTO) and 1600 kg (GEO)
� Support a wide range of payloads up to 400 kg and 4 kW
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� Launch Flexibility
� Optimised for direct injection
� Apogee Engine Module for GTO option
� ITAR free design goal
Highly flexible and modular geostationary communica tion satellite
UP TO DATE FLIGHT PROVEN TECHNOLOGIES
Up to date flight proven technologies
� Li-Ion batteries� Electrical propulsion (two manufactures)� Triple-junction GaAs solar cells� LEON II – FT flight processor� Star Tracker based ACS� MIL standard 1553B & optional CAN Bus
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� MIL standard 1553B & optional CAN Bus� S-, C-, X- or Ku-band TT&R
Options: � GPS receiver (IOD)� Secure TT&R encryption
Providing better performance and the same reliabilit y as the existing platforms
MODULAR PLATFORM DESIGN - PLATFORM INTEGRATION
Propulsion ModulePlatform Module
� Individually adaptable to mission needs
� Parallel integration for quick delivery schedule
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Core Module
Repeater Module
MODULAR PLATFORM DESIGN - PLATFORM INTEGRATION
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Platform Module
Individually adaptable to mission needs & parallel integration for quick delivery
HISPASAT ADVANCED GENERATION 1 MISSION
Innovative Payload Technologies
� Multi-channel payload on-board processor to provide regenerative signal processing and multiplexing 3/5 Ka-band transparent transponders
� New metallization process to improve ohmic
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� New metallization process to improve ohmic losses on reflector antennas
� Direct radiating RX antenna to provide flexible beam antenna
� Optical TM/TC interface between payload units and payload control unit; flex MPM (TWTA) to provide efficient on board power output adjustment capability
The first commercial satellite contract
ESA ARTES-11 sub-element 1: Platform development co ntract for Phase B/C/D
� Start: January 2007; End: Late 2012
� SRR successful in July 2007
� PDR is under going and has been completed by June 2008
ARTES-11 sub-element 2: First mission contract
� Commercial operator: HISPASAT
� Launch 2012
� LUXOR Commercial Product Line is in the way
STATUS OF THE PRODUCT DEVELOPMENT
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� LUXOR Commercial Product Line is in the way
2008 2009 2010 2011 2012 2013
Platform Phase BPlatform Phase B
Platform Phase C/DPlatform Phase C/D
QAR 1 QAR 2
Mission Phase AMission Phase AHISPASAT Mission Phase B/C/DHISPASAT Mission Phase B/C/D
Launch
ESA and OHB with its partners are ready to offer th e European LUXOR to the market
WORLDWIDE COMMERCIAL MARKET FEEDBACK
Product Introduction to the global commercial marke t in “Satellite 2008”
� Welcomed by the commercial customers
� Eight opportunities identified during the conference
� SES America bought five small satellites; Intelsat bought two and plans to buy
several in the next decade
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� The expansion of HDTV, Video to mobile terminals and broadband/IP businesses
would eat up the in orbit assets quickly and demand more satellites
� February to October 2008 five small satellite contracts awarded
� The size of the market is larger than six satellites per year
predicated by the business plan
� Two satellite primes in Europe: Thales and EADS� Third Rising Prime: OHB with First Prime Contract – SGEO
Follow-on in institutional market
THIRD RISING PRIME IN EUROPE
Satellite Number
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Satellite Number
ESA Data Relay Satellite 1 (ESA)
German Heinrich Hertz Communications Satellite 1 (DLR)
Meteosat Third Generation 2 (plus 4 Meteosat)
German Lunar Exploration Orbiter 1 (DLR)
� Provide Data Relay Services to ESA GMES EO satellites� OHB-System is currently doing Phase-A study� Phase B starting in Q4 2009 and will be launched in 2013� EDRS will fly an advanced laser communications terminal� Funding approved at ESA Conference on ministerial level in Nov 2008
ESA DATA RELAY SATELLITE
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MeteoSat Third Generation: Key Features
� At present, largest budget Earth Observation Programme: EUR 850 million ESA (2 geostationary satellites) total EUR 2,205 million (+ Eumetsat 4 geostationary satellites)
� Industrial Invitation to competitive tender in June 2009
� First Launch: End of 2015
METEOSAT THIRD GENERATION
Back-up
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� OHB prepares for Bid of the 6 satellite platforms, based on the Small GEO design
NominalMTG-I
FCI, LI, DCP, S&RNominal MTG-S
IRS, UVS
Back-upMTG-I
FCI, LI, DCP, S&R0°
Thales Concept
LUNAR EXPLORATION ORBITER (LEO)
� DLR Program for a moon orbiter mission, funding currently open
� Orbiter in polar orbit around the moon, incl. 12 instruments, e.g.:
� High resolution camera for three-dimensional mapping
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mapping
� Water search with best appropriate methods
� High-precision surveying of the moon‘s magnet and gravity fields
� Mission duration 4 years
� Jointly realisation by EADS Astrium (Prime)and OHB-System (Co-Prime)
Moon is the step stone to Mars
EUROPEAN GPS - GALILEO-SYSTEM
� OHB is encouraged by ESA / EC to be the alternative supplier of space segment
� OHB is bidding as prime
� SSTL is the subcontractor
� OHB / SSTL have been down selected for competitive dialogue after evaluation of Preliminary proposal
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proposal
� Project Schedule
� Responding to RFI in August 2008
� Contract expected in 2009
� Based on
� SGEO/LUXOR platform (components)
� SAR-Lupe platform (experience; bus-components)
A cost-effective solution for European Galileo Prog ram
SUMMARY
� There is a need for an European small geostationary satellite
� OHB leads a consortium developing a 3,000 kg (GTO) and 1,600 kg (GEO) satellite
with 400 kg and 4 kW payload capacity under ESA ARTES-11 program
� First mission for a commercial operator has been contracted and will be launched
at the end of 2012
� SGEO opens up substantial businesses for OHB in both global commercial and
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� SGEO opens up substantial businesses for OHB in both global commercial and
institutional market
OHB-System - the Third Rising Prime in Europe
THANK YOU!
OHB-System AG | Bremen, February 11, 2009