The Status of Space R&D and Commercialization …BSX2010 & World Space-Biz 2010 The Status of Space...

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BSX2010 & World Space-Biz 2010 The Status of Space R&D and Commercialization Activities in Korea 2010. 8. 26 Gwanghyeok JU Satellite R&D Head Office Korea Aerospace Research Institute 1

Transcript of The Status of Space R&D and Commercialization …BSX2010 & World Space-Biz 2010 The Status of Space...

Page 1: The Status of Space R&D and Commercialization …BSX2010 & World Space-Biz 2010 The Status of Space R&D and Commercialization Activities in Korea 2010. 8. 26 Gwanghyeok JU Satellite

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

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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

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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

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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

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National Space Development Plan

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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

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y

7 2012-2017 Sun-Synch. Orbit N/A EO Earth Observation

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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

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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

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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

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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

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KOMPSAT-3 Image

Ocean MonitoringOcean Monitoring GIS(Geographic Information Systems)GIS(Geographic Information Systems)

KOMPSAT-3 Results (Prediction)

CartographyCartography National Security ApplicationNational Security Application

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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

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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

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■ Launch Vehicle : Dnepr■ Launch Vehicle : Dnepr

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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

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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

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■ Launch Vehicle : Ariane 5■ Launch Vehicle : Ariane 5

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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

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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

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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%

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Applications 760,431(85.7%) (72.1) 18.0%

SUM 887,255(100.0%) 864,335(100.0) ▵2.6%

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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,,

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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)

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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

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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

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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.

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Thank You

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