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MARS 2020

NSSDCA ID: MARS-2020
COSPAR ID: 

Description

The Mars 2020 mission involves landing a large roving vehicle on the surface of Mars to conduct mobile studies of the surface environment with particular emphasis on habitability, past life, and sample collection for future missions. The primary science objctives of Mars 2020 are to identify past environments capable of supporting microbial life, seeking signs of possible past microbial life, collecting core rock and regolith samples and caching them on the surface for future missions, and testing oxygen production from the martian atmosphere. It will also carry the Mars Helicopter, a small rotorcraft designed to fly in the tenuous martian atmosphere.

Spacecraft and Subsystems

The spacecraft has three primary major components: The cruise stage; the entry, descent, and landing system; and the rover. The cruise stage encloses the rover and landing system for the journey to Mars. and includes an aeroshell (backshell and heat shield) for initial entry into the martian atmosphere. The entry, descent, and landing system comprises a heat shield, parachute, retrorockets, and a sky crane.

The Mars 2020 rover is based on the Mars Science Laboratory Curiosity rover. it has a mass of approximately 1050 kg and measures roughly 3 meters in length, 2.7 meters in width, and 2.2 meters in height. It has six 52.5 cm diameter wheels and a 2.1 m long robotic arm. The top of the rover is the equipment deck.

Communications are via a UHF (~400 MHz), a steerable high-gain (X-band, 7-8 GHZ), and a low-gain (also X-band) antenna. The UHF antenna communicates with the Mars orbiters, the high-gain antenna is primarily for direct Earth transmission and reception, and the low-gain antenna is omnidirectional to receive signals from Earth. Power is provided by a radioisotope thermal generator using 4.8 kg of plutonium dioxide, and stored in two rechargeable lithium dioxide batteries. Mobility is provided by the six wheels in a rocker-bogie suspension, it can withstand a tilt of 45 degrees and can turn 360 degrees in place.

The rover is equipped with a number of scientific investigations, including: the Mastcam-Z camera; the WATSON camera; the MEDA environmental instrument; the RIMFAX radar imager; the PIXL x-ray fluorescence spectrometer; the SHERLOC UV Raman spectrometer; the SuperCam chemical analyzer; and the MOXIE oxygen generation experiment. MOXIE and much of the electronics for the instruments are mounted on or below the rover equipment deck. The RIMFAX antenna is mounted on the bottom rear of the rover. Mastcam-Z, and Supercam are mounted on top of the rover mast. The MEDA wind sensors, three temperature sensors, and radiation and dust sensor are on the mid- to lower mast. Two MEDA temperature sensors are mounted near the front of the rover, and a pressure sensor is on the deck. PIXL, WATSON, and SHERLOC are mounted on the end of the robotic arm.

Mission Profile

The mission launch window opens on 17 July 2020 and runs until 5 August 2020. Launch is on an Atlas V-541 from Cape Canaveral Air Force Station. After a 7 month cruise, landing will take place on 18 February 2021 in Jezero Crater on the western edge of the Isidis Planitia impact basin on Mars. The rover is planned to operate for at least one martian year (687 Earth days).

Mars Helicopter

The Mars Helicopter is an experimental technology test, the primary objective is to demonstrate that autonomous, controlled flight can be achieved in the tenuous martian atmosphere. The helicopter has a mass of roughly 1.8 kg and flies with twin counter-rotating blades which will rotate at almost 3000 rpm. The body of the helicopter has fout landing legs. Power is provided by solar panels mounted above the rotors charging lithium-ion batteries. The helicopter has a heating mechanism for night-time survival. Communications will be relayed through the rover. There are no science experiments on board, as this is strictly a proof-of-concept demonstration. The helicopter is mounted on the belly of the rover, encapsulated for protection from dust. When a suitable location for the test flights is found, the rover will drop the helicopter off and move to a safe distance to relay commands. The helicopter will then charge its batteries and conduct preliminary tests. The first flight is planned to last about 30 seconds and involves hovering at 3 meters altitude. It will make up to four more test flights, lasting as long as 90 seconds and covering distances to a few hundred meters.

Image credit: NASA/JPL

Alternate Names

    Facts in Brief

    Launch Date: 2020-07-17
    Launch Vehicle: Atlas V
    Launch Site: Cape Canaveral, United States
    Mass: 1050 kg
    Nominal Power: 110 W

    Funding Agency

    • National Aeronautics and Space Administration (United States)

    Discipline

    • Planetary Science

    Additional Information

    Questions and comments about this spacecraft can be directed to: Dr. David R. Williams

     

    Personnel

    NameRoleOriginal AffiliationE-mail
    Dr. John B. McNameeProject ManagerNASA Jet Propulsion Laboratoryjmcnamee@mailhost4.jpl.nasa.gov
    Dr. Matthew T WallaceDeputy Project ManagerNASA Jet Propulsion Laboratorymatthew.t.wallace@jpl.nasa.gov
    Dr. Mitch D SchulteProgram ScientistNASA Headquartersmitchell.d.schulte@nasa.gov
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