Europa Lander (NASA)
The Europa Lander is a proposed astrobiology mission concept by NASA to Europa, an icy moon of Jupiter. If funded and developed as a Flagship mission, it would be launched in 2025 to complement the studies by the Europa Clipper orbiter mission and perform analyses on site.
The objectives of the mission are to search for biosignatures at the subsurface ≈10 cm, to characterize the composition of non-ice near-subsurface material, and determine the proximity of liquid water and recently erupted material near the lander's location.
History
NASA had previously evaluated a Europa Lander concept in 2005 with the Europa Lander Mission concept. Also, a lander was evaluated in 2012. There was continued support for Europa missions, including in 2014, when the U.S. Congress House Appropriations Committee announced a bipartisan bill that included US$80 million in funding to continue the Europa mission concept studies.The United States Congress issued a congressional directive on a Europa Lander, and NASA initiated a study in 2016, assessing and evaluating the concept. The mission concept is being supported by the Ocean Worlds Exploration Program. NASA's Planetary Science Division delivered its report in early February 2017. This was a six-month-long study by a Science Definition Team. The study assesses the science value and engineering design of a potential Europa lander mission.
Overview
The primary mission goal is detection of organic indicators of past or present life, called biosignatures. The lander was described as a logical follow-up to the Galileo orbiter and probe mission in the 1990s, for which a major result was the discovery of a large sub-surface ocean that may offer habitable aquatic conditions. Earth life can be found in essentially all locations where water is present. It follows that Europa is an excellent candidate in the search for life elsewhere in the Solar System. This subsurface water may not only be warmed by geological activity, but likely also enriched with dissolved minerals and organic compounds. Various ecosystems exist on Earth without any access to sunlight relying instead on hydrothermal vents or other sources of chemicals suitable to energy production by extremophiles. Measurements to date indicate that Europa has an ocean approximately twice the volume of Earth's oceans. This water layer below the ice may be in contact with the moon's interior allowing ready access to hydrothermal energy and chemistry. A surface mission can take advantage of the relatively young, active surface of Europa as this activity may allow deep subsurface materials to regularly relocate to the surface.Status
In 18 July 2017, the House Space Subcommittee held hearings on the Europa Clipper as a scheduled Large Strategic Science Mission, and to discuss this lander as a possible follow up. The President's 2018 and 2019 federal budget proposals do not fund the Europa Lander, but it did assign $195 million for concept studies, and research on the required science instruments.Objectives
The lander mission would have three main science objectives:- Search for biosignatures.
- Assess the habitability of Europa via in situ techniques uniquely available to a landed mission.
- Characterize the surface and subsurface properties at the scale of the lander to support future exploration of Europa.
Spacecraft
and landing. The spacecraft would consist of several modules that would be discarded at different phases of its deorbiting and landing sequence. The complete stack would be propelled by the Carrier Stage, that also features the solar panels. After orbit injection around Jupiter, the spacecraft would spend about two years adjusting its orbit and velocity before attempting to land on Europa.
In preparation to its landing, the Carrier Stage would be discarded, leaving the spacecraft stack in a configuration called Deorbit Vehicle that would decelerate and initiate the descent. The engine module for this phase, called Deorbit Stage would be discarded after the burn, leaving what is called the Powered Descent Vehicle - which comprises the lander and the sky crane system. The sky crane system would lower the lander with a tether to a soft landing with a accuracy.
The lander would feature a robotic arm with 5 degrees of freedom, that would enable it to dig out several shallow sub-surface samples at a maximum depth of and deliver them to its onboard laboratory.
Power
Once landed, the lander would operate for up to 22 days by using chemical battery power, rather than a radioisotope thermoelectric generator or solar power. The 2019 concept proposes four batteries, which would provide three times the needed energy for safety margin during its ≈22-day surface operations. The baseline is 7 days to complete its surface mission, the additional 14 days are for contingencies.Regardless of the power source, one of the limiting factors for the lifetime of the mission may be surviving radiation; the surface of Europa is estimated to experience 2.3 Mrad or 540 rem per day, whereas a typical Earth surface dose is about 0.14 rem/year. Radiation damaged the electronics of the Galileo orbiter during its mission.
