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  • A STANDARD SPACE TRANSPORTATION AND INFRASTRUCTURAL SYSTEM FOR AN AFFORDABLE THREE STEPS PATH TO MARS MANNED MISSIONS

    Paper number

    IAC-16,D2,IP,1,x32794

    Coauthor

    Mr. Giorgio Gaviraghi, Unispace Exponential Creativity, Italy

    Year

    2016

    Abstract
    Recently , with the  availability  of  heavy launchers such as the Falcon heavy  from Space X and  the SLS from NASA  it will be possible to send ambitious manned missions out of LEO due to its higher payload capacity.
     In order to optimize its utilization and obtain the maximum results at affordable conditions we may require a  transportation system composed of few standard components that can be reutilized while  simplifying  all operations in a cruiser/cycler-feeder system allowing affordable costs for outer space manned missions.                                                                                                                                                                                     Such components  for the transportation system can be summarized as :                                                                                                                             1-The Cruiser (to be positioned in a cycling trajectory, Moon, Mars etc)
    -Service module  (with SEP capabilities)                                                                                                                  -Standard container system (including Hab module)                                                                                                                     -Node modules (for expansion possibilities)                                                                                                        -Telescoping spikes and ring modules (for future 1 G capability)                                                                                                                  2-The Feeder  (to connect the cruiser with ground or space stations)                                                                                                                                                                                -Ground  lander  (Mars , Moon , Phobos etc) with container delivery                                                                                                                         -Space transfer module (cruiser to space station  etc)
    3-An Earth return capsule, from those that will be available from private companies or from NASA  ( Orion)
    The infrastructural system in space will be composed by the same modules as the cruiser while on the ground by:                                                                                                                                                                                          -Inflatable and 3d printed basic module (for HAB,  lab, agricultural and manufacturing  functions)      –A connector system , equipped with hydroponics cultivation                                                                                                                      – An airlock and rover vehicle shelter unit
    With a sequential launches and reutilization of this system we can obtain  immediate and affordable  results such as :
    -Venus and Mars manned flyby (2021 window opportunity with Falcon Heavy launcher utilizing on board 3d printing for Hab module)                                                                                                                                                                                        – Phobos  manned way station  (with SLS launcher ) and unmanned Mars preliminary lander  (separate SLS launch)                                                                                                                         -Martian manned mission with support from the Phobos station (SLS launcher)
    The above will be briefly described in this paper , including 3d printing utilization for the station and outpost construction in Phobos and Mars
    Abstract document

    IAC-16,D2,IP,1,x32794.brief.pdf

    Manuscript document

    (absent)