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Titan Sample Return Mission using V-Infinity LeveragingThe unique environment of the Saturnian moon Titan provides a particular incentive for a sample return mission in the mid twenty-first century. The thick atmosphere and low gravity provide both useful benefits and harrowing challenges that make optimizing the return trajectory, whether for time of flight or ΔV, especially important for such a long-term mission in order to maximize return. V-infinity leveraging provides a unique capability for finding epoch independent, reduced ΔV return trajectories which can be reliably converged from theoretical results. This paper will demonstrate the ability to use this technique to enable Titan sample missions and examine it relative to other options.
Document ID
20220010401
Acquisition Source
Glenn Research Center
Document Type
Conference Paper
Authors
Jeffrey D. Pekosh
(Glenn Research Center Cleveland, Ohio, United States)
Steven L. McCarty
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
July 8, 2022
Subject Category
Astrodynamics
Report/Patent Number
AAS 22-550
Meeting Information
Meeting: 2022 AAS/AIAA Astrodynamics Specialist Conference
Location: Charlotte, NC
Country: US
Start Date: August 7, 2022
End Date: August 11, 2022
Sponsors: American Institute of Aeronautics and Astronautics, American Astronautical Society
Funding Number(s)
WBS: 371544.01.21.01.22.01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
Technical Review
Single Expert
Keywords
Titan
Trajectory
Optimization
Mission Design
V-Infinity Leveraging
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