Abstract:Abstract-One goal of radar remote sensing is the extraction of terrain statistics and surface dielectric properties from backscatter data for some range of wavelengths, incidence angles, and polarizations. This paper addresses empirical approaches used to estimate terrain properties from radar data over a wider range of roughness than permitted by analytical models. Many empirical models assume, at least implicitly, that roughness parameters like rms height or correlation length are independent of the horizont… Show more
“…Nearside Maria 45 deg Incidence The mean circular polarization ratios for Mare Imbrium flows of low TiO 2 content are similar to or greater than those of rough terrestrial lava surfaces, which have a maximum CPR value of about 0.6 at 60°incidence angle (Campbell, 2009). These relatively high values are partly a result of the sensitivity of the 12.6-cm radar signal to few-centimeter scale, near-surface rocks associated with even small impact craters in the mare regolith.…”
“…Nearside Maria 45 deg Incidence The mean circular polarization ratios for Mare Imbrium flows of low TiO 2 content are similar to or greater than those of rough terrestrial lava surfaces, which have a maximum CPR value of about 0.6 at 60°incidence angle (Campbell, 2009). These relatively high values are partly a result of the sensitivity of the 12.6-cm radar signal to few-centimeter scale, near-surface rocks associated with even small impact craters in the mare regolith.…”
“…The radar images have a best spatial resolution of ∼3 km, but the echoes are sensitive to small-scale (0.1-1 m) surface roughness and to rocks larger than a few cm within the signal's penetration depth (1-3 m). Arecibo image data provide a strong constraint on surface roughness by comparison with well-calibrated observations of terrestrial-analog surfaces (e.g., Campbell 2001;2009;. Low-power returns may indicate a fine-grained mantling material, which can be further investigated by other means.…”
Section: Arecibo Roughness and Reflectivitymentioning
The selection of the Discovery Program InSight landing site took over four years from initial identification of possible areas that met engineering constraints, to downselection via targeted data from orbiters (especially Mars Reconnaissance SPAC 11214 layout: Small Condensed v.2.1 file: spac321.tex (ELE) class: spr-small-v1.2 v.2016/06/09 Prn:2016/12/02; 14:37 p. 1/91» « d o c to p i c : R e v i e w P a p e rn u m b e r i n g s t y l e : C o n t e n t O n l yr e f e r e n c e s t y l e : a p s » latitude (initially 15°S-5°N and later 3°N-5°N for solar power and thermal management of the spacecraft), ellipse size (130 km by 27 km from ballistic entry and descent), and a load bearing surface without thick deposits of dust, severely limited acceptable areas to western Elysium Planitia. Within this area, 16 prospective ellipses were identified, which lie ∼600 km north of the Mars Science Laboratory (MSL) rover. Mapping of terrains in rapidly acquired CTX images identified especially benign smooth terrain and led to the downselection to four northern ellipses. Acquisition of nearly continuous HiRISE, additional Thermal Emission Imaging System (THEMIS), and High Resolution Stereo Camera (HRSC) images, along with radar data confirmed that ellipse E9 met all landing site constraints: with slopes <15°at 84 m and 2 m length scales for radar tracking and touchdown stability, low rock abundance (<10 %) to avoid impact and spacecraft tip over, instrument deployment constraints, which included identical slope and rock abundance constraints, a radar reflective and load bearing surface, and a fragmented regolith ∼5 m thick for full penetration of the heat flow probe. Unlike other Mars landers, science objectives did not directly influence landing site selection.
AUTHOR'S PROOF
“…A double‐bounce geometry occurs when the radar wave reflects from two surfaces before returning to the receiver, thereby causing the received circular polarization state to be the same as that transmitted. Extremely rugged terrain can sometimes produce circular polarization ratios greater than one [e.g., Campbell and Campbell , 1992; Campbell , 2009]. These high CPR values cannot be caused by Bragg scattering from wavelength scale roughness [e.g., Ulaby et al , 1986] and require that a significant amount of the backscatter come from double‐bounce geometries.…”
The Mini‐RF radar on the Lunar Reconnaissance Orbiter spacecraft has revealed a great variety of crater ejecta flow and impact melt deposits, some of which were not observed in prior radar imaging. The craters Tycho and Glushko have long melt flows that exhibit variations in radar backscatter and circular polarization ratio along the flow. Comparison with optical imaging reveals that these changes are caused by features commonly seen in terrestrial lava flows, such as rafted plates, pressure ridges, and ponding. Small (<20 km) sized craters also show a large variety of deposits, including melt flows and ponds. Two craters have flow features that may be ejecta flows caused by entrained debris flowing across the surface rather than by melted rock. The circular polarization ratios (CPRs) of the impact melt flows are typically very high; even ponded areas have CPR values between 0.7 and 1.0. This high CPR suggests that deposits that appear smooth in optical imagery may be rough at centimeter‐ and decimeter‐ scales. In some places, ponds and flows are visible with no easily discernable source crater. These melt deposits may have come from oblique impacts that are capable of ejecting melted material farther downrange. They may also be associated with older, nearby craters that no longer have a radar‐bright proximal ejecta blanket. The observed morphology of the lunar crater flows has implications for similar features observed on Venus. In particular, changes in backscatter along many of the ejecta flows are probably caused by features typical of lava flows.
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