Launch and trajectory
The launcher would be the Space Launch System, with a suggested launch in 2025. The SLS is proposed given the spacecraft's mass of 16.6 metric tons, including the solid propellant to place the spacecraft into orbit around Jupiter, and the sky crane landing system. One calculated trajectory would see a launch aboard SLS in 2025, Earth gravity assist in 2027, and Jupiter/Europa arrival in 2030. It would spend some time orbiting around Jupiter over the next year to maneuver for its landing on Europa. The landing would be performed two years after orbit insertion around Jupiter.Landing sites
At Europa, it would have to land on the surface, matching its velocity, but with essentially no atmosphere there is no "entry", it is just a descent and landing. The Planetary Society noted that NASA called this DDL de-orbit, descent, and landing. In 1995, astronomers using the Hubble Space Telescope discovered that Europa has a very tenuous exosphere composed of oxygen. Compared to Earth, its atmosphere is extremely tenuous, with pressure at the surface predicted to be 0.1 μPa, or 10−12 times that of the Earth.The lander would communicate directly to Earth, but the Europa Clipper, if still operational, could function as an additional communications relay for the lander. To ensure communication, there is a suggestion to include a telecomm orbiter with the lander mission.
;Surface texture
A study published in October 2018 suggests that most of Europa's surface may be covered with closely spaced ice spikes, called penitents, as tall as 15 meters. Although the imaging available from the Galileo orbiter does not have the resolution needed to confirm this, radar and thermal data are consistent with this interpretation. This supports the need to first perform high-definition reconnaissance with the Europa Clipper and ESA's Jupiter Icy Moons Explorer, both planned to launch in 2022, before planning a lander mission.
Science payload
The mission concept would require funding and further development to be launched. One of the key requirements is to operate in the radiation environment at the moon's surface. The radiation environment at Europa is extreme, so the lander may need additional protection as the Juno Radiation Vault in the Juno Jupiter orbiter. The vault helped reduce radiation exposure to vulnerable systems, especially electronics on the orbiter.NASA announced in May 2017 to the scientific community to think on possible Europa Lander instruments. The concept study reports were made available in June 2019.
NASA selected 14 potential instruments for maturation under Instrument Concepts for Europa Exploration 2 awarding approximately $2 million each for two years.
The ICEE-2 project would allow the maturation of novel instrument approaches to meet the science goals and objectives of the mission.
| Instrument | Principal investigator |
| C-LIFE: Cold-Lightweight Imagers for Europa | Shane Bryne, University of Arizona |
| ELSSIE: Europa Lander Stereo Spectral Imaging Experiment | Scott L. Murchie, Johns Hopkins University Applied Physics Laboratory |
| CORALS: Characterization of Ocean Residues and Life Signatures | Ricardo D. Arevalo, University of Maryland |
| MASPEX-ORCA: MAss Spectrometer for Planetary EXploration-ORganic Composition Analyzer | Christopher R. Glein, Southwest Research Institute |
| MOAB: Microfluidic Organic Analyzer for Biosignatures | Richard A. Mathies, University of California Berkeley |
| EMILI: Europan Molecular Indicators of Life Investigation | W. B. Brinckerhoff, Goddard Space Flight Center |
| CIRS: Compact Integrated Raman Spectrometer | James L. Lambert, Jet Propulsion Laboratory |
| ELM: Europa Luminescence Microscope | Richard Quinn, Ames Research Center |
| SIIOS: Seismometer to Investigate Ice and Ocean Structure | Samuel H. Bailey, University of Arizona |
| ESP: Europa Seismic Package | Mark P. Panning, Jet Propulsion Laboratory |
| MICA: Microfluidic Icy-World Chemistry Analyzer | Antonio J. Ricco, Ames Research Center |
| MAGNET: Radiation Tolerant Magnetometer | Mark B. Moldwin, University of Michigan, Ann Arbor |
| EMS: Europa Magnetotelluric Sounder | Robert E. Grimm, Southwest Research Institute |
| CADMES: Collaborative Acceptance and Distribution for Measuring Europan Samples System | Charles A. Malespin, Goddard Space Flight Center |