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- W2912759030 abstract "For spacecraft interplanetary mission, gravity assist manoeuvres are usually used because they allow to get generally high ∆V without have recourse to the consumption of propellant, but exploiting the energy provided by the gravitational attraction of a celestial body. This allows to improving the useful mass for a specific mission, for a modest increase in flight time. Thus, when evasion from Earth’s sphere of influence is considered, lunar gravity assist manoeuvers become a valid alternative to direct escapes. In this paper two consecutive gravity assist manoeuvres are considered and is researched the possible moon-to-moon trajectories that allow their. Af- terward, considering different spacecraft initial speeds relative to Moon, the effect on the escape orbit is analyzed, with the purpose to link the features of the latter – heliocentric flight-path angle and declination – to the maximum obtainable specific mechanical energy (i.e. the achievable escape velocity)." @default.
- W2912759030 created "2019-02-21" @default.
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- W2912759030 date "2018-10-23" @default.
- W2912759030 modified "2023-09-27" @default.
- W2912759030 title "Escape maneuvers with lunar gravity assists" @default.
- W2912759030 hasPublicationYear "2018" @default.
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