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Trajectory design considerations for small-body touch-and-go"Touch-and-Go," or TAG, is an approach to small-body surface interrogation missions in which the spacecraft descends to the surface, remains in contact for a short time, and then ascends without coming to rest. Appropriate trajectory design solutions to support TAG missions vary widely based on the spacecraft dynamics, small-body environment, spacecraft and ground systems capabilities, and mission objectives. This paper discusses various factors that are considered during the process of developing a TAG mission trajectory and presents a few case study examples to demonstrate how TAG trajectories may vary from mission to mission.
Document ID
20210005744
Acquisition Source
Jet Propulsion Laboratory
Document Type
Preprint (Draft being sent to journal)
External Source(s)
Authors
Cangahuala, Alberto
Bhaskharan, Shyam
Bonfiglio, Eugene
Broschart, Stephen
Wallace, Mark S.
Date Acquired
February 14, 2011
Publication Date
February 14, 2011
Publication Information
Publisher: Pasadena, CA : Jet Propulsion Laboratory, National Aeronautics and Space Administration, 2011.
Distribution Limits
Public
Copyright
Other
Technical Review

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