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Mars Exploration Rover Project

Engineering Constraints

NEW Engineering and Landing Constraints Nov, 2001

  • Ellipse, (revised doc) updated Jan 2001
    • Varied Ellipse in 2.5° Increments
    • MER A - Oriented 66° to 86° from 77km x 30km at 15°S to 219km x 30km at 5°N
    • MER B - Oriented 79° to 99° from 338km x 30km at 10°N to 130km x 30km at 10°S
  • Elevation
    • Entire Ellipse below 1.3 km (MOLA Geoid) for parachute
    • Atmosphere Column Density (VL1 Surface P)
    • Low altitude winds less than 20 m/s
    • TES mean T
    • GCM Variability
  • Slope
    • Slope less than 15°
    • RMS Slopes less than 6°
    • MOLA inter and intra shot slopes
  • Rock Abundance
    • Less than 1° area covered by rocks greater than 50 cm high
    • Total rock abundance less the 20° - IRTM Data (Christensen)
  • Fine Component Thermal Inertia
    • CGS Units greater than 3-4 10-3 - IRTM Data (Christensen)
    • Extreme Dust 125-170 SI
    • Same as TES low TI and high Albedo Unit A (Mellon et al.)
  • Dust
    • Must have radar reflective surface greater than 0.05
    • Load bearing surface
  • Hazard Free in MDIM
    • Smooth, flat looking in MDIM
    • Avoid bumps, hills, etc.
    • Avoid all obvious fresh craters greater than 5-10 km diameter

Engineering Constraints And Landing Site Selection

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