Europa Clipper


Europa Clipper is an interplanetary mission in development by NASA comprising an orbiter. Set for a launch in 2024, the spacecraft is being developed to study the Galilean moon Europa through a series of flybys while in orbit around Jupiter.
This mission is a scheduled flight of the Planetary Science Division, designated a Large Strategic Science Mission, and funded under the Planetary Missions Program Office's Solar System Exploration program as its second flight. It is also supported by the new Ocean Worlds Exploration Program. Europa Clipper will perform follow-up studies to those made by the Galileo spacecraft during its eight years in Jupiter orbit, which indicated the existence of a subsurface ocean underneath Europa's ice crust. Plans to send a spacecraft to Europa were initially conceived with projects such as Europa Orbiter and Jupiter Icy Moons Orbiter, in which a spacecraft would be injected into orbit around Europa. However, due to the adverse effects of radiation from Jupiter's magnetosphere in Europan orbit, it was decided that it would be safer to inject a spacecraft into an elliptical orbit around Jupiter and make 44 close flybys of the moon instead. The mission began as a joint investigation between the Jet Propulsion Laboratory and the Applied Physics Laboratory.
The mission will complement ESA's Jupiter Icy Moons Explorer launching in 2022, which will fly-by Europa twice and Callisto multiple times before moving into orbit around Ganymede. They may launch within a year of each other, but the Jupiter Icy Moons Explorer may have a cruise phase almost three times as long. This would be the case if Europa Clipper launches on the Space Launch System and uses a direct trajectory to Jupiter. If another launch vehicle and Earth or other gravity assists are used, the two missions would arrive at more similar times.
The Europa Clipper orbiter will be built and manufactured with a scientific payload of nine instruments, contributed by the JPL, APL, Southwest Research Institute, University of Texas at Austin, Arizona State University and University of Colorado Boulder.

History

Europa has been identified as one of the locations in the Solar System that could possibly harbor microbial extraterrestrial life. Immediately following the Galileo spacecraft's discoveries, JPL conducted preliminary mission studies that envisioned a capable spacecraft such as the Jupiter Icy Moons Orbiter, the Jupiter Europa Orbiter, an orbiter, and a multi-flyby spacecraft: Europa Clipper.
Europa Clipper is still in its planning phase and early development, but the approximate cost estimate rose from $2 billion in 2013, to $4.25 billion in 2020. The mission is a joint project between the Johns Hopkins University's Applied Physics Laboratory, and the Jet Propulsion Laboratory. The mission's name is a reference to the lightweight clipper ships of the 19th century that routinely plied trade routes around the world. The moniker was chosen because the spacecraft will "sail" past Europa, as frequently as every two weeks.
In March 2013, $75 million were authorized to expand on the formulation of mission activities, mature the proposed science goals, and fund preliminary instrument development, as suggested in 2011 by the Planetary Science Decadal Survey. In May 2014, a House bill substantially increased the Europa Clipper funding budget for the 2014 fiscal year from $15 million to $100 million to be applied to pre-formulation work.
Following the 2014 election cycle, bipartisan support was pledged to continue funding for the Europa Multiple Flyby Mission project. The executive branch has also granted $30 million for preliminary studies.
In April 2015, NASA offered to the European Space Agency to submit concepts for an additional probe to fly together with the Europa Clipper spacecraft, with a mass limit of 250 kg maximum. It could be a simple probe, an impactor, or a lander. An internal assessment at ESA is underway to see if there is interest and funds available, opening a collaboration scheme similar to the very successful Cassini-Huygens approach.
In May 2015, NASA chose nine instruments that would fly on board the orbiter. They will cost about $110 million over the next three years. In June 2015, NASA announced its approval of the mission concept, allowing the orbiter to move to its formulation stage, and in January 2016 it approved a lander as well. In May 2016, the Ocean Worlds Exploration Program was approved, of which the Europa mission is part. In February 2017, the mission moved from Phase A to Phase B.
On 18 July 2017, the House Space Subcommittee held hearings on the Europa Clipper as a scheduled Large Strategic Science Missions class, and to discuss a possible follow up mission simply known as the Europa Lander.
Phase B continued into 2019. In addition, subsystem vendors were selected, as well as prototype hardware elements for the science instruments. Spacecraft sub-assemblies will be built and tested as well.
On 19 August 2019, the Europa Clipper was confirmed to move on to Phase C: final design and fabrication. Phase D will include assembly, testing, and launch.

