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Titan In-situ Resource Utilization (ISRU) Sample Return (TISR)Titan is unique in the outer solar system in that it is the only moon with a thick atmosphere, and the only body in the solar system outside the Earth with liquid seas on its surface. The Titanian oceans, however, are seas of liquid hydrocarbons, and the rocks on the surface are solid water ice. Like other icy Moons of the outer solar system, beneath the ice crust, Titan also has a subsurface ocean. Rodriguez et al. refer to it as the “world with two oceans”, an organic-rich body with interior-surface-atmosphere interactions that are comparable in complexity to the Earth. [1]
Titan is scientifically fascinating in many ways [2], [3], [4]. The Compass Team will emphasize just one here: Titan is a high priority target for astrobiology [4] [5] [6] [7] [8] [9] [10] [11]. It is a world with a surface and atmosphere rich in the complex organic compounds known as tholins. A detailed understanding of the nature of these complex compounds will require an analysis using a full laboratory on Earth. Because of its value to understanding the organic compounds of the outer solar system which may be the primordial building-blocks of life, return of samples from Titan to laboratories on Earth will be the primary goal of this mission.
While this would give unprecedented science return, returning even a small sample from Titan using conventional technology would be tremendously difficult. Saturn is almost a billion miles from the Earth, about thirteen times farther than Mars. A return mission to Saturn requires such a large total-mission ∆V that, with conventional technology, the mass ratios required are prohibitive. Such a sample return would truly be “mission incredible.” But to date, a sample return mission from so distant a target has been assumed to be, not merely incredible, but mission impossible. The Compass Team has proposed [2] [12] that by manufacturing the propellant for the return to Earth using the resources available on Titan, such a mission becomes possible. The task of this report is to show that it is reasonable with credible space technology.
Document ID
20220016292
Acquisition Source
Glenn Research Center
Document Type
Technical Memorandum (TM)
Authors
Steven Oleson
(Glenn Research Center Cleveland, Ohio, United States)
Geoffrey Landis
(Glenn Research Center Cleveland, Ohio, United States)
Ralph Lorenz
(Johns Hopkins University Applied Physics Laboratory North Laurel, Maryland, United States)
Elizabeth Turnbull
(Glenn Research Center Cleveland, Ohio, United States)
Thomas Packard
(HX5, LLC)
Anthony Colozza
(HX5, LLC)
David Smith
(HX5, LLC)
Jeffrey Pekosh
(Glenn Research Center Cleveland, Ohio, United States)
Steven McCarty
(Glenn Research Center Cleveland, Ohio, United States)
Zachary Zoloty
(Glenn Research Center Cleveland, Ohio, United States)
Laura Burke
(Glenn Research Center Cleveland, Ohio, United States)
James Fittje
(Science Applications International Corporation (United States) McLean, Virginia, United States)
John Gyekenyesi
(HX5, LLC)
Paul Schmitz
(Power Computing Solutions Inc. Avon Lake, Ohio, USA)
Lucia Tian
(Glenn Research Center Cleveland, Ohio, United States)
Steven Korn
(Glenn Research Center Cleveland, Ohio, United States)
Nick Uguccini
(Glenn Research Center Cleveland, Ohio, United States)
Brent Faller
(Glenn Research Center Cleveland, Ohio, United States)
Christine Schmid
(Glenn Research Center Cleveland, Ohio, United States)
Christopher Heldman
(Glenn Research Center Cleveland, Ohio, United States)
W Peter Simon
(Glenn Research Center Cleveland, Ohio, United States)
Onoufrios Theofylaktos
(Glenn Research Center Cleveland, Ohio, United States)
Date Acquired
October 28, 2022
Publication Date
December 14, 2022
Subject Category
Launch Vehicles And Launch Operations
Lunar And Planetary Science And Exploration
Spacecraft Design, Testing And Performance
Spacecraft Propulsion And Power
Report/Patent Number
CD-2021-186
E-20085
NASA/TM-20220016292
Funding Number(s)
WBS: 371544.01.21.01.22.01
Distribution Limits
Public
Copyright
Use by or on behalf of the US Gov. Permitted.
Technical Review
NASA Peer Committee
Keywords
Titan
Sample Return
ISRU
In-situ Resource Utilization
RPS
DRPS
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