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Robust Imaging from Space Adjunct Reference Document #1 Satellite and Airborne SAR Sensor Specifications The following tables provide detailed specifications of currently operational and proposed satellite and airborne SAR sensors, including those having reached end of life. Table A - Operational satellite SAR sensors and specifications _________________________ 1 Table B - Future/proposed satellite SAR sensors and specifications._____________________ 7 Table C - Operational airborne SAR sensors and specifications. _______________________ 13 Table D - Decommissioned SAR sensors. __________________________________________ 18

Satellite and Airborne SAR Sensor Specifications

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Page 1: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space

Adjunct Reference Document #1

Satellite and Airborne SAR Sensor Specifications

The following tables provide detailed specifications of currently operational and proposed satellite and airborne SAR sensors, including those having reached end of life.

Table A - Operational satellite SAR sensors and specifications _________________________ 1

Table B - Future/proposed satellite SAR sensors and specifications. _____________________ 7

Table C - Operational airborne SAR sensors and specifications. _______________________ 13

Table D - Decommissioned SAR sensors. __________________________________________ 18

Page 2: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table A - Operational satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 1

Table A - Operational satellite SAR sensors and specifications

X-BAND

Nat

ion

Sensor, operating agency, launch, Design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

GER

MA

NY

SAR-Lupe 1-5 DLR/Bundeswehr 5 satellite constellation for delivering high resolution

SAR images for military reconnaissance 1

st 2006, 2

nd 2007, 3

rd 2007, 4

th 2008, 5

th 2008

Est. Cost 250 mil EUR EOL: 10 yrs

Polar 500 km 98.2° Daily

8 5.5

X-band SAR Encrypted S-band for telemetry & command transmissions Stripmap mode Spotlight mode

<1

TSX-1 (TerraSAR-X) DLR, 2007-2013

Scientific & commercial use hydrology, geology, climatology, oceanography, environment & disaster monitoring, cartography

Sun-synch 514 km 97.44° 11 days

10 10 15-30 100

X- Multiple imaging modes High resolution Spotlight SP (HH or VV) or DP (HH/VV) Spotlight SP (HH or VV) or DP (HH/VV) Stripmap SP (HH or VV) or DP (HH/VV, HH/HV, VV/VH) ScanSAR SP

1.48-3.49 1.48-3.49 1.7-3.49 1.7-3.49

20-55 20-55 20-45 20-45 Left and right looking

TDX-1 (TanDEM-X) DLR, 2010-2014 Global DEM generation & earth observation, new

applications using along-track InSAR (e.g., measuring ocean currents), pol-InSAR, bistatic processing and formation flying

EOL: 5 yrs Co-fly in close formation with TSX-1, near identical capability

Sun-synch 514 km 97.44° 11 days

30 10 100

Interferometric imaging: Bistatic mode Monostatic mode Along-track interferometry (ATI) Polarimetric interferometry SAR imaging (same as TerraSAR-X): Stripmap DP Spotlight DP ScanSAR DP

12 (DEM) (abs v.acc 10 m, rel acc. <2 m) 3 1 16

25-55

Page 3: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table A - Operational satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 2

X-BAND

Nat

ion

Sensor, operating agency, launch, Design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

ITA

LY

Cosmo-SkyMed 1-4 (Constellation of small Satellites for Mediterranean basin Observation) ITA, -1 2007, -2 2007, -3 2008, -4 2009 EOL: 5 years 4 X-band EOS satellite constellation Dual use: Civilian: disaster/risk management, ice monitoring,

agriculture, urban Defence: intelligence gathering, ship detection,

maritime surveillance, security

Sun-synch 620 km 97.86° Daily-16 days

10 30-40 100-200 30

Selectable single pol (HH,VV,HV,VH) Spotlight Stripmap ScanSAR Ping pong or Stripmap – 2x selectable pol (HH, VV, HV, VH)

1 3-15 30-100 15

25-50 Left and right looking

RU

SSIA

Meteor-M N1 (Meteorological Satellite) ROSHYDROMET, ROSKOSMOS. 2009-2014 EOL: 5 yrs

Operational meteorological services, regional & global weather analysis & prediction, ocean surface water states, space weather analysis

