Titlebook: Small Satellites for Earth Observation; Selected Contributio Rainer Sandau,Hans-Peter Röser,Arnoldo Valenzuela Book 2008 Springer Science+B

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Trends and Visions for Small Satellite Missionsevelopment efforts leading to miniaturization of engineering components, development of micro-technologies for sensors and instruments, and others which allow the design of dedicated, well-focused Earth observation missions. Application Specific Integrated Micro-instruments (ASIM) are enabled by Mic

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Development of the MicroSat Programme at INTA-5 ASAP, the Phase-A one year study was initiated in Oct. 05. At this moment we are running the Phase-B started in Nov. 06 that will finish with a PDR in Dec. 07. The first INTAµSAT-1 will be a very agile Earth observation mission using CMGs, with a launch tentative date by the beginning of 2010. Th

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Moving Towards Commercial Earth Observation Services with Small Satellite Constellationss of small spacecraft. The paper will discuss two new spacecraft for customers in Spain and Nigeria, and how these meet traditional needs for Earth Observation data at a low cost. The range of payload options which SSTL can offer for a wide variety of Earth imaging applications covering high and med

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Small Satellites and Earth Observation Systems for Small Countries and Regions students from the International Space University (ISU) worked on a project aiming at making EO accessible to small countries and regions. Although EO programs are costly to initiate, they are often feasible and beneficial for small countries and regions. However an information gap exists between EO

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Development of a High-Performance Optical System for Small Satellitesed electro-optical system as part of the national space research and development program. Its optical aperture diameter is 120 mm, the effective focal length is 462 mm, and its full field-of-view is 5.08 degrees. The dimension is about 600mm x 400mm x 400mm and its weight is less than 15 kg..To demo

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Feasibility of a Constellation of Miniature Satellites for Perform ing Measurements of the Magnetic nd boom design for such a mission is discussed. After studying communication, power and mass requirements it is found that it is feasible to develop a 10 x10 x 30 cm. satellite with a mass of about 2.5,kg, which can fulfill such a mission. We also study the feasibility of controlling a constellation

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Preliminary Concepts and Analysis of Future Earth Observation Missions Based on Distributed Radarsignals from multiple coherent receivers allows to overcome intrinsic performance limitations of monolithic SAR systems. This paper deals with an overview of recent advances and ideas in the field of distributed sparse filled aperture radar concepts and required signal processing. Then, preliminary s