Objectives

The goals of Europa Clipper are to explore Europa, investigate its habitability and aid in the selection of a landing site for the future Europa Lander. This exploration is focused on understanding the three main requirements for life: liquid water, chemistry, and energy. Specifically, the objectives are to study:
Because Europa lies well within the harsh radiation fields surrounding Jupiter, even a radiation-hardened spacecraft in near orbit would be functional for just a few months. Most instruments can gather data far faster than the communications system can transmit it to Earth because there are a limited number of antennas available on Earth to receive the scientific data. Therefore, another key limiting factor on science for a Europa orbiter is the time available to return data to Earth. In contrast, the amount of time during which the instruments can make close-up observations is less important.
Studies by scientists from the Jet Propulsion Laboratory show that by performing several flybys with many months to return data, the Europa Clipper concept will enable a $2bn mission to conduct the most crucial measurements of the cancelled $4.3bn Jupiter Europa Orbiter concept. Between each of the flybys, the spacecraft will have seven to ten days to transmit data stored during each brief encounter. That will let the spacecraft have up to a year of time to transmit its data compared to just 30 days for an orbiter. The result will be almost three times as much data returned to Earth, while reducing exposure to radiation. The Europa Clipper will not orbit Europa, but instead orbit Jupiter and conduct 44 flybys of Europa at altitudes from each during its 3.5-year mission. A key feature of the mission concept is that the Clipper would use gravity assists from Europa, Ganymede and Callisto to change its trajectory, allowing the spacecraft to return
to a different close approach point with each flyby. Each flyby would cover a different sector of Europa in order to achieve a medium-quality global topographic survey, including ice thickness. The Europa Clipper could conceivably flyby at low altitude through the plumes of water vapor erupting from the moon's ice crust, thus sampling its subsurface ocean without having to land on the surface and drill through the ice.
The Europa Clipper will inherit tested technology of the Galileo and Juno Jupiter orbiters with regards to radiation protection. Shielding will be provided by 150 kilograms of titanium. To maximize its effectiveness, the electronics will be nested in the core of the spacecraft for additional radiation protection.

Design and construction

Power

Both radioisotope thermoelectric generator and photovoltaic power sources were assessed to power the orbiter. Although solar power is only 4% as intense at Jupiter as it is in Earth's orbit, powering a Jupiter orbital spacecraft by solar panels was demonstrated by the Juno mission. The alternative to solar panels was a multi-mission radioisotope thermoelectric generator, fueled with plutonium-238. The power source has already been demonstrated in the Mars Science Laboratory mission. Five units were available, with one reserved for the Mars 2020 rover mission and another as backup. In September 2013, it was decided that the solar array was the less expensive option to power the spacecraft, and on 3 October 2014, it was announced that solar panels were chosen to power Europa Clipper. The mission's designers determined that solar was both cheaper than plutonium and practical to use on the spacecraft. Despite the increased weight of solar panels compared to plutonium-powered generators, the vehicle's mass had been projected to still be within acceptable launch limits.
Initial analysis suggest that each panel will have a surface area of and produce 150 watts continuously when pointed towards the Sun while orbiting Jupiter. While in Europa's shadow, batteries will enable the spacecraft to continue gathering data. However, ionizing radiation can damage solar panels. The Europa Clipper orbit will pass through Jupiter's intense magnetosphere, which is expected to gradually degrade the solar panels as the mission progresses. The solar panels will be provided by Airbus Defense and Space Netherlands.

