INPE Agency Report

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

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

PLAN 2010 - 2020

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)

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

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

MMP - INPE-LIT (2008)

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

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

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

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

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

Proposed instrument package Passive Microwave Imager/Sounder

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

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