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• W965431534 abstract "When confronting the design of a new space science mission the ideal situation would be one where a team ofscientists would set the scientific goals and define a model payload. Subsequently, an engineering team would definethe constraints this payload imposes on the mission analysis, spacecraft design and ground segments. But this ismuch more complex since limitations imposed by system-related elements have also an impact on the payloaddesign. Because of this, both the scientific and engineering teams must work together and be capable of redefiningscientific requirements so as to obtain a feasible design that does not compromise the essential objectives of themission. For this process to be seamless, members of the scientific team should have some understanding of thetechnical issues, and members of the technical team should have a knowledge base that allowed them to understandthe critical science issues. In reality, the fact that in a (e.g. concurrent) design study there are rarely payloaddevelopers present in either group tends to create a situation where the science team focuses on maximizingfunctionality, whereas the engineers target a robust system, and neither are able to size and define the payload and itsimpact on the system in a rapid and realistic way. To aggravate the situation, there are presently no tools, nor anyknown rules or relations between objectives and instruments that can help in the preliminary modelling of multiplepayload sets. A study at the DLR Institute of Space Systems is currently ongoing to unearth said relations if theyexist, with a long term goal of developing system engineering tools which can help in the preliminary design processfor scientific exploration missions. The present paper recalls the problems and processes during the preparation of ascience mission, especially in the European environment. It outlines how information from past missions could leadto a more robust preliminary system design through the use of dedicated analyses tools which propose potentialinstrument combinations, and can increase mutual understanding between scientists and engineers. This paperdescribes the steps of DLR’s attempt to better organize such activities, and presents some preliminary results aboutinstrument evolutions, trends and relations, based on the initial historical data gathering phase. These constantlyevolving results will be later used to create tools for e.g. model payload proposals and system requirementderivation." @default.
• W965431534 created "2016-06-24" @default.
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• W965431534 date "2014-10-03" @default.
• W965431534 modified "2023-09-27" @default.
• W965431534 title "SUPPORTING MODEL PAYLOAD SELECTION FOR SCIENCE MISSION FORMULATION" @default.
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• W965431534 hasPublicationYear "2014" @default.
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