Sun-synch 830 km 98.79° 37 days

450-600 Onboard Radar Complex (OBRC) – Severjanin, Vertical pol Low resolution MSS (MSU-MR) IR Fourier Spectrometer (IRFS-2) MS imaging system (KMSS) Microwave imaging/sounding radiometer (MTVZA) Spectrometer for Geoactive Measurements (MSGI) Data Collection System (DCS)

400-1000 25-48

JAP

AN

IGS-7A (Information Gathering Satellite) 2011- Dual use Military: surveillance, early warning of hostile

launches Civilian: disaster monitoring

Polar 500 km

1

Page 4: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table A - Operational satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 3

X-BAND

Nat

ion

Sensor, operating agency, launch, Design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

IND

IA

RISAT-2 (Radar Imaging Satellite 2) ISRO, 2009-2013 Dual use Civil: agriculture, forestry, soil moisture, geology,

sea ice, coastal processes, object detection, flood mapping

Military: reconnaissance, border surveillance, ship detection

Sun-synch 550 km

10-50 Spotlight Stripmap Mosaic mode

3-8

ISR

AEL

TecSAR (Technological SAR) IAI, 2008- EOL: 4 yrs

Low-earth orbit reconnaissance

450-580 km 41°

Selectable pol (HH,HV,VH,VV) Stripmap Spotlight ScanSAR Mosaic mode

1

Page 5: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table A - Operational satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 4

C-BAND

Nat

ion

Sensor, operating agency, launch, Design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

IND

IA

RISAT-1 (Radar Imaging Satellite) ISRO, 2012-2017 EOL: 5 yrs Dual use Civil: agriculture, forestry, soil moisture, geology,

sea ice, coastal processes, object detection, flood mapping

Military: reconnaissance, border surveillance, ship detection

Sun-synch circ 609 km 97.84° 12 days

10 30 30 120 240

Spotlight SP/DP Stripmap mode-1 (FRS-1) SP/DP Stripmap mode-2 (FRS-2) QP Med res ScanSAR (MRS) SP/DP Coarse res ScanSAR (CRS) SP/DP

<2 3 12 25 50

±34 Left or right looking

CA

NA

DA

RADARSAT-1 CSA, 1995-

Earth observation: disaster management, interferometry, agriculture, cartography, hydrology, forestry, oceanography, ice studies, coastal monitoring

Sun-synch 798 km 98.6° 24 days

45 100 150 300 500 75 170

C- Multiple imaging modes Fine HH Standard HH Wide HH ScanSAR narrow ScanSAR wide Extended high Extended low

8 30 30 50 100 18-28 30

37-47 20-49 20-45 20-49 29-49 52-58 10-22 Right looking

RADARSAT-2 CSA, 2007-

Earth observation: maritime surveillance, disaster management, ecosystem monitoring

Sun-synch 798 km 98.6° 24 days

20 50 50 100 150 300 500 75 25 25

Multiple imaging modes Ultra-Fine SP Multi-look Fine SP Fine SP/DP Standard SP/DP Wide SP/DP ScanSAR Narrow SP/DP ScanSAR Wide SP/DP Extended High SP Fine QP Standard QP

3 8 8 25 30 50 100 18 12 25

30-49 30-50 30-50 20-49 20-45 20-46 20-49 49-60 20-41 20-41

Page 6: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table A - Operational satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 5

S-BAND

Nat

ion

Sensor, operating agency, launch, Design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

RU

SSIA

Kondor-E NPO, 2012-2022 EOL: 3-10 yrs Dual use Military: navigation and reconnaissance Earth observation: agriculture, forestry, land use

management, geology and mineral exploration, environmental protection

Polar 800 km

20-150 10-20

Spotlight HH, VV Stripmap ScanSAR

1-2 1-3 5-30

20-55 Left and Right looking

CH

INA

HJ-1C (Huan Jing-1) CRESDA, 2011-2014 Environmental monitoring & prediction, solid waste

monitoring, disaster monitoring & prediction (flood, drought, typhoon, wind damage, sand storm, earthquake, land creep, frost, grassland fires, crop pests, ocean disaster monitoring)

Sun-synch circ 500 km 97.3° 31 days

40 100

1 radar + 2 optical constellation (HJ-1A: CCD+IR camera, HJ-1B: CCD+HSI camera) StripMap SP (HH or VV) ScanSAR

5 20

31-44.5

Page 7: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table A - Operational satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 6

L-BAND

Nat

ion

Sensor, operating agency, launch, Design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