Scientific payload

The Europa Clipper mission is equipped with a sophisticated suite of 9 instruments to study Europa's interior and ocean, geology, chemistry, and habitability. The electronic components will be protected from the intense radiation by a 150-kilogram titanium and aluminum shield. The spacecraft payload and trajectory are subject to change as the mission design matures. The nine science instruments for the orbiter, announced in May 2015, have an estimated total mass of and are listed below:
Instrument nameAbbr.Description and scientific objectives
Europa Thermal Emission Imaging SystemE-THEMISThe Europa Thermal Emission Imaging System will provide high spatial resolution, multi-spectral imaging of Europa in the mid infrared and far infrared bands to help detect active sites, such as potential vents erupting plumes of water into space. This instrument is derived from the Thermal Emission Imaging System on the 2001 Mars Odyssey orbiter, also developed by Philip Christensen.
  • Principal investigator: Philip Christensen, Arizona State University
Mapping Imaging Spectrometer for EuropaMISEThe Mapping Imaging Spectrometer for Europa is an imaging near infrared spectrometer to probe the surface composition of Europa, identifying and mapping the distributions of organics, salts, acid hydrates, water ice phases, and other materials. From these measurements, scientists expect to be able to relate the moon's surface composition to the habitability of its ocean. MISE is built in collaboration with the Johns Hopkins University Applied Physics Laboratory.
  • Principal investigator: Diana Blaney, Jet Propulsion Laboratory
    • Europa Imaging SystemEISThe Europa Imaging System is a visible-spectrum wide and narrow angle camera instrument that will map most of Europa at resolution, and will provide images of selected surface areas at up to 0.5 m resolution.
  • Principal investigator: Elizabeth Turtle, Applied Physics Laboratory
    • Europa Ultraviolet SpectrographEuropa - UVSThe Europa Ultraviolet Spectrograph instrument will be able to detect small plumes and will provide valuable data about the composition and dynamics of the moon's exosphere. Principal Investigator Kurt Retherford was part of a group that discovered plumes erupting from Europa while using the Hubble Space Telescope in the UV spectrum.
  • Principal investigator: Kurt Retherford, Southwest Research Institute
    • REASONThe is a dual-frequency ice penetrating radar instrument that is designed to characterize and sound Europa's ice crust from the near-surface to the ocean, revealing the hidden structure of Europa's ice shell and potential water pockets within. This instrument will be built by JPL.
  • Principal investigator: Donald Blankenship, University of Texas at Austin
    • Interior Characterization of Europa using MagnetometryICEMAGICEMAG was cancelled due to cost overruns. Will be replaced by a simpler magnetometer.
    Plasma Instrument for Magnetic SoundingPIMSThe Plasma Instrument for Magnetic Sounding measures the plasma surrounding Europa to characterise the magnetic fields generated by plasma currents. These plasma currents mask the magnetic induction response of Europa's subsurface ocean. In conjunction with a magnetometer, it is key to determining Europa's ice shell thickness, ocean depth, and salinity. PIMS will also probe the mechanisms responsible for weathering and releasing material from Europa's surface into the atmosphere and ionosphere and understanding how Europa influences its local space environment and Jupiter's magnetosphere.
  • Principal investigator: Joseph Westlake, Applied Physics Laboratory
    • Mass Spectrometer for Planetary ExplorationMASPEXThe Mass Spectrometer for Planetary Exploration will determine the composition of the surface and subsurface ocean by measuring Europa's extremely tenuous atmosphere and any surface materials ejected into space. Jack Waite, who led development of MASPEX, was also Science Team Lead of the Ion and Neutral Mass Spectrometer on Cassini spacecraft.
  • Principal investigator: Jack Waite, Southwest Research Institute
    • SUrface Dust AnalyzerSUDAThe SUrface Dust Analyzer is a mass spectrometer that will measure the composition of small solid particles ejected from Europa, providing the opportunity to directly sample the surface and potential plumes on low-altitude flybys. The instrument is capable of identifying traces of organic and inorganic compounds in the ice of ejecta.
  • Principal investigator: Sascha Kempf, University of Colorado Boulder

