Applying the perturbative integral in aeromaneuvers around Mars to calculate the cost

The perturbative integral method was applied to quantify the contribution of external forces during a specific interval of time in trajectories of spacecraft around asteroids and under the Luni-solar influence. However, this method has not been used to quantify the contributions of drag in aerocaptu...

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Veröffentlicht in:	arXiv.org 2023-07
Hauptverfasser:	Jhonathan O Murcia Piñeros, Antônio F Bertachini de Almeida Prado, dos Santos, Walter Abrahão, Rodolpho Vilhena de Moraes
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerobraking Aerocapture Drag devices Energy consumption Maneuvers Mars Mass ratios Mathematics - Dynamical Systems Orbits Physics - Earth and Planetary Astrophysics Propulsion systems Retrograde orbits Solar sails Three body problem Trajectory analysis
Online-Zugang:	Volltext
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