CH

INA

JianBing-5 (JB-5) JB 5-2/Yaogan3, JB 9-1/Yaogan6, JB 9-2/Yaogan8, Yaogan9A/9B/9C, JB 9-3/Yaogan10, Yaogan13 Y3 2007-, Y6 2009-, Y8 2009-, Y9 2010-, Y10 2010-, Y13 2011 Dual use Military: intelligence gathering, surveillance and

reconnaissance Earth observation: land survey, disaster forecasting,

crop yield evaluation, urban planning

635 km (Y3) 518 km (Y6) 1200 km (Y8) 1089 km (Y9) 629 km (Y10) 97.8 °

20 100

Spotlight ScanSAR

5 40 1.5 (Y6)

63.4 (Y9)

MULTI-FREQUENCY

Nat

ion

Sensor, operating agency, launch, Design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

RU

SSIA

Smotr Gascom, 2009 EOL: 7-10 yrs 4 low-orbit satellites for monitoring oil/gas pipeline

and earth observation (2 radar, 2 optical)

Sun-synch 670 km 98°

10-15 30-100

X- or C-band High resolution mode Low resolution mode

1-3 5-15

Priroda RKA, 1996- Launched & installed on MIR space station Geoecology, land surface & ocean exploration

400 km 52° 6 days

50 Radiometer, SAR and optical imaging L-HH and S-VV

50 35

Page 8: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table B - Future/proposed satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 7

Table B - Future/proposed satellite SAR sensors and specifications

X-BAND

Nat

ion

Sensor, operating agency, launch, design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

SPA

IN

SEOSAR/PAZ (SAR Observation Spanish Satellite) 2012-2016 Dual use Defence: land/water surveillance, border control,

tactical support Civil: natural disaster monitoring, risk & crisis

management

Sun-synch 514 km 97.44° 11 days

5-10 15-30 100

Based on TerraSAR-X Spotlight SP/DP Stripmap SP/DP ScanSAR (HH, VV)

1-2 3-6 15

15-60 Left and right looking

ITA

LY

Cosmo-SkyMed Second Generation (CSG-1, CSG-2) ASI, MiD CSG-1 2015-2023, CSG-2 2016-2023 Environmental monitoring, surveillance and risk

management, maritime, topographic mapping, law enforcement

Sun-synch 620 km 97.8° 16 days

10 40 100, 200 30

Spotlight DP Stripmap DP ScanSAR DP Ping-pong QP

1 3 20, 40 15

GER

MA

NY

TerraSAR-X2 DLR, 2015-2018 Commercial follow-on mission to TSX-1:

cartography, land surface, civil planning, DTMs, environmental monitoring

Sun-synch

10-40 50-500

Spotlight Stripmap ScanSAR

0.5 1-4 5-50

UK

AstroSAR Astrium EOL: 5 yrs Mini-satellite proposed to UK Ministry of Defence Cost: <$100 mil. Dual use: civil/military Maritime, environment, security &

disaster monitoring

Sun-synch 500 km Hourly-daily

10 20 100 900

Spotlight SP (HH or VV) or DP (HV) Stripmap SP/DP ScanSAR SP/DP Maritime

1 3 30 20

±45 Left and right looking

Page 9: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table B - Future/proposed satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 8

X-BAND

Nat

ion

Sensor, operating agency, launch, design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

RU

SSIA

Meteor-M N2, N3 (Meteorological Satellite) ROSHYDROMET, ROSKOSMOS, N2 2012, N3 2015 EOL: 5 yrs Operational meteorological services, regional &

global weather analysis & prediction, ocean surface water states, space weather analysis

Sun-synch 835 km 98.7° 37 days

450-600 Onboard Radar Complex (OBRC) – Severjanin, Vertical pol Module for Geophysical Measurements (GGAK-M) Fourier spectrometer (IKFS-2) MS imager (KMSS) MS scanning imager/radiometer (MSU-MR) Scanning microwave imager-sounder (MTVZA) Data Collection System (DCS)

400-1000 25-48

KO

REA

KOMPSAT-5 (Korea Multi-Purpose Satellite-5) KARI, 2012-2017 EOL; 5 yrs Civil/scientific use; GIS, ocean & land management,

environment and disaster monitoring

Sun-synch 550 km 97.6° 28 days

5 30 100

Selectable pol (HH,HV,VH,VV) High resolution mode Standard mode Wide swath mode

1 3 20

20-55

IND

IA RISAT-2F (Radar Imaging Satellite)

