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The Europa Clipper Gravity and Radio Science (G/RS) InvestigationNASA’s Europa Clipper flagship mission launched on October 14, 2024 and will arrive at Jupiter in April 2030. There, it will investigate the habitability of Jupiter’s moon Europa. Gravity and Radio Science (G/RS) is one of ten complementary investigations devoted to understanding Europa through studies of its ice shell and ocean, its composition, and its geology. G/RS makes use of the Europa Clipper telecommunications system to obtain radiometric tracking data during the Europa flybys.

Unlike past missions, the primary raw data for the G/RS investigation are obtained from OpenLoop Receivers (OLR) at the Deep Space Network (DSN) ground stations. Indeed, the flyby geometry, spacecraft attitude, and spacecraft antenna configuration are such that the signal-tonoise ratio of the return radio signals will be small (<10 dB-Hz) and insufficient for the typical closed-loop tracking. Processing of the OLR with special retracking algorithms will be necessary to obtain range-rate (Doppler) observations. Given the lack of a stable oscillator onboard Europa Clipper, two-way tracking will be used to achieve high frequency stability, leveraging the accurate DSN clocks. Radio tracking during the flybys will be performed at a single frequency (X-band), so careful modeling of media perturbations is important to maximize the G/RS results. We will discuss recent work to assess the impact of media perturbations from the Io Plasma Torus on orbit reconstruction and geophysical parameter recovery.

G/RS will obtain measurements of Europa’s static and time-variable gravity field. The tidal Love number k2 will verify the presence of a subsurface ocean and help constrain the ice shell. The moment of inertia, derived from degree-2 gravity coefficients, will help determine the interior structure. The radio tracking data will also be sensitive to Europa’s ionosphere when geometry allows.

We will present the G/RS investigation and observation plans, its expected performance, and provide a first look at the tracking data during cruise.
Document ID
20250000526
Acquisition Source
Goddard Space Flight Center
Document Type
Abstract
Authors
Erwan Mazarico
(Goddard Space Flight Center Greenbelt, United States)
Dustin Buccino
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Julie Castillo-Rogez ORCID
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
Andrew Dombard
(University of Illinois Chicago, Rockford campus Rockford, United States)
Antonio Genova
(Sapienza University of Rome Rome, Lazio, Italy)
Hauke Hussmann
(German Aerospace Center Cologne, Germany)
Walter Scott Kiefer
(Lunar and Planetary Institute Houston, Texas, United States)
Jonathan Lunine
(Jet Propulsion Laboratory (JPL), California Institute of Technology (CalTech) Pasadena, CA, United States)
William McKinnon ORCID
(Washington University in St. Louis St Louis, United States)
Francis Nimmo ORCID
(University of California, Santa Cruz Santa Cruz, United States)
Ryan Park ORCID
(Jet Propulsion Laboratory La Cañada Flintridge, United States)
James Roberts
(Johns Hopkins University Applied Physics Lab)
Paolo Tortora
(University of Bologna Bologna, Italy)
Paul Withers
(Boston University Boston, United States)
Gael Cascioli
(Sapienza University of Rome Rome, Lazio, Italy)
Martina Caussi
(University of Illinois Chicago, Rockford campus Rockford, United States)
Martina Ciambellini
(Sapienza University of Rome Rome, Lazio, Italy)
Benjamin Idini
(University of California, Santa Cruz Santa Cruz, United States)
Andrea Magnanini
(University of Bologna Bologna, Italy)
Alyssa C Mills
(Baylor University Waco, Texas, United States)
Flavio Petricca
(Sapienza University of Rome Rome, Lazio, Italy)
Marco Zannoni
(University of Bologna Bologna, Italy)
Date Acquired
January 15, 2025
Subject Category
Lunar and Planetary Science and Exploration
Meeting Information
Meeting: European Geosciences Union (EGU 2025)
Location: Vienna
Country: AT
Start Date: April 27, 2025
End Date: May 2, 2025
Sponsors: European Geosciences Union
Funding Number(s)
WBS: 684499.04.02.04
Distribution Limits
Public
Copyright
Portions of document may include copyright protected material.
Technical Review
NASA Peer Committee
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