the status of space r&d and commercialization …bsx2010 & world space-biz 2010 the status...
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BSX2010 & World Space-Biz 2010
The Status of Space R&D and Commercialization Activities in Korea
2010. 8. 26
Gwanghyeok JUSatellite R&D Head Office
Korea Aerospace Research Institute
11
Contents
Ⅰ I t d ti t KARIⅠ. Introduction to KARI
Ⅱ. Korean Space Research & Development Status
Ⅲ. Commercialization Activities
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Korea Aerospace Research Institute
■ Korea Aerospace Research Institute (KARI) has been a leading national aerospace R&D institute since its establishment in 1989
■ Mission and major functions
■ Korea Aerospace Research Institute (KARI) has been a leading national aerospace R&D institute since its establishment in 1989
■ Mission and major functions■ Mission and major functions- Perform basic and applied studies in aerospace technology- R&D Fields
• Satellite launch vehicles and aircraft development
■ Mission and major functions- Perform basic and applied studies in aerospace technology- R&D Fields
• Satellite launch vehicles and aircraft development Satellite, launch vehicles, and aircraft development• Space science and space applications research• Aerospace safety and certification
- Total personnel : ~700, Annual budget : ~360 million US dollars
Satellite, launch vehicles, and aircraft development• Space science and space applications research• Aerospace safety and certification
- Total personnel : ~700, Annual budget : ~360 million US dollars
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Mission & Function of KARI
Objective of Establishment
Contribute to the Sound Development of the National Economy and Improvement of Public Life by Venturing into the Realm of Aerospace Science & Technology and Leading and Spreading Technology
Mission & Function
•Research & Development and Utilization of the Integrated System and Core Technologies for Aircraft, Satellite and Space Launch VehicleD l T h l t E A S f t d Q lit•Develop Technology to Ensure Aerospace Safety and Quality
•Help Develop Policy for National Aerospace Development•Collaborate with Industry and Academy in the Use of Testing and Evaluation Facilities
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KARI Organization
PresidentPresident AuditorAuditorAuditing DivisionProject Strategy Division Public Relations
& Media Cooperation Division
Vice PresidentVice President
DD
Program Evaluation &Coordination Division
DD DD
Satellite InforSatellite InforA
eronautics Res
Aeronautics R
esD
evelopment H
eaD
evelopment H
ea
Aviation Safety R
Aviation Safety R
Smart U
AV D
eveSm
art UA
V Deve
Space App
Space App
Satellite Resea
Satellite Resea
Developm
ent Hea
Developm
ent Hea
KSLV R
esearK
SLV Resear
Developm
ent Hea
Developm
ent Hea
Aerospace
Aerospace
Policy, PlaPolicy, Pla
Adm
inistraA
dministra
rmation R
esearchrm
ation Researchsearch &
search &ad O
fficead O
fficeA
eA
e
R&
D C
enterR
&D
Center
elopment C
enterelopm
ent Center
plication & Futur
plication & Futur
arch &arch &ad O
fficead O
ffice
rch &rch &ad O
fficead O
ffice
Ro
Ro
Ae
Ae
CO
MC
OM
KO
MK
OM
KO
MK
OM
SatSat
SatSat
KSL
KSL
NA
RN
AR
KSL
KSL
SpaSpa
e Safety & C
ertifie Safety &
Certifi
anning & Internat
anning & Internat
ation Division
ation Division