    • Possible secondary elements

    The Europa Clipper mission considers an extra mass of about 250 kg to carry an additional flight element. About a dozen proposals have been suggested, a few of which are described next:
    ;Nanosatellites
    is a 10 cm cube.
    Since the Europa Clipper mission may not be able to easily modify its orbital trajectory or altitude to fly through the episodic water plumes, scientists and engineers working on the mission have investigated deploying from the spacecraft several miniaturized satellites of the CubeSat format, possibly driven by ion thrusters, to fly through the plumes and assess the habitability of Europa's internal ocean. Some early proposals include Mini-MAGGIE, DARCSIDE, and Sylph. The Europa Clipper would relay signals from the nanosatellites back to Earth. With propulsion, some nanosatellites could also be capable of entering orbit around Europa.
    ;Secondary orbiters
    ;* Biosignature Explorer for Europa
    ;* Europa Tomography Probe
    ;Impactor probes
    ;Flyby sample return
    The Europa Life Signature Assayer concept by the University of Colorado consists of a probe that is flown as a secondary payload. ELSA would use a small impactor to create a plume of subsurface particles and catapult them to altitudes where it would be able to pass through to collect samples and analyze them on board. A variation of this concept is the 1996 Ice Clipper, which involves a 10 kg impactor that would be jettisoned from the main spacecraft to impact Europa, thereby creating a debris cloud in nearby space about 100 km altitude, subsequently sampled by a small spacecraft on a close flyby and use Europa's gravitational force for a free return trajectory. The collection mechanism is tentatively considered to be Aerogel.

    Add-on lander history

    An early Europa Clipper concept called for including a stationary lander about 1 meter in diameter, perhaps about with a maximum of for instruments plus propellant. Suggested instruments were a mass spectrometer and a Raman spectrometer to determine the chemistry of the surface. The lander was proposed to be delivered to Europa by the main spacecraft and possibly require the sky crane system for a high precision, soft landing near an active crevasse. The lander would operate about 10 days on the surface using battery power. In January 2016, it was determined that including the additional mass of a lander and detachable probes, meant the Europa Clipper may need be launched with NASA's Space Launch System heavy lift launch vehicle that could arrive at Jupiter on a direct trajectory in less than three years.
    The Europa Clipper would take about three years to image 95% of the surface of Europa at about 50 meters per pixel. With this data, scientists could then find a suitable landing site. By one estimate, including a lander could add as much as $1 billion to the mission's cost.
    ;Separate launch
    It was determined in February 2017 that designing a system capable of landing on a surface about which very little is known, is too much risk, and that the Europa Clipper will lay the foundation for a future landing mission by performing detailed reconnaissance first. This led to a stand-alone mission proposal in 2017: the Europa Lander. The NASA Europa Lander, if funded, would be launched separately in 2025 to complement the studies by the Europa Clipper mission. If funded, approximately 10 proposals may be selected to proceed into a competitive process with a $1.5 million budget per investigation. The President's 2018 and 2019 federal budget proposals do not fund the Europa Lander, but it did assign $195 million for concept studies.

    Launch and trajectory

    In the baseline mission profile, Europa Clipper is planned to be carried aboard NASA's Space Launch System heavy-lift launch vehicle, on a direct trajectory to Jupiter in less than three years., it should be ready for launch by 2024. Congress has mandated that Europa Clipper be launched on SLS, but NASA has requested that other vehicles be allowed to launch the spacecraft due to a foreseen lack of available SLS vehicles.
    Since the development and readiness of the SLS may not match the mission's timing, an alternative trajectory profile would use a commercial rocket such as Delta IV Heavy or Falcon Heavy, with a longer 6-year cruise time involving gravity assist maneuvers at Venus, Earth and Earth again. Another option is to launch on a Falcon Heavy and use a Star 48B solid rocket or a Castor 30B solid rocket as a kick stage, This would require only one gravity assist, with Earth, and would shorten the cruise phase. Launch windows are available from 2022 to 2025.