Year: 2025
Type: article
Abstract: To accomplish scientific objectives, spacecraft exploring the Jovian system require close flybys of Jupiter’s inner moon of Europa. However, the ΔV cost of a direct transfer to Europa is prohibitively expensive, so ballistic flybys with the other moons in the system are required to lower the energy of the spacecraft relative to Jupiter. Sequences of ballistic flybys can simultaneously alter the spacecraft’s trajectory in a desirable way and provide additional opportunities for scientific observation. Using a patched conics simulation, the N-Revolution Lambert’s problem can be solved to find sequences of flybys that enable low transfers between the four major Jovian moons.
Source: Journal of Student Research
Authors: Adi Suhit Jha, William Brandenburg
Language: English
Subfield: Aerospace Engineering
Field: Engineering
Domain: Physical Sciences
Open Access status: diamond
OpenAlex ID: W4413564944