1. INPE
Agency Report

2. CBERS: China-Brazil Earth Remote Sensing Satellite
CBERS-2B Launch (19 September 2007 – end March 2010)

3. CBERS-2B Composed image CCD - HRC Sao Paulo Airport - March 2008

4. PLAN

5. Roteiro INPE 2020 CBERS-3 CBERS-4 CBERS-5 CBERS-6 SABIA Lattes-1 GPM
2009
2010
2011
2012
2013
2014
2015
2016
2017
2018
2019
2020
CBERS-3
CBERS-4
CBERS-5
CBERS-6
SABIA
Platform CBERS
Platform PMM
Lattes-1
GPM
Lattes-2
Platform
Nanosatellite
Missions to be defined
Amazônia-1
MAPSAR
Amazônia-2
GEO Met BR
SCD Avan. (1)
SCD Avan. (1)

6. CBERS 3 – 4 Sensor Configuration
WFI 73 m (860 km)
MSS 40 m (120 km)
CCD 20 m (120 km)
MUX 10 m (60 km)
PAN 5 m (60 km)
0.4
0.5
0.7
0.9
1.1
1.5
1.7
2.1
2.3
Built by China
Built by Brazil mm

7. Multimission Plataform - MMP
Orbit : 600 a 1200 km
Payload :280 kg Platform: 250 kg 7

8. MMP - INPE-LIT (2008)

9. Remote Sensing Satellite – AMAZON 1
PMM equipped with CCD camera and a data collecting transponder.
Polar orbit.
Main applications:
Agriculture – Surveying of cultivated areas and productivity estimates;
Water resources – monitoring of pollution in coastal areas;
Disaster management.
AWFI
0,45-0,52 B
0,52-0,59 G
Spectral bands ( m m)
0,63-0,69 R
0,77-0,89 NIR
Spatial resolution (m) 40
Swath (km)
800
Revisit period (days) 5

10. LATTES (missões EQUARS e MIRAX)
MIRAX: Hard and soft X-rays
EQUARS
Stratosphere Temperature, Water vapor in the troposphere ionosphere electron perturbation

11. MAPSAR Parameters subreflector, data downlink antenna reflector
MMP
SAR payload
antenna feed horn
solar panel
subreflector, data downlink
MAPSAR
Under Revision
Parameters
Frequency L band
Polarization single, dual and quad polarization
Incidence interval 20° – 45°
Spatial resolution 3 – 20 m
Swath 20 – 55 km
Orbit sun-synchronous
Coverage global
Look direction ascending/descending and left/right
Revisit period weekly
Access to data near real time
Add. requirements Interferometry and stereoscopy

12. Global Precipitation Mission (GPM-BR)
Core Satellite Sensor is a Passive Microwave Sensor, Conical Scanning
Low inclination Orbit
Brazilian- French contribution to GPM constellation
INPE – CNES
Phase Zero to be concluded in September 2010

13. GPM – Sensors specification been considered ìn phase Zero
Altitude: ~600km
Sampling sector: ~130°
Antenna size: ~80cm
Onboard angle: ~47° (this leads to a incident angle of ~53° on Earth surface, below the Brewster angle)
The effective swath would be about 1200km

14. Proposed instrument package
Passive Microwave Imager/Sounder

15. Proposed instrument package
Sub-millimetric passive microwave imager
Lightning Imaging Sensor
TOA Radiation imager

16. Thank you