MELOS (Mars Exploration of Life and Organism Search) is a Japaneserover mission concept under study for an engineering demonstration of precision landing, and to look for possiblebiosignatures onMars using a rover. JAXA has not published updates since 2015.
Japan's aerospace agency (JAXA) started to develop the mission concept on 2008, when MELOS stood for "Mars Explorations with Landers and Orbiters" or "Mars Exploration with Lander-Orbiter Synergy" which included several landers to be deployed simultaneously, that were to study meteorology and atmospheric gas escape.[1][2][3] The first MELOS concept would have consisted of an orbiter and up to 4 small landers; all elements would be launched together on the same rocket. The orbiter would study the atmosphere, its and interactions with thesolar wind, and image the current weather. Each of the four stationary landers would have been deployed on pre-determined landing sites and perform different measurements:[2][4]
Orbiter — Meteorology
Lander A — Surface
Lander B —Astrobiology —This lander would analyze soil near amethane vent. The proposed method is to usefluorochrome dye and a microscope to stain and scan forproteins and cellular membranes. The target sensitivity would be 10 cells / 1 g of soil (compared to 104 cells / 1 g in Earth desert). It would also detect other organicbiosignatures orbiomolecules.
Lander C — Interior
Lander D — Sample return
By 2015, MELOS was down-scaled to a rover mission for an engineering demonstration,[1] and possibly anaircraft.[1] Under the latest concept, MELOS stands for "Mars Exploration of Life and Organism Search".
As of July 2015, the concept proposal includes a robotic rover whose primary objective is an engineering demonstration for long-range roving.[5] Its secondary objective is science, specifically: meteorology, geology andastrobiology.[1] The demonstration rover would use NASA'ssky crane system for landing, and once on the surface, would deploy the MELOS rover.
The scientific objectives of the mission include:[1]
Meteorology
Basic meteorological observations, dust devil observation and dust entrainment.Payload: thermometer, anemometer, barometer. Optional instruments include: a spectroscope for methane detection, a dust particle sensor, electromagnetic & sonic wave measurement of dust, and short rangeLIDAR.
Geology
Geological description of the landing site including interior layered deposits and subsurface structure of regolith.Payload:ground penetrating radar (10-50m depth), multi-band stereo cameras (400-980 nm), VIS-NIRspectrometer (10ｰ20 nm). Optional: Geochronology Instrument (isochron dating method).
Astrobiology
Identification ofbiosignatures (current life from Mars or Earth).Payload: sample arm,fluorescence microscope (using pigments to visualize livingcells), and an optional "daughter rover" to access samples in difficult places.
The mission concept also contemplates the optional deployment of a robotic airplane as a flight technology demonstrator.[1][6] It would have a wing span of 1.2 m, mass of 2.1 kg and would be released at an altitude of 16,400 feet (5 km) during the entry and landing event. Its flight duration is estimated at 4 minutes, covering a distance of 25 km (16 mi). Its only scientific payload would be a camera.
Since the mission aims for access to a "special region", strictplanetary protection sterilization protocols must be followed to prevent forward contamination of Earth microbes to Mars.[1]
Missions are ordered by launch date. Sign† indicates failure en route or before intended mission data returned.‡ indicates use of the planet as agravity assist en route to another destination.
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