ISRO, 2013-? Research and disaster management applications

Sun-synch 550 km

Page 10: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table B - Future/proposed satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 9

C-BAND

Nat

ion

Sensor, operating agency, launch, design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

ITA

LY

Sentinel-1 A,B,C ESA A 2012-2020, B 2014-2022, C 2019-2026 Sea ice monitoring, marine surveillance, land surface

motion, disaster management

693 km 98.18° 12 days

80 250 400

VV+VH, HH+HV StripMap Interferometric Wide swath Extra wide swath Wave mode

5 5x20 20x40 5x5

20-45

CA

NA

DA

RADARSAT Constellation Mission (RCM) C-1, C-2, C-3 CSA, C1,C2 2014-2021, C3 2015-2022 3 EOS satellites for near real-time maritime

surveillance (ship detection, oil spill monitoring & sea ice mapping), disaster management, InSAR for geohazards, climate change & environment monitoring

592.7 km 97.74° 12 days

500 350 30 125 30 20 350 350

HH,VV,HV,VH, compact pol Low resolution Med resolution (maritime) Med resolution (land) Med resolution (land) High resolution Very high resolution Ice/oil low noise 25 m ship mode

100 50 16 30 5 3 100 variable

19-54 19-58 20-47 21-47 19-54 18-54 19-58 19-58 Right looking

S-BAND

Nat

ion

Sensor, operating agency, launch, design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

UK

NovaSAR-S SSTL, 2013-2020 Scientific/EO: flood and disaster monitoring,

forestry, maritime surveillance, agriculture, land cover/use

Sun-synch or LI equatorial 580 km Daily-4 days

15-20 100 150 750

SP/DP/TP: (HH, HV, VH, VV) Stripmap ScanSAR ScanSAR wide Maritime surveillance

6 20 30 30

16-34 16-30 15-31 48-73

Page 11: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table B - Future/proposed satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 10

L-BAND

Nat

ion

Sensor, operating agency, launch, design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

GER

MA

NY

TanDEM-L DLR, 2017-2022

760 km 8 days

350 L-band SAR Single-pass InSAR Polarimetry - quad Wide swath mode

20-100 26.3-46.6

JAP

AN

ALOS PALSAR-2 (Phase Array L-band SAR) JAXA, 2013-2017

Earth observation, interferometry

628 km 97.9° 14 days 66 days 42 days 14 days

25 50 50 70 350 490

Spotlight SP Ultra Fine SP/DP High sensitive SP/DP/FP/CP Fine SP/DP/FP/CP ScanSAR nominal SP/DP ScanSAR wide SP/DP (*SP: HH or VV or HV; DP: HH+HV or VV+VH; FP: HH+HV+VH+VV; CP: compact pol)

3x1 3 6 10 100 60

30-44 Left or right looking

IND

IA

RISAT-1F and -3L (Radar Imaging Satellite) ISRO, 1F 2012-2018, 3L 2014-2020 Dual use Civil: agriculture, forestry, soil moisture, geology,

sea ice, coastal processes, object detection, flood mapping

Military: reconnaissance, border surveillance, ship detection

Sun-synch 97.84° 12 days

SAR L-radiometer

USA

DESDNyl NASA JPL, 2017-2022

Earth observation: land surface change & hazards, terrestrial & climate variables

Sun-synch 600-800 km 97° 12-16 days

180-240 Multiple polarisations Single/dual-pol repeat pass InSAR Expt. quad-pol repeat pass InSAR

10-100

Page 12: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table B - Future/proposed satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 11

L-BAND

Nat

ion

Sensor, operating agency, launch, design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

SMAP (Soil Moisture Active Passive) NASA JPL, 2014-2017 Global measurements of soil moisture and

freeze/thaw state for improved understanding of water, energy & carbon cycles, climate modelling, flood prediction, drought monitoring

Sun-synch 680 km 2-3 days

1000 L-band SAR VV,HH,HV L-band Radiometer

1-3 km 40 km

40

AR

GEN

TIN

A &

ITA

LY

SAOCOM (SAR Observation and Communications Satellite) CONAE, Argentina and ASI, Italy Satellite EOS constellation 1A 2014-2019, 1B 2015-2020, 2A 2015-2020, 2B 2016-2021 EOL: 5 yrs

