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Space Topics: Phoenix

Science Instruments

Robotic Arm
Both Mars Polar Lander and Mars Surveyor 2001 were equipped with robotic arms, but the one built for Phoenix is longer than these two at 2.35 meters (7 feet, 9 inches).  The arm is equipped with a digging tool that can also be used to retrieve samples.  It also carries the Robotic Arm Camera and one component of the MECA instrument.  The arm will dig to a depth of half a meter or until it reaches an impenetrable ice layer, whichever comes first.  The back of the arm's scoop is equipped with ripping tines and scrapers in order to facilitate the retrieval of a sample of ice.

Phoenix RAC
Phoenix RAC
Originally built for the Mars Surveyor 2001 lander, RAC will capture close-up views of soil and ice. The two blue-dotted panels are light sources for illuminating images captured within the trench. Credit: NASA / UA

Robotic Arm Camera
Like the Microscopic Imager on the Mars Exploration Rovers, the RAC will enable Phoenix to take close-up images of rocks, ice, and soil within reach of the robotic arm, achieving a resolution of 23 micrometers per pixel.  In order to see the soils within the trench, the RAC also carries two lighting assemblies to illuminate its view.

Phoenix SSI
Credit: NASA / UA

Surface Stereoscopic Imager (SSI)
The stereo imager is based upon the design of the Imager for Mars Pathfinder and the stereo imager that was flown aboard Mars Polar Lander, but has nearly four times better resolution at 0.25 mrad/pixel (a few percent sharper than Pancam on the Mars Exploration Rovers).  It will provide high-resolution color panoramas of the landing site and also important positioning information for the robotic arm from a viewpoint two meters off the ground.

Phoenix TEGA
Phoenix TEGA
Shown here under construction, Phoenix's TEGA instrument has eight ovens for heating samples. Credit: NASA / UA
Phoenix MECA
Phoenix MECA
Phoenix's MECA instrument has four wet chemistry "beakers" (this is one of them) that will be used to perform chemical analyses on soil samples. Credit: NASA / UA

Thermal and Evolved Gas Analyzer (TEGA)
Built to a design inherited from Mars Polar Lander, TEGA heats samples delivered by the robotic arm to 1,000ºC (1,800ºF).  The power required to maintain a constant rate of heating within the oven gives clues to the quantity and composition of volatile compounds within the sample as the heat causes them to vaporize.  The gases that are driven from the sample are sent to a mass spectrometer, which measures abundances and isotope ratios for hydrogen, oxygen, carbon, nitrogen, and heavier gases.  The mass spectrometer can detect gases with concentrations as low as 10 parts per billion.  TEGA has eight ovens; soil samples can be gathered by the arm for study by TEGA from up to eight different depths below the surface.

Microscopy, Electrochemistry, and Conductivity Analyzer (MECA)
Built for Mars Surveyor 2001, MECA is a powerful suite of soil analysis tools mounted on the lander, including an optical microscope, atomic-force microscope, wet chemistry laboratory, and a thermal and electrical conductivity probe.  The microscopes can examine up to 10 different samples.  The robotic arm delivers samples to a wheel containing 69 different substrates, including magnets, sticky spots, and bulk sampling buckets.  The optical microscope will examine soil grains on the wheel with a resolution of 4 micrometers per pixel and a field of view one by two millimeters in size; and its atomic force microscope can view selected grains at a resolution of approximately 10 nanometers.  The wet chemistry laboratory consists of four tiny cells containing a warmed solution, which can soak and stir soil samples (the water is brought from Earth).  After cycles of soaking, stirring, and measurement lasting throughout the Martian day, the instrument drops in two chemical pellets that will allow testing for carbonates, sulfates, and soil oxidants.  The chemical sensors in the wet chemistry lab measure the salt content and composition, oxidation potential, acidity, and trace mineral concentrations in the soil.  MECA is critical to the mission's objective of understanding the habitability of the Martian soil.  MECA has four wet chemistry cells, so the experiment will be performed once with a sample from the surface; once from below the surface; and once from just above an ice layer.  One MECA cell is reserved as a spare.

Phoenix MARDI
Credit: NASA / JPL / MLSS

Mars Descent Imager (MARDI)
MARDI will take pictures as Phoenix approaches for its landing, providing important geological context for Phoenix's in-situ measurements.  It has a 66-degree field of view and will capture images from about eight kilometers (five miles) elevation all the way down to the ground.

Meteorological Station (MET)
MET will allow Phoenix to act as a polar weather station, monitoring changes in water abundance, dust, temperature, and other variables throughout Phoenix's landed mission.  MET includes temperature and pressure sensors and a LIDAR instrument that is designed to measure the size and location of atmospheric dust particles.  The temperature and pressure sensors are based on heritage from the Viking landers and Mars Pathfinder.