@Article{SchmittBeRoMoMoLo:2022:ReArGr,
               author = "Schmitt, Rodrigo N. and Bertaglia, Ana Beatriz Bressan and Rosa, 
                         Giovanni J. and Moscati, Ney R. and Moreira, Diego F. M. and 
                         Loureiro, Geilson",
          affiliation = "{Instituto Nacional de Pesquisas Espaciais (INPE)} and {Instituto 
                         Nacional de Pesquisas Espaciais (INPE)} and {Instituto Nacional de 
                         Pesquisas Espaciais (INPE)} and {Instituto Nacional de Pesquisas 
                         Espaciais (INPE)} and {Instituto Nacional de Pesquisas Espaciais 
                         (INPE)} and {Instituto Nacional de Pesquisas Espaciais (INPE)}",
                title = "OneMars: Requirements for Artificial Gravity in a Spacecraft for 
                         Transportation of a Crew to Mars",
              journal = "IEEE Journal Of Radio Frequency Identification",
                 year = "2022",
               volume = "6",
                pages = "332--346",
             keywords = "Systems engineering, Mars, stakeholder, casestudy, manned mission, 
                         lifecycle.",
             abstract = "This paper used the processes of simultaneous and systems 
                         engineering to develop a solution that addresses both the main 
                         concerns of a manned mission to Mars and the Artificial Gravity 
                         System (AGS) requirements that shall be used during the concept 
                         phase of a spacecraft to be utilized to transport a crew to Mars. 
                         The study shows different tools of the systems engineering 
                         process. Steps taken in the paper include: (a) determining the 
                         main stakeholders, objectives and measures of effectiveness, 
                         analysis of the operation scenario, capabilities and constraints, 
                         concept of operations; (b) outlining the lifecycle of the project 
                         and determining main reviews and the product breakdown structure; 
                         (c) analyzing stakeholder for the spacecraft, including concerns 
                         and requirements; (d) breaking down stakeholder requirements to 
                         non-functional and functional requirements; (e) analyzing the 
                         systems main functions by reviewing the context, circumstances, 
                         operation modes, list of events, essential functions, hazards and 
                         risks; (f) architecting the spacecraft through: breakdown of 
                         subsystems, morphological diagram, architecture flow and 
                         interconnect diagrams, analysis of artificial gravity options and 
                         requirements specification for the artificial gravity subsystem.",
                  doi = "10.1109/JRFID.2022.3162098",
                  url = "http://dx.doi.org/10.1109/JRFID.2022.3162098",
                 issn = "2469-7281",
                label = "lattes: 8964296905359885 2 SchmittBeRoMoMoLo:2022:ReArGr",
             language = "en",
           targetfile = "
                         
                         OneMars_Requirements_for_Artificial_Gravity_in_a_Spacecraft_for_Transportation_of_a_Crew_to_Mars.pdf",
        urlaccessdate = "25 jun. 2024"
}