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  • 6
  • session 6

    Title

    System Engineering Tools, Processes and Training (2)

    type

    oral

    Description

    This session will focus on state-of-the-art system engineering methodologies, design techniques, tools, processes, and training that reduce the time and cost, and improve the quality of space system design. Of special interest are multi-disciplinary methods, tools, and processes including modelling and simulation used to define system architectures to improve risk management, safety, reliability, testability, quality of life cycle cost estimates, and to improve the training of system engineers.

    Date

    2013-09-27

    Time

    13:30

    Room

    302B

    IPC members
    • Chairman: Dr. Tibor S. Balint, Jet Propulsion Laboratory, United States;

    • Chairman: Dr. Norbert Frischauf, TU Graz, Austria;

    • Rapporteur: Dr. Geilson Loureiro, National Institute for Space Research - INPE, Brazil;

    papers

    Order

    Time

    Paper title

    Mode

    Presentation status

    Speaker

    Affiliation

    Country

    1

    enhanced model-based system engineering to aid the DelFFi formation flying mission

    15'

    confirmed

    Dr. Lin Huang

    *Delft University of Technology (TU Delft), The Netherlands; #DFH Satellite Company, Ltd.

    China

    2

    Model Based Systems Engineering (MBSE) applied through a SysML model to the MASCOT asteroid lander

    15'

    confirmed

    Mr. Michael Kretzenbacher

    Monash University

    Australia

    3

    Analysis and verification of communication link budgets for small satellites

    15'

    confirmed

    Ms. Miriam Vázquez Vázquez

    Delft University of Technology (TU Delft)

    The Netherlands

    4

    Probabilistic Assessment and Optimization for Fractionated Spacecraft Architecture from the Economic Cost Point of View

    15'

    confirmed

    Mr. Ang Zhang

    Beihang University

    China

    5

    A Complete Performance Tests of an Analogue Sun Sensor with Improved Linearity, Variable Slit and Shutter Distance

    15'

    confirmed

    Dr. Pavel Paces

    Czech Technical University In Prague (CTU)

    Czech Republic

    7

    a general conceptual model for launch vehicle design and analysis

    15'

    confirmed

    Mr. Suhong Ma

    Beijing Institute of Aerospace Systems Engineering, China Aerospace Science and Technology Corporation (CASC)

    China

    8

    THE MICROSATELLITE LAUNCH VEHICLE (VLM-1) FUNCTIONAL ANALYSIS

    15'

    confirmed

    Mr. Jonas Bianchini Fulindi

    Instituto de Aeronáutica e Espaço (IAE)

    Brazil

    9

    AN APPROACH TO THE DEVELOPMENT OF THE VLM-1 FIRST STAGE PYROTECHNIC SUBSYSTEM

    15'

    confirmed

    Mr. Luis Henrique Ferreira da Silva

    DCTA-IAE

    Brazil