MM
h Instituteh Institute
SateSateA
ppA
pp
KO
MK
OMronautics Technoronautics Techno
re Technology Di
re Technology Di
tocraft Program
tocraft Program
ronautical Systeronautical Syste
MS Program
Offi
MS Program
Offi
MPSA
TM
PSAT--
55ProgrProgr
MPSA
TM
PSAT--
33ProgrProgr
ellite Technologyellite Technology
ellite Test Divisio
ellite Test Divisio
LV Systems O
fficLV System
s Offic
RO
Space Center
RO
Space Center
LV Technology DLV Technology D
ace Propulsion Dace Propulsion D
cation Center
cation Center
tional Relations D
tional Relations D
Managem
ent Div
Managem
ent Div
ellite Operations
ellite Operations
plication Division
plication Division
MPSA
TM
PSAT--
33A divis
A divis
55
ology Division
ology Division
visionvision
Office
Office
ms D
ivisionm
s Division
iceice
ram O
fficeram
Office
ram O
fficeram
Office
y Division
y Division
onon cece rr Division
Division
Division
Division
Division
Division
visionvision
&&nnsionsion
Satellite Integration & Test Center (SITC)
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Large TV Chamber
• Working Volume : Φ 8 m × L 10 m• Temp. Range :
Min : ≤ 190Min. : ≤ -190Max. : ≥ 150
• Vacuum Level : ≤ 10-6 torr
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Large T/V Chamber for Optical Payload
• Working Volume : H 3.6 m x W 4m x L 10 m• Temp. Range : -150 ~ -120• Vacuum Level : 10-6 torrVacuum Level : 10 6 torr
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Satellites Operation Facilities at KARI
9M AntennaLEO Operation
Mission Operation Room7.3M Antenna
RF Equipment RoomLEO Operation LEO Operation
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13M Antenna GEO Operation
13M AntennaLEO Operation
Satellites Operation Facilities in South Pole(Sejong Antenna Site)( j g )
• The south latitude 62 deg, the west longitude 58 deglongitude 58 deg
• Provide Maximum 10 communication chance in a day
– Initial Operation after launchInitial Operation after launch– Urgent command
• Real-time remote control in Daejeon
1010
National Space Development Plan
1111
Korea Multi-Purpose Satellite (KOMPSAT) Program
No.Development
Period
Spec.Payload Mission
Orbit Weight (Kg)Orbit Weight (Kg)
1 1994 ~ 1999 Sun-Synch. Orbit 500EOC (PAN : 6.6m)OSMI, SPS
Earth ObservationScience Physics
MSC2 1999 ~ 2006 Sun-Synch. Orbit 765
MSC(PAN:1.0m,MS:4.0m)
Earth Observation
AEISSE3 2004-2011 Sun-Synch. Orbit <1,000 (PAN:0.7m,
MS:2.8m) Earth Observation
5 2005-2010 Sun-Synch. Orbit <1,400 SAR (1m/5Km, 3m/30Km) Earth Observation)
3A 2006-2013 Sun-Synch. Orbit <1,000(PAN:0.7mIR:7m)
Earth Observation
6 2010-2015 Sun-Synch. Orbit N/A SAR Earth Observation
1212
y
7 2012-2017 Sun-Synch. Orbit N/A EO Earth Observation
KOMPSAT-1
■ Development Outline• Period : Nov ’94 ~ Jan ’00
■ Development Outline• Period : Nov ’94 ~ Jan ’00• Period : Nov. 94 ~ Jan. 00• Joint Development by KARI & TRW• Launch : Dec. 22, ‘99
■ Pa load
• Period : Nov. 94 ~ Jan. 00• Joint Development by KARI & TRW• Launch : Dec. 22, ‘99
■ Pa load■ Payload• Electro-Optical Camera (EOC)• Resolution : 6.6m (PAN)
■ Payload• Electro-Optical Camera (EOC)• Resolution : 6.6m (PAN)
■ Lifetime : 3 years
■ Altitude : 685Km
■ Lifetime : 3 years
■ Altitude : 685Km
■ Weight : 470kg, Power : 636W
■ Launch Vehicle : TAURUS
■ Weight : 470kg, Power : 636W
■ Launch Vehicle : TAURUS
1313
KOMPSAT-2
