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Europa Jupiter System Mission

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Europa Jupiter System Mission
NameEuropa Jupiter System Mission
Mission typePlanetary science
OperatorEuropean Space Agency / National Aeronautics and Space Administration
Launch datePlanned 2020s (reconfigured)
StatusReconfigured; elements continued as JUICE and Europa Clipper

Europa Jupiter System Mission

The Europa Jupiter System Mission was a joint project proposed by European Space Agency and National Aeronautics and Space Administration to study the Jovian system, with emphasis on Europa, Ganymede, Callisto, and Io. The concept united expertise from agencies such as Agenzia Spaziale Italiana, Centre National d'Études Spatiales, Deutsches Zentrum für Luft- und Raumfahrt, and contractors like Thales Alenia Space, aiming to combine a European orbiter and a US-led probe. Planning engaged scientific communities associated with institutions including Jet Propulsion Laboratory, Max Planck Institute for Solar System Research, University of Oxford, California Institute of Technology, and University of Colorado Boulder.

Background and objectives

The proposal followed discoveries by missions such as Voyager 1, Voyager 2, Galileo, and Cassini–Huygens that revealed subsurface oceans and active geology on icy satellites. Objectives aligned with priorities set by panels like the NRC and European Science Foundation, addressing astrobiology questions posed by Exobiology-focused researchers at NASA Astrobiology Institute and the European Astrobiology Institute. Primary aims included characterizing Europa’s ice shell, mapping Ganymede’s magnetosphere, assessing Callisto’s surface, and studying Io volcanic activity, consistent with recommendations from the Planetary Science Decadal Survey and the Cosmic Vision program.

Mission concept and design

The original concept envisioned a two-spacecraft architecture: a NASA-led Europa orbiter and an ESA-led Jupiter Ganymede orbiter, inspired by multi-spacecraft strategies used by Cassini–Huygens and Rosetta. Design studies involved firms including Airbus Defence and Space, Lockheed Martin, Boeing, and research centers such as Institut d'Astrophysique Spatiale and Smithsonian Astrophysical Observatory. Engineering constraints referenced heritage from Mars Reconnaissance Orbiter, Magellan, and MESSENGER, while addressing radiation mitigation techniques developed at Los Alamos National Laboratory and NASA Glenn Research Center. The mission architecture examined power systems similar to MMRTG, communications strategies from Deep Space Network, and launch options using vehicles like Ariane 5, Atlas V, and Delta IV Heavy.

Spacecraft and instrumentation

Instrument suites drew on instruments analogous to Juno's magnetometer, New Horizons's imaging systems, and Galileo's plasma instruments. Proposed payloads included ice-penetrating radar developed by teams at German Aerospace Center (DLR), spectrometers from Royal Observatory, Edinburgh, high-resolution cameras from European Southern Observatory collaborators, and mass spectrometers from University of Bern. Additional instruments considered were thermal imagers leveraging expertise from Institut d'Astrophysique Spatiale, laser altimeters inspired by ICESat technology, and submillimeter radiometers from NASA Jet Propulsion Laboratory groups. Radiation-hardened electronics relied on research at Fraunhofer Society and Sandia National Laboratories.

Planned operations and trajectory

Baseline trajectories included gravity assists similar to paths used by Galileo and Cassini–Huygens, with potential flybys of Earth, Venus, or Mars to achieve Jupiter insertion. Operational planning referenced mission ops centers like European Space Operations Centre and NASA's Deep Space Network, and employed navigation strategies developed at NASA Jet Propulsion Laboratory and European Space Operations Centre. Science orbits considered polar mapping of Europa, long-term monitoring of Ganymede magnetospheric dynamics, and coordinated flybys of Io to observe volcanic plume activity, following operational precedents set by Galileo and Voyager 1 mission timelines.

Scientific goals and experiments

Experiments targeted characterization of subsurface oceans inferred from Magellan-era geophysical methods and later missions, investigation of surface composition via spectrometers to detect compounds like water (H2O), carbon dioxide, and organic molecules, and assessment of radiation-driven chemistry relevant to astrobiology discussions at NASA Astrobiology Institute. Studies intended to examine tidal heating processes analyzed by researchers at Caltech and University of Arizona, map magnetic induction signatures studied at Imperial College London, and search for plumes analogous to discoveries at Enceladus. Collaborative science teams included investigators from Smithsonian Institution, Cornell University, University of Tokyo, and California Institute of Technology.

International collaboration and management

Management structures proposed mirror arrangements from Cassini–Huygens and Rosetta, with shared responsibilities between European Space Agency and National Aeronautics and Space Administration, and contributions from agencies like Japan Aerospace Exploration Agency, Canadian Space Agency, Russian Federal Space Agency, and Australian Space Agency partners. Scientific governance involved advisory panels including members from International Astronomical Union, European Science Foundation, and the National Academy of Sciences. Industrial participation encompassed Thales Alenia Space, Arianespace partners, Space Systems/Loral, and university consortia such as Jet Propulsion Laboratory-led teams and European university laboratories.

Development history and cancellation/reconfiguration

The project evolved through mission studies at European Space Agency and NASA Jet Propulsion Laboratory after initial proposals in the 2000s, influenced by budgetary decisions shaped at institutions like the United States Congress and European Parliament and reprioritization in the Planetary Science Decadal Survey. Programmatic reviews invoked lessons from Mars Climate Orbiter and Mars Polar Lander failures and fiscal constraints linked to broader agency portfolios. Ultimately, elements of the design were reconfigured: the European component advanced as JUICE focusing on Ganymede, while the US component progressed as Europa Clipper concentrating on Europa, reflecting international negotiation outcomes similar to earlier collaborations like Cassini–Huygens and later cooperative agreements between NASA and ESA.

Category:Proposed space probes to Jupiter