The use of libration points as transfer nodes for an Earth-Mars transportation system is briefly described. It is assumed that a reusable Interplanetary Shuttle Vehicle (ISV) operates between the libration point and Mars orbit. Propellant for the round-trip journey to Mars and other supplies would be carried from low Earth orbit (LEO) to the ISV by additional shuttle vehicles. Different types of trajectories between LEO and libration points are presented, and approximate delta-V estimates for these transfers are given. The possible use of lunar gravity-assist maneuvers is also discussed.
Libration-Point Staging Concepts for Earth-MARS Transportation
1986
12 pages
Report
No indication
English
Spacecraft Trajectories & Flight Mechanics , Manned Spacecraft , Earth-mars trajectories , Interplanetary flight , Libration , Manned space flight , Space transportation system , Spacecraft trajectories , Stage separation , Earth orbits , Mars (Manned reusable spacecraft) , Propellant transfer , Shuttle derived vehicles , Space shuttle orbiters , Transfer orbits
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