■ Development Outline• Period : Dec ’99 ~ July ’06
■ Development Outline• Period : Dec ’99 ~ July ’06• Period : Dec. 99 ~ July. 06• Launch : July. 28, ‘06
■ PayloadM lti S t l C (MSC)
• Period : Dec. 99 ~ July. 06• Launch : July. 28, ‘06
■ PayloadM lti S t l C (MSC)• Multi-Spectral Camera (MSC)
• Resolution : 1m (PAN) / 4m (MS)
■ Lifetime : 3 years
• Multi-Spectral Camera (MSC)• Resolution : 1m (PAN) / 4m (MS)
■ Lifetime : 3 years
■ Altitude : 685Km
■ Weight : 800kg, Power : 1KW
■ Altitude : 685Km
■ Weight : 800kg, Power : 1KW
■ Launch Vehicle : ROCKOT■ Launch Vehicle : ROCKOT
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KOMPSAT-2 Image
KOMPSAT-2 Results : Olympic Main Stadium, Seoul
1515
KOMPSAT-2 Image
KOMPSAT-2 Results : 5.1 Stadium, Pyongyang
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KOMPSAT Program Evolution
KOMPSAT 3KOMPSAT - 3- ’04 ~ ’11- Critical Design Completed - To be launched at ’11
KOMPSAT - 2- Launced at ’06.7- Operational
KOMPSAT - 5
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KOMPSAT 5- ’04 ~ ’10- Critical Design Completed- SAR Payload (Radar Image)- To be launched at ‘10
KOMPSAT-3
■ Development Outline• Period : Aug ’04 ~ Dec ’11
■ Development Outline• Period : Aug ’04 ~ Dec ’11• Period : Aug. 04 ~ Dec. 11• Launch : 2011
■ PayloadAd d E th I i S t (AEISS)
• Period : Aug. 04 ~ Dec. 11• Launch : 2011
■ PayloadAd d E th I i S t (AEISS)• Advanced Earth Imaging System (AEISS)
• Resolution : 0.7m (PAN) / 2.8m (MS)
■ Lifetime : 4 years
• Advanced Earth Imaging System (AEISS)• Resolution : 0.7m (PAN) / 2.8m (MS)
■ Lifetime : 4 years
■ Altitude : 685Km
■ Weight : 1,000kg, Power : 1.3KW
■ Altitude : 685Km
■ Weight : 1,000kg, Power : 1.3KW
■ Launch Vehicle : H-2A■ Launch Vehicle : H-2A
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KOMPSAT-3 Image
Urban PlanningUrban Planning Agriculture & ForestryAgriculture & Forestry
KOMPSAT-3 Results (Prediction)
National Resource ObservationNational Resource ObservationDisaster MonitoringDisaster Monitoring
19196
KOMPSAT-3 Image
Ocean MonitoringOcean Monitoring GIS(Geographic Information Systems)GIS(Geographic Information Systems)
KOMPSAT-3 Results (Prediction)
CartographyCartography National Security ApplicationNational Security Application
20207
KOMPSAT-3A
■ Development Outline• Period : Dec ‘06 ~ Dec 2013
■ Development Outline• Period : Dec ‘06 ~ Dec 2013• Period : Dec. 06 ~ Dec. 2013• Launch : 2013
■ PayloadEO/IR C
• Period : Dec. 06 ~ Dec. 2013• Launch : 2013
■ PayloadEO/IR C• EO/IR Camera
• Resolution : 0.55m (PAN) / 2.2m (MS) / 5.5m (IR)
• EO/IR Camera• Resolution : 0.55m (PAN) / 2.2m (MS) /
5.5m (IR)
■ Lifetime : 4 years
■ Altitude : 530Km
■ Lifetime : 4 years
■ Altitude : 530Km
■ Weight : 1,000kg, Power : 1.4KW
■ Launch Vehicle : TBD
■ Weight : 1,000kg, Power : 1.4KW
■ Launch Vehicle : TBD
2121
KOMPSAT-5
■ Development Outline• Period : June ‘05 ~ Jun 2011
■ Development Outline• Period : June ‘05 ~ Jun 2011• Period : June 05 ~ Jun. 2011• Launch : 2010
■ PayloadS th ti A t R d (SAR)
• Period : June 05 ~ Jun. 2011• Launch : 2010
■ PayloadS th ti A t R d (SAR)• Synthetic Aperture Radar (SAR)
• Resolution- High Resolution : 1m/5km- Standard Resolution : 3m/30km
• Synthetic Aperture Radar (SAR)• Resolution
- High Resolution : 1m/5km- Standard Resolution : 3m/30km- Wide Swath Mode : 20m/100km