Soil moisture mapping to support agricultural, hydrological & health applications, General NRM & disaster management

Sun-synch 620 km 97.89° 16 days (1 sat) 8 days (const)

20-40 100-150 220-350

Stripmap SP/DP TopSAR narrow SP/DP/QP TopSAR wide SP/DP/QP/CL (*SP: HH or HV or VH or VV; DP: HH+HV or VV+VH; QP: HH+HV+VH+VV; CL: RH+RV or LH+LV)

10 30-50 50-100

17-50.4 17.6-47.3 17.6-48.9 Right looking

Page 13: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table B - Future/proposed satellite SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 12

P-BAND

Nat

ion

Sensor, operating agency, launch, design life (EOL), application area

Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Imaging modes Spatial resolution (m)

Incidence angle (°)

ITA

LY BIOMASS

ESA, Italy, 2016-2021 642 km 25-45 days

60 105

P-band InSAR full pol StripMap ScanSAR

50x65 23-32 Left or right looking

MULTI-FREQUENCY

RU

SSIA

Arkon-2M Roskosmos, 2013-2018 Military surveillance, earth observation and weather

information

Sun-synch 550-600 km

2-10 20-100 100-450

X- L- R- (69 cm)

1-1.5 3-5 30

CH

INA

HY-3A, HY-3B, HY-3C CRESDA 3A 2015-2020, 3B 2017-2022, 3C 2022-2027 EOL: >3 yrs

Ocean monitoring, environmental protection, coastal zone survey

Sun-synch 799 km 98.48° 29 days

20-40 60-80 120-150 5 150 650 650

X- SAR Precise mode HH,VV X- Stripmap HH,VV X- ScanSAR HH,VV C- SAR Wave mode HH+VV or HH+HV or VV+VH C- Image mode HH+VV or HH+HV or VV+VH C- Wide swath mode HH+VV or HH+HV or VV+VH C- Global monitoring mode HH+VV or HH+HV or VV+VH

1 5 10 10 25 100 1000

15-60

USA

SCLP (Snow and Cold Land Processes) NASA JPL, 2030-2033

Snow accumulation for freshwater availability

Sun-synch 15 days

K-band radiometer Ku and X-band radars

50-100

Page 14: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table C - Operational airborne SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 13

Table C - Operational airborne SAR sensors and specifications

Nat

ion

Sensor, operating agency and date, application area Flying height (km) Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

EUROPE

FRA

NC

E

Sethi ONERA, 2007- Earth observation, interferometry, security and

scientific applications (e.g., Tropisar campaign – preparation for BIOMASS satellite mission)

Multispectral & SAR system X- L-, P-

0-90 5-165

RAMSES ONERA

Scientific: topography, subsidence, vegetation, geology, soil moisture

P-, L-, S-, C-, X- full pol Ku, Ka full pol W

40-80

GER

MA

NY

DO-SAR Dornier

S-VV, VH, HH, HV C-VV, VH, HH, HV X-VV, VH, HH, HV Ka-VV

E-SAR DLR, 1989/94-

3.9 L- full pol X-VV or HH X-VV or HH P- full pol

2x0.085 20-60

UK

DRA-SAR (Defence Research Agency SAR) DRA

C- full pol X-HH

DEN

MA

RK

EMISAR EMI/TUD, 1993/94-

C- full pol L- full pol

2

Page 15: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table C - Operational airborne SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 14

Nat

ion

Sensor, operating agency and date, application area Flying height (km) Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

SWED

EN CARABAS (Coherent All Radio Band Sensing)

FOA

Wide-area surveillance, target detection, vegetation and biomass, disaster monitoring

1-5 1-5 VHF 20-90 MHz HH

3 40-70

NET

HER

LAN

DS PHARUS (Phased Array Universal SAR)

FEL-TNO, Delft, 1995-

Military (target detection, cartography) and civil use (forestry, agriculture, oceans)

6-20 C- full pol 3 10-75

RUSSIA

SAR TRAVERS Vega, Moscow

S- VV or HH

IMARC Vega, Moscow Soil & terrain mapping, hydrology studies, DEM

generation

24 X-, L-, P- full polarimetric VHF (118 MHz)

4-15

ASIA

JAP

AN

Pi-SAR-L (Polarimetric and Interferometric SAR) JAXA, 1996- Disaster monitoring & earth observation

