THE MICROSATELLITE LAUNCH VEHICLE (VLM-1) FUNCTIONAL ANALYSIS
- Paper number
IAC-13,D1,6,8,x18285
- Author
Mr. Jonas Bianchini Fulindi, Instituto de Aeronáutica e Espaço (IAE), Brazil
- Coauthor
Dr. Luis Eduardo Loures da Costa, CTA-IAE, Brazil
- Coauthor
Mr. Josef Ettl, Deutsches Zentrum für Luft- und Raumfahrt e.V. (DLR), Germany
- Coauthor
Prof. Geilson Loureiro, Instituto Nacional de Pesquisas Espaciais (INPE), Brazil
- Year
2013
- Abstract
This papers aims to present the functional analysis for the microsatellite launch vehicle – VLM-1. In this phase of the systems VLM-1 development the systems requirements are linked to the functional logical models. Concerning on the necessity to develop an architecture free of implementation the functional architecture lead to the functions that the VLM-1 should accomplish. The functions are deployed from the scenarios in the product life cycle processes. This approach focus on the model-based systems engineering. A commercial systems engineering tool is used to capture and manage the functions derived from the logical models of the vehicle and its scenarios. The results are the management of the exchange of engineering product data derived from the VLM-1 system analysis and the traceability through the life cycle of the product. Models generated using the commercial systems engineering tool also enables an effective control and configuration management.
- Abstract document
- Manuscript document
(absent)