| Operator | Spanish National Research Council |
|---|---|
| Manufacturer | Spanish Astrobiology Center (CSIC-INTA) |
| Instrument type | Suite of environmental sensors |
| Function | Measure dust size, morphology, weather |
| Mission duration | 1 Mars year[1] |
| Properties | |
| Mass | 5.5 kg (12 lb) |
| Power consumption | 17 watts |
| Host spacecraft | |
| Spacecraft | Mars 2020 Perseverance rover |
| Launch date | July 30, 2020 |
| Rocket | Atlas V 541 |
| Launch site | Cape Canaveral SLC-41 |
The Mars Environmental Dynamics Analyzer (MEDA) is an instrument on board the Mars 2020 Perseverance rover that will characterize the dust size and morphology, as well as surface weather.[2][3] Specifically, the information obtained will help address future human exploration objectives, as dust sizes and shapes, daily weather report and information on the radiation and wind patterns on Mars, that are critical for proper design of in situ resource utilization systems.[2][3] MEDA is a follow-on project from REMS, of the Curiosity rover mission.[4] MEDA has an increased scope, with greater data collection on Mars dust which contributes to overall Mars program objectives and discovery goals.[4]
The instrument suite was developed and provided by the Spanish Astrobiology Center at the Spanish National Research CouncilinMadrid, Spain. On April 8, 2021, NASA reported the first MEDA weather report on Mars: for April 3–4, 2021, the high was "minus-7.6 degrees, and a low of minus-117.4 degrees ... [winds] gusting to ... 22 mph".[5]
The Principal Investigator is José Antonio Rodríguez Manfredi and the Deputy Principal Investigator is Manuel de la Torre Juarez (JPL-NASA) [6][7]
List of coinvestigators and their affiliations:[7]
| Nathan Bridges
Johns Hopkins University/Applied Physics Laboratory Laurel, Maryland |
Olga Prieto-Ballesteros
Instituto Nacional de Tecnica Aeroespacial Madrid, Spain |
Pamela Conrad
NASA Goddard Space Flight Center Greenbelt, Maryland | |||
| Miguel Ramos
Universidad de Alcala de Henares Madrid, Spain |
Javier Gomez-Elvira
Instituto Nacional de Tecnica Aeroespacial Madrid, Spain |
Alfonso Saiz-Lopez
Agencia Estatal Consejo Superior de Investigaciones Científicas Instituto de Quimica Fisica Rocasolano Madrid, Spain | |||
| Felipe Gomez-Gomez
Instituto Nacional de Tecnica Aeroespacial Madrid, Spain |
Agustin Sanchez-Lavega
Universidad del Pais Vasco UPV/EHU Bilbao, Biscay, Spain |
Ari-Matti Harri Ilmatieteen Laitos Helsinki, Finland | |||
| John SchofieldNASA Jet Propulsion Laboratory
Pasadena, California |
Mark LemmonTexas A &M College Station, Texas |
Eduardo Sebastian
Instituto Nacional de Tecnica Aeroespacial Madrid, Spain | |||
| German Martinez
University of Michigan Ann Arbor, Michigan |
Michael Smith
NASA Goddard Space Flight Center Greenbelt, Maryland |
Sara Navarro Lopez
Instituto Nacional de Tecnica Aeroespacial Madrid, Spain | |||
| Leslie Tamppari
NASA Jet Propulsion Laboratory Pasadena, California |
Claire Newman
Aeolis Research Pasadena, California | ||||
Dust dominates Mars' weather the way that water dominates Earth's weather. Martian weather cannot be predicted unless dust behavior is studied and understood in the weather context.[3][8] MEDA is a suite of environmental sensors designed to record dust optical properties and six atmospheric parameters: wind speed/direction, pressure, relative humidity, air temperature, ground temperature, and radiation (UV, visible, and IR ranges of the spectrum).[3][9]
The technology used on MEDA was inherited from the REMS package operating on the Curiosity rover and the TWINS package on InSight lander.[2] The sensors are located on the rover's mast and on the deck, front and interior of the rover's body. It records data whether the rover is active or not, at both day and night.[9] The instruments will collect data for 5 minutes every 30 minutes.[8]
| Parameter | Performance/units[3][9] |
|---|---|
| Mass | 5.5 kg (12 lb) |
| Power | Max 17 watts |
| Data return | ≈11 megabytes |
| Temperature | accuracy: 5 K resolution: 0.1 K |
| Relative humidity | accuracy of 10% in the 200-323 K range |
| Pressure | Range: 1 to 1150 Pa accuracy: 20 Pa resolution: 0.5 Pa |
| Radiation | eight upward looking photodiodes:
• 255 +/– 5 nm for the O3 |
| Wind | accuracy: 2 m/sec resolution: 0.5 m/sec |
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Science instruments on satellites and spacecraft
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