6-12 15 X- InSAR Mode 1 HH or VV X- and L- full pol Mode 2 HH, HV, VH, HH

3x3.2 10-60

NASAR-1 NASDA/EORC, 1996-

20 L- full pol 3

NECSAR NASDA/EORC, 1992-

Interferometry & topographic mapping

X-HH

Page 16: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table C - Operational airborne SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 15

Nat

ion

Sensor, operating agency and date, application area Flying height (km) Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

CH

INA

CASSAR CAS/ISRA Agriculture, soil moisture, vegetation parameters,

biomass, surface roughness

7.2 X-HH, VV

10 73-83

AUSTRALIA

INGARA DSTO Scientific: coherent change detection studies &

feature extraction

12-48

X- full pol Stripmap Spotlight Interferometric

2-8 0.3

45-89

PLIS (Polarimetric L-band Imaging SAR) Flinders University, Adelaide Test bed for SMAP with applications in soil moisture

estimation

0.3-3 0.1-2.2 L-band scatterometer Full pol Single pass InSAR

11-29 15-45 Left and right looking

SOUTH AFRICA SASAR-1 (South African SAR)

University of Cape Town, 1999- Terrain mapping, vegetation studies

4 VHF (0.141 GHz) full pol

CANADA STAR-1,2 (Sea ice and Terrain Assessment Radar)

Intermap, 1990- Sea ice monitoring, terrain analysis

19-50 X-HH 5-18

NORTH AMERICA GeoSAR

Interferometer and LiDAR profiler Fugro EarthData, 2000-

Commercial/scientific: thematic & topographic mapping, hydrology, oil and gas exploration,

10-12

10-12 X- and P- HH+HV or VV+VH

1.25-3 (X-) 1.25-5 (P-) 5 (DEM)

25-60

Page 17: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table C - Operational airborne SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 16

Nat

ion

Sensor, operating agency and date, application area Flying height (km) Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

infrastructure planning, crop monitoring, forestry, fuel mapping

UAVSAR NASA JPL

Differential interferometry for investigating dynamic phenomena (earthquakes, volcanoes, deformation, vegetation, soil moisture, ice/glaciers, oceanography)

13.8 16 L- full pol 2 rng

STAR3i/IFSARE (Interferometric SAR – Elevation) ERIM, USA, 1992- Military and civil use: interferometric mapping, DEM

generation

12.2 10 X-HH 3 2.5-10 DEM (abs V.Acc 3)

45

SOUTH AMERICA

AR

GEN

TIN

A SARAT

CONAE, Argentina

Test bed for SAOCOM satellite and integration with multi-frequency SAR data for extracting physical information

9 L-band polarimetry HH,HV,VH,VV

3x0.4 23-69

BR

AZI

L

Orbisar-RFP (Radar for Foliage Penetration) OrbiSat, Brazil Cartographic products, including DTMs, ortho-

images, contour maps, topographic maps for applications in mining, gas and oil, defence, environment, energy

X- and P-band InSAR

US MILITARY

DCS (Data Collection System) ERIM, US Air Force -Single-pass interferometry

6.1 X- full pol Ku-VV

1.2 45

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table C - Operational airborne SAR sensors and specifications

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 17

Nat

ion

Sensor, operating agency and date, application area Flying height (km) Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

ASARS-2A (Advanced SAR System) Onboard U2 aircraft US Air Force Military reconnaissance & surveillance, target

detection, damage assessment, disaster survey

Payloads: electro-optical, IR and SAR imagers, film camera, signals intelligence equipment

P-3/SAR ERIM, Navy

UWB (0.35 GHz) VV, VH, HH, HV L-VV, VH, HH, HV C-VV, VH, HH, HV X-VV, VH, HH, HV

SAR onboard RC-7 ARL aircraft US Military

Military intelligence gathering

Payloads: communications, signals and imagery intelligence

1.8

Phased-array radar onboard E-8C JSTARS aircraft US Air Force

Ground surveillance & moving target detection

Multi-mode SAR system Wide Area Surveillance (WAS) Moving Target Indicator (MTI)

Antenna tilted to either side 120° FOV

SAR onboard MQ-1 Predator UAV US Air Force, 1995- Military surveillance and reconnaissance,

intelligence gathering, weapons delivery

7.62 0.3-1

SAR onboard RQ-4A Global Hawk UAV US Air Force

Military intelligence, moving target detection, damage assessment

19.8 10 37

UAV equipped with electro-optical, IR and SAR imagers SAR MTI system, X-band Spotlight mode Stripmap mode Wide-area mode