■ Lifetime : 5 years
- Wide Swath Mode : 20m/100km
■ Lifetime : 5 years
■ Altitude : 550Km
■ Weight : 1,400kg, Power : 1.4KW
■ Altitude : 550Km
■ Weight : 1,400kg, Power : 1.4KW
2222
■ Launch Vehicle : Dnepr■ Launch Vehicle : Dnepr
KOMPSAT-5 Image
GIS(Geographic Information Systems)
National Security ApplicationKOMPSAT-5 Results (Prediction)
DEMMAP
기름유출 홍수피해
Resolution = Resolution = Resolution =
GIS(Geographic Information Systems)Disaster Monitoring
1meter 1Foot 4Inches
해안선 감시해안선 감시 태풍감시태풍감시 수분함량 측정수분함량 측정 유빙분석유빙분석
Ocean Monitoring Environment Monitoring
토지피복 분석작황분석
Land Monitoring
232315
COMS(Communication, Ocean, Metrological Satellite)
■ Development Outline• Period : Sept. ‘03 ~ Dec. ‘10• Launch : June 2010
■ Development Outline• Period : Sept. ‘03 ~ Dec. ‘10• Launch : June 2010
■ Mission• Meteorological & Ocean Monitoring• Development of next generation
■ Mission• Meteorological & Ocean Monitoring• Development of next generation
communication payload technology
■ Payload• GOCI / MI / K-band Antenna
communication payload technology
■ Payload• GOCI / MI / K-band AntennaGOCI / MI / K band Antenna• Resolution : 1km(기상), 0.5km(해양)
■ Lifetime : 7 years
GOCI / MI / K band Antenna• Resolution : 1km(기상), 0.5km(해양)
■ Lifetime : 7 years
■ Altitude : 36,000Km
■ Weight : 2,500kg, Power : 2.7KW
■ Altitude : 36,000Km
■ Weight : 2,500kg, Power : 2.7KW
2424
■ Launch Vehicle : Ariane 5■ Launch Vehicle : Ariane 5
Advanced KOMPSAT Series for Earth Observation
■ KOMPSAT-7 • Launch : 2017
Resolution (EO) : 0 5m (TBD)
■ KOMPSAT-7 • Launch : 2017
Resolution (EO) : 0 5m (TBD)• Resolution (EO) : 0.5m (TBD)
■ KOMPSAT-9 • Launch : 2022
R l ti (EO) 0 3 (TBD)
• Resolution (EO) : 0.5m (TBD)
■ KOMPSAT-9 • Launch : 2022
R l ti (EO) 0 3 (TBD)• Resolution (EO) : 0.3m (TBD)• Resolution (EO) : 0.3m (TBD)
■ KOMPSAT-6 • Launch : 2015 • Resolution (SAR) : TBD
■ KOMPSAT-6 • Launch : 2015 • Resolution (SAR) : TBD
■ KOMPSAT-8 • Launch : 2020 • Resolution (SAR) : TBD
■ KOMPSAT-8 • Launch : 2020 • Resolution (SAR) : TBD
2525
New GEO Satellite for Weather, Ocean and EnvironmentMonitoring (Planned)
■ Development Outline• Period : 2011 ~ 2018• Launch : 2017 / 2018
■ Development Outline• Period : 2011 ~ 2018• Launch : 2017 / 2018
■ Mission• Weather Monitoring• Ocean & Environment Monitoring
■ Mission• Weather Monitoring• Ocean & Environment Monitoring
■ Payload• Meteorological Payload• Ocean & Environment Payload
■ Payload• Meteorological Payload• Ocean & Environment PayloadOcean & Environment Payload• Resolution : 1km(MI) / 0.5km(Ocean) /
5km(Environment)
■ Lifetime : 10 years (TBD)
Ocean & Environment Payload• Resolution : 1km(MI) / 0.5km(Ocean) /
5km(Environment)
■ Lifetime : 10 years (TBD)■ Lifetime : 10 years (TBD)
■ Altitude : 36,000Km
■ Lifetime : 10 years (TBD)
■ Altitude : 36,000Km
2626
Space Market in Korea
7 ,000
8 ,873 8 ,644
8000
10000
5 ,589
4000
6000
0
2000
2005년 2006년 2007년 2008년2005년 2006년 2007년 2008년
FY2007(Mwon) FY2008(Mwon)
Space H/W & S/W
126,824(14.3%) 240,914(27.9) 90.0%
Space 760 431(85 7%) 623,441 ▵18 0%
2727
Applications 760,431(85.7%) (72.1) 18.0%
SUM 887,255(100.0%) 864,335(100.0) ▵2.6%
Commercialization Status
■ The Images of KOMPSAT-2 has been successfully entered into world ■ The Images of KOMPSAT-2 has been successfully entered into world market by two excellent distributing agents.
