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There is a need to achieve optimal cost effectiveness from remote sensing missions. Concurrently, a key scientific need in remote sensing is to address the spatial and temporal resolution of atmospheric measurements. Improved temporal resolution observations of the atmosphere – and importantly a reduced latency between observation and delivery to the user – can directly improve weather forecasting services.
Surrey Satellite...
This summary presents the work by the University of Strathclyde, SCISYS and Roke Manor Research in response to the ESA SysNova Challenge AO7891; Remote sensing with cooperative nanosats, Challenge #3 – Weather. The objective of this work was to evaluate the performance and cost of multi-agent satellite networks capable of providing data in support of severe weather monitoring.
UNIVERSITY OF STRATHCLYDE
Performance of nanosatellite systems is reaching a level sufficient for supporting Earth Observation applications, while instrument development focuses on miniaturization. By using a multitude of cooperating and cost effective satellites, nanosat technology could be a serious competitor for conventional EO missions
Instituto Superior de...
The Light Touch2 concept proposes the use of laser ablation to change the orbital velocity of a 4m, 130 ton, asteroid by 1m/s in less than 3 years A laser beam is used to sublimate part of the asteroid material and generate a low and continuous thrust. This study demonstrates how to implement this concept on a medium class interplanetary spacecraft, here called AdAM (Asteroid Ablation Mission).
Methodology
UNIVERSITY OF STRATHCLYDE
KABOOM
We study a low-cost interplanetary mission to demonstrate the capability of artificially modifying the orbit of a small (250 ton) binary asteroid body. The targeting spacecraft survives the slow (~1 m/s) impact to carry out the orbit modification measurement afterwards.
Methodology:
Politechnico di Milano
BEAST aims to modify the orbital period of the small secondary object of a binary asteroid by kinetic impact. BEAST analyses a commercial LEO platform accommodating as payload the impactor and GNC system with total mission cost below 150 M€.
The objective of the Cobra mission is to use a conventional chemical thruster to modify the orbit of a man-made object through plume impingement. The proposed concept uses a standard satellite platform with a modified payload to suit mission needs.
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