0.3-1.8 6

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Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table D - Decommissioned SAR sensors

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 18

Table D - Decommissioned SAR sensors

AIRBORNE

Nat

ion

Sensor, operating agency and date, application area Flying height (km)

Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

USA

AIRSAR (Airborne SAR) and TOPSAR (Topographic SAR) NASA JPL, USA 1993-2000

8 10-15 4.6 TOPSAR

C-, L- and P- Polarimetric Cross-track Interferometric (XTI) Along-track Interferometric (ATI)

10 0-70

SATELLITE

Nat

ion

Sensor, operating agency, launch, application area Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

X-BAND

JAP

AN

IGS-1B, IGS-4B (Information Gathering Satellites) 1B 2003-2007, 4B 2007-2010

Military surveillance

486-491 km 97.3°

1-3

C-BAND

ITA

LY ERS-1 (Earth Resources Satellite)

ESA, 1991-2000

Earth observation, meteorology, topographic mapping

Sun-synch polar 100 C-VV 30x26.3 23

Page 20: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table D - Decommissioned SAR sensors

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 19

Nat

ion

Sensor, operating agency, launch, application area Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

ERS-2 ESA, 1995-2011 -Earth observation

800 km 98.5° 35 days

100 5

SAR image mode C-VV SAR wave mode Wind scatterometer mode

26 20-26 Right looking

ENVISAT ASAR (Advanced SAR) ESA, 2002-2012

Earth observation: land, sea, ice, ocean monitoring & surveillance

800 km 98.5° 35 days

100 100 400 400 5

Image mode (HH or VV) Alternating pol (VV+HH or VV+VH or HH+HV) Wide swath mode (HH or VV) Global monitoring mode (HH or VV) Wave mode (HH or VV)

30 30 150 1000 30

15-45 Right looking

S-BAND

RU

SSIA

Almaz-1 1991-1992 Oceanography, geology, cartography & geophysics,

climate change, forestry, Agriculture, ecology

270 km 72.7°

40

HH 10-15 25-60 Left and right looking

USA

Lacrosse 1-5/Onyx NRO, 1988-2011 Military reconnaissance

666 km 57-68°

5 satellite program 1

L-BAND

JAP

AN

JERS-1 (Japanese Earth Resources Satellite) JAXA, 1992-1998

Tropical & boreal forest mapping

570 km 98.5° 44 days

75 L-HH 18 32-38

Page 21: Satellite and Airborne SAR Sensor Specifications

Robust Imaging from Space Satellite and Airborne SAR Sensor Specifications

Table D - Decommissioned SAR sensors

Cooperative Research Centre for Spatial Information (CRC-SI) – June 2012 Page | 20

Nat

ion

Sensor, operating agency, launch, application area Orbit & altitude (km) Inclination angle (°) Target revisit time

Swath width (km)

Frequency Imaging modes

Spatial resolution (m)

Incidence angle (°)

ALOS PALSAR (Phase Array L-band SAR) JAXA, 2006-2011

Earth observation

691 km 98.16° 46 days

70 70 30 350

L- Multiple modes Fine Beam Single HH Fine Beam Dual HH+HV Quad pol HH+HV+VH+VV Wide Beam HH

10 20 30 100

34.3-41.5 34.3-41.5 21.5 18-43 Right looking

CH

INA

JianBing-5 (JB 5-1/Yaogan 1) 2006-2010 Dual use Military: intelligence gathering, surveillance and

reconnaissance Earth observation: land survey, disaster forecasting,

crop yield evaluation, urban planning

628 km 97.8 °

40 100

Spotlight ScanSAR

5 20

MULTI-FREQUENCY

USA

SIR-C/X-SAR (Shuttle Imaging Radar) NASA JPL, 1994 Experimental program for multi-freq/pol/ang SAR

for extracting physical information

215 57° 2x11 day missions

15-90 15-40

C- and L- full pol (HH,HV,VH,VV) X-VV

10-200 49 Multi-ang pointing capability

USA

& G

ERM

AN

Y SRTM (Shuttle Radar Topography Mission)

NASA JPL, USA and DLR, Germany Feb 2000

Near-global DEM generation

233 km 57° 11 day mission

225

SIR-C HH+VV X-SAR HH+VV

30-90 (abs v.acc 16 m)

17-65