• SPOT IMAGE Ltd.• KAI Image Ltd.
market by two excellent distributing agents.• SPOT IMAGE Ltd.• KAI Image Ltd.
■ Several aerospace companies have participated in KOMPSAT, COMS & LV development.■ Several aerospace companies have participated in KOMPSAT, COMS & LV development.
■ Satrec-I has already joined small satellite systems for earth observation.• RazakSat• DubaiSat 1, 2
■ Satrec-I has already joined small satellite systems for earth observation.• RazakSat• DubaiSat 1, 2,,
2828
Industry Participation for KOMPSAT Program
Koreanization Items
Battery RadiatorMLI
Propulsion Assy Dual ThrusterRDU VDE
Doowon (Thermal)Hanwha (Propulsion)
FSSA CSSADoosan (Control)
Payload Module Equipment ModulePCU ECU
S-bandTransponder
OBC
AdapterPropulsion ModuleDDC SAR KAI (Telemetry)KAI (Power)
2929
Korean Air (Structure)( )
MLI : Multi-Layer Insulator PCU : Power Control Unit ECU : EPS Control UnitDDC : Deployment Device Controller SAR : Solar Array Regulator VDE : Valve Drive ElectronicsRDU : Remote Drive Unit FSSA : Fine Sun Sensor Ass’y KAI : Korea Aerospace Industries
KARI’s Commercialization Policy
■ KOMPSAT-3/3A are representative models of commercialization.• The Images of KOMPSAT-3 will be provided to world market in 2012
ft l h i 2011
■ KOMPSAT-3/3A are representative models of commercialization.• The Images of KOMPSAT-3 will be provided to world market in 2012
ft l h i 2011after launch in 2011.• Commercially top class optical images with 0.7m PAN and 2.8m MS• Two images can be merged to create 0.7 m pan-sharpened color
imagery
after launch in 2011.• Commercially top class optical images with 0.7m PAN and 2.8m MS• Two images can be merged to create 0.7 m pan-sharpened color
imageryimagery.• If there is customer’s need for IR channel, an alternative choice is
KOMPSAT-3A■ KARI proposes either Co-Development or Sale of KOMPSAT-3 or 3A on
imagery.• If there is customer’s need for IR channel, an alternative choice is
KOMPSAT-3A■ KARI proposes either Co-Development or Sale of KOMPSAT-3 or 3A onKARI proposes either Co Development or Sale of KOMPSAT 3 or 3A on the basis of recurrent model.■ The comprehensive services are available including construction of AIT facility, implementation and test equipments such as T/V chamber,
KARI proposes either Co Development or Sale of KOMPSAT 3 or 3A on the basis of recurrent model.■ The comprehensive services are available including construction of AIT facility, implementation and test equipments such as T/V chamber, y, p q p ,acoustic chamber, etc, training, engineering service for construction.
■ Total services are available including construction of entire ground t i l t ti f i i t t i i d
y, p q p ,acoustic chamber, etc, training, engineering service for construction.
■ Total services are available including construction of entire ground t i l t ti f i i t t i i d
3030
system, implementation of image processing system, training, and consultation of construction , and operation.system, implementation of image processing system, training, and consultation of construction , and operation.
Thank You
3131