ERDSAT, a satellite concept for Earth observations with combined optical and microwave payload

Abstract

The concept of a European remote sensing satellite (ERDSAT) launched by ARIANE is characterized by a model payload, consisting of a synthetic aperture radar (SAR) and an optical multispectral scanner with 9 channels, for land applications or coastal zone missions. The mission goal of ERDSAT is based on European user requrements where a strong need for optical and microwave sensor operation on board the same satellite in a simultaneous or sequential mode is expressed. A data collection system is included. The proposed spacecraft is three-axes-stabilized and has a Sun-synchronous, near polar circular orbit with 750 km altitude. The selected configuration separates payload module and bus module. A thermostable carbon fibre grating structure is the central framework of the satellite. Each major subsystem is housed in a separate compartment and can be integrated and tested individually. First mass estimates resulted in 450 kg for the payload and 880 kg for the bus. The maximum power needed is 1750 W (for 6 min three times a day), which will be provided by a 1330 W solar array and two batteries. A “low cost” model philosophy is defined; the time schedule envisages a program start in late 1980 and a launch possibility end of 1985.