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  • Advanded propulsion for fast lunar missions

    Paper number

    IAC-21,A5,1,14,x63408

    Author

    Prof. Giancarlo Genta, Italy, Politecnico di Torino

    Year

    2021

    Abstract
    The Moon is the closest celestial body and can be reached easily and in a relatively short time using chemical propulsion, as was demonstrated half a century ago by the Apollo missions. The introduction of reusable launchers and other innovations will reduce the cost of reaching our satellite making it easier to build lunar infrastructures and to develop a lunar economy, of which lunar tourism will be an important part. All this can be done without advances in propulsion, except for improvements and cost reduction or chemical rockets. While these developments will be under way, advanced propulsion will be developed mostly for human planetary missions, which on the contrary lie beyond (or in the case of Mars at the border of) the possibilities of chemical propulsion.
    The first possibility is Nuclear Thermal propulsion (NTP), which can allow to reduce the time to reach the Moon from 4-4.5 days to about 3 days, with a reduction of the initial mass in low Earth orbit (IMLEO). Perhaps it is not worth while to develop NTP for this application, but if made available to reach Mars, it would be useful to build a fast lunar reusable nuclear shuttle.
    All other advances in propulsion are linked with low thrust devices, which are more suitable for interplanetary than for lunar missions, in which all the travel must be performed in a gravitational field much stronger than the interplanetary field. A low thrust lunar trajectory is made of a multi-turn geocentric spiral plus a selenocentric spiral with possibly a coasting arc in between. With the thruster and power generator performance expected for near and medium term NEP and SEP devices the minimum travel time is at least 10 days, with many hours (or days) spent in the Van Allen radiation belts. 
    This means that SEP and NEP (and even more solar sails) are unsuitable for human lunar missions, while allowing to build cargo spacecraft.
    Thigs may be different if generators with a very low specific mass are built, or above all if the studies on Direct Fusion Drive (DFD) technology prove to be successful. A DFD spacecraft will allow to reach the Moon two days or less, an interesting perspective for human transportation to the lunar bases and other touristic infrastructures.
    The present paper shows examples of lunar missions performed with different types of advanced propulsion, improving human transportation to the Moon only when large advances in propulsion will be achieved. Even in the unlikely case in which the ideas about propellantless propulsion will prove to be more than just dreams, the constraints about the specific mass of the generator will remain.
    Abstract document

    IAC-21,A5,1,14,x63408.brief.pdf

    Manuscript document

    IAC-21,A5,1,14,x63408.pdf (🔒 authorized access only).

    To get the manuscript, please contact IAF Secretariat.