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Sylph - A SmallSat Probe Concept Engineered to Answer Europa's Big QuestionEuropa, the Galilean satellite second from Jupiter, contains a vast, subsurface ocean of liquid water. Recent observations indicate possible plume activity. If such a plume expels ocean water into space as at Enceladus, a spacecraft could directly sample the ocean by analyzing the plume’s water vapor, ice, and grains. Due to Europa’s strong gravity, such sampling would have to be done within 5 km of the surface to sample ice grains larger than 5 µm, expected to be frozen ocean spray and thus to contain non-volatile species critical to a biosignature-detection mission. By contrast, the planned Europa Multiple Flyby Mission’s closest planned flyby altitude is 25 km. Sylph is a concept for a SmallSat free-flyer probe that, deployed from the planned Europa Mission, would directly sample the large grains by executing a single ~2-km altitude plume pass. The 40-kg probe would be deployed by the Europa mission just before it executes a plume fly-through. Within the probe’s 16-hour lifespan, it would autonomously navigate to perform a parallel, simultaneous pass at the lower altitude. The Sylph flight system design concept combines SmallSat technologies with robust traditional components and advanced manufacturing technologies. Its payload would comprise Mini-SUDA (SUrface Dust Mass Analyzer), a dual-channel, miniature impact ionization mass spectrometer. Sylph represents a novel type of SmallSat concept: purpose-built configuration, optimized for the harsh environment at Europa and for planetary-protection requirements, and hybridized from both mainstream and SmallSat components.
Document ID
20190025605
Acquisition Source
Jet Propulsion Laboratory
Document Type
Conference Paper
External Source(s)
Authors
Imken, Travis
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Sherwood, Brent
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Elliott, John
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Frick, Andreas
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
McCoy, Kelli
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Oh, David
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Kahn, Peter
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Karapetian, Arbi
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Polit-Casillas, Raul
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Cable, Morgan
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Lunine, Jonathan
(Cornell Univ. Ithaca, NY, United States)
Kempf, Sascha
(Colorado Univ. Boulder, CO, United States)
Southworth, Ben
(Colorado Univ. Boulder, CO, United States)
Tucker, Scott
(Colorado Univ. Boulder, CO, United States)
Waite, J. Hunter
(Southwest Research Inst. San Antonio, TX, United States)
Date Acquired
June 3, 2019
Publication Date
August 6, 2016
Subject Category
Spacecraft Instrumentation And Astrionics
Report/Patent Number
SSC-XI-06
JPL-CL-16-2517
Report Number: SSC-XI-06
Report Number: JPL-CL-16-2517
Meeting Information
Meeting: AIAA/USU Conference on Small Satellites
Location: Logan, UT
Country: United States
Start Date: August 6, 2016
End Date: August 11, 2016
Sponsors: American Institute of Aeronautics and Astronautics (AIAA), Utah State Univ.
Distribution Limits
Public
Copyright
Other

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