MELOS explained

MELOS
Names List:Mars Explorations with Landers and Orbiters (2008)
Mars Exploration of Life and Organism Search (2015)
Mission Type:Technology demonstrator
Operator:JAXA
Mission Duration:Nominal: 68 sols
Desired extension: 1 Mars year
Manufacturer:JAXA
Landing Mass:EDM (sky crane): 909kg (2,004lb)
Rover: 150kg (330lb)
Payload Mass:15kg (33lb)
Power:Solar panels (1.5 m²)
Battery: 720 Wh
Launch Date:2024 (proposed)
Interplanetary:
Type:rover
Arrival Date:2025
Distance:Goal: 50km (30miles)

MELOS (Mars Exploration of Life and Organism Search) is a Japanese rover mission concept under study for an engineering demonstration of precision landing, and to look for possible biosignatures on Mars using a rover. JAXA has not published updates since 2015.

History

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. 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 the solar 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:[1]

By 2015, MELOS was down-scaled to a rover mission for an engineering demonstration, and possibly an aircraft.[2] Under the latest concept, MELOS stands for "Mars Exploration of Life and Organism Search".

Rover

As of July 2015, the concept proposal includes a robotic rover whose primary objective is an engineering demonstration for long-range roving.[3] Its secondary objective is science, specifically: meteorology, geology and astrobiology.[2] The demonstration rover would use NASA's sky crane system for landing, and once on the surface, would deploy the MELOS rover.

Scientific objectives and payload

The scientific objectives of the mission include: [2]

Meteorology
Geology
Astrobiology

Aircraft

See also: Mars aircraft. The mission concept also contemplates the optional deployment of a robotic airplane as a flight technology demonstrator.[2] [4] 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 25km (16miles). Its only scientific payload would be a camera.

Proposed landing sites

The proposed landing sites will target 'wet' environments and include Valles Marineris (Melas Chasm and Juvantae Chasm), located near the confirmed recurring slope lineae, and Marte Vallis near dark slope streaks. [2]

Since the mission aims for access to a "special region", strict planetary protection sterilization protocols must be followed to prevent forward contamination of Earth microbes to Mars.[2]

See also

Notes and References

  1. MELOS: Japan's Mars Exploration Plan for 2020s. MEPAG in Lisbon, Portugal (16–17 June 2011)
  2. Current plan of the MELOS, a proposed Japanese Mars mission . MEPAG meeting 2015 . Miyamoto . Hirdy .
  3. Hatakenaka . Ryuta . Fujita . Kazuhisa . Nonomura . Taku . Takai . Takai . Preliminary Thermal Design of the Japanese Mars Rover . PDF . 45th International Conference on Environmental Systems . 12 July 2015 .
  4. A Parametric Study of Mars Airplane Concept for Science Mission on Mars. Koji . FUJITA. Hiroki . NAGAI. Akira . OYAMA. Trans. JSASS Aerospace Tech. Japan. 14. ists30. Pk_83–Pk_88. 2016. 10.2322/tastj.14.Pk_83. 2016JSAST..14.Pk83F. free.