Mission Analysis for Landing on Pluto from a Fast, Hyperbolic Trajectory

The results of a Pluto landing analysis study for a fast, hyperbolic approach trajectory are presented by assuming the use of a novel entry, descent, and landing system called an enveloping aerodynamic decelerator. A landing site uncertainty analysis is performed for an 11 September 2040 arrival by...

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Veröffentlicht in:	Journal of spacecraft and rockets 2023-05, Vol.60 (3), p.972-981
Hauptverfasser:	Warnecke, Mark, Nock, Kerry T., Aaron, Kim M.
Format:	Artikel
Sprache:	eng
Schlagworte:	Altitude Atmosphere Deceleration Gravity Hyperbolic trajectories Landing aids Landing sites Pluto Uncertainty analysis Velocity
Online-Zugang:	Volltext
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