3. INVESTIGATION APPROACH

    3.1. Observational Requirements
    3.2. Mission Constraints
    3.3. Methods and Procedures/Anticipated Results
      3.3.1 Retrievals of Dust, Cloud, and Ozone Opacities
        3.3.1.1. Cloud Opacities
        3.3.1.2. Dust Opacities
        3.3.1.3. Ozone Opacities
      3.3.2. Wide Angle Studies
      3.3.3. Medium Angle Studies

3.1. Observational Requirements

Based on the science studies most likely to benefit from observations from the Mars Surveyor '98 Orbiter, science observational requirements can be established:

1. Repetitious, global coverage at scales between 1 and 10 km/pixel.

2. Multispectral capability to distinguish between cloud compositions (water, CO2 ice and dust).

3. UV imaging capability at limb and nadir to observe ozone as a measure both of atmospheric photochemistry and as a surrogate for water vapor concentration.

4. Medium resolution (10's meters/pixel) observations of selected areas, multispectrally, to study specific processes and/or phenomena at local scale (frost formation and evolution in the polar regions, local dust storm formation and movement, etc.).

These requirements translate to technical requirements for the MARCI cameras (Table 2).

Table 2: Science Requirements for MARCI


    Requirement      Wide Angle Camera   Medium Angle Camera

    Resolution       1-10 km/pixel       50 m/pixel                 
                     nadir, < 7 km limb                             

   Field of View     limb to limb        nadir, repeat coverage     
                                         in timescale << seasonal   

   Spectral Bands    ~ 5, including      5-10 bands, 450-1000 nm    
                     250 and 330 nm                                 

   MTF @ Nyquist     0.10                0.10

        SNR          >= 20:1, for Albedo = 0.10, at aphelion,          
                     with illumination angle (i) <= 75° (sun        
                     elevation >= 15° )                              

    Photometry       5% relative (within an image), 10% absolute       
                     (between images)                                  

Table 3: Mars Surveyor '98 Orbiter Mission Constraints for MARCI


Data Volume          Varies by over two orders of magnitude         
                     during mission, from 21.5 Mb/day to 3,375      
                     Mb/day                                         

Computational        2-18 MIPS, depending on available power;       

Resources            fraction of 500 Kb program memory, 40 Kb       
                     sequence                                       

Power                18 W available; 28 V unregulated               

Mass                 <= 3 Kg                                        

Communications       RS-422, 1 Mb/sec                               

Thermal              To be determined in conjunction with S/C       

Other Physical       As described in PIP                            
Environments                                                        
(Vibration, Shock,                                                  
Acoustics,                                                          
Acceleration)                                                       

Attitude & Control   Control: 25 mrad/axis
(3 sigma)            Knowledge: 25 mrad/axis
                     Stability: 1.5 mrad/1 sec, 3 mrad/12 sec

Radiation            Total dose:  7 Krads/yr at outer surface of    
                     instrument from external sources during        
                     cruise (assuming 0.1 inch Al shielding)        

3.2. Mission Constraints

In addition to the observational requirements, mission parameters also constrain instrument design. Some of these constraints are operational (e.g., the location, altitude, and attitude of the spacecraft as a function of time), while others are environmental (e.g., the thermal and ionizing radiation environment). Additionally, there are the constraints imposed on resources, including mass, power, and downlink data rate. Some of the values given in the PIP and summarized in Table 3 were taken as guidelines for the various constrained parameters.

3.3. Methods and Procedures/Anticipated Results

As noted earlier, a unique opportunity exists for using UV imaging to extract important quantitative information about atmospheric constituents. This section begins with a more detailed description of the intent of this particular aspect of this investigation and techniques to be used, before outlining the broad aspects of other imaging methods and expected results.

3.3.1 Retrievals of Dust, Cloud, and Ozone Opacities

The use of combined visible/ultraviolet imaging of Mars has been demonstrated from HST observations to provide strong constraints on dust, cloud, and ozone opacities in the Mars atmosphere (James et al., 1994). The key strengths of the 230-330 nm observations are the low albedos of the Mars surface (0.01-0.02; Hord et al., 1974) relative to atmospheric Rayleigh scattering, the resulting sensitivities to small dust and cloud opacities (< 0.05, see below) in nadir as well as limb viewing, and the ability to observe the Hartley band absorption of atmospheric ozone as a proxy for Mars atmospheric water vapor (Barth et al., 1973; James et al., 1994). The combination of MARCI visible and UV limb imaging discriminates dust from cloud aerosols, and provides vertical profiling of cloud, dust, and ozone opacities over altitudes of 0-50 km. Each of these capabilities is described below in terms of specific measurement/retrieval goals and methods for the MARCI experiment.

3.3.1.1. Cloud Opacities

Clouds appear very bright against the dark surface of Mars at violet and UV wavelengths. Figure 3 presents north-south cross sections of 230 and 336 nm brightnesses from December 1990 HST images of Mars (from James et al, 1994), in which the north polar hood (tau ~0.2) appears roughly 3 times brighter than the surface plus Rayleigh atmospheric reflectances. Also note the violet image projection of the low latitude cloud belt observed around Mars aphelion in 1995, as presented in Figure 4 (from Clancy et al., 1995). Neither of these large-scale cloud systems are very apparent in green and red light imaging, and the spatial variations of such diffuse clouds are not easily separated from the strong spatial variations of surface albedos at these longer wavelengths. The very low surface albedos in the UV and the distinct Rayleigh scattering component of the UV reflectance (note the presence of the enhanced Rayleigh scattering over Hellas Basin, pixels 125-175 in the 230 nm cross section of Figure 3) provide optimum mapping of cloud opacities as small as 0.02, from nadir viewing. In limb viewing geometry, MARCI should obtain the vertical distribution of clouds with ~4 km vertical resolution to altitudes as high as 70 km, depending on the cloud optical depths and vertical distributions. The combined UV/visible imaging will also distinguish dust and cloud aerosol scattering, as described below.


Figure 3: UV reflectance and Column Density of O3


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Figure 4: HST image of Mars at 410 nm

3.3.1.2. Dust Opacities

Owing to the low UV single scattering albedo of the dust particles (~0.4-0.6, Pang and Ajello, 1977) and the substantial UV Rayleigh scattering optical depths of a 6 mbar CO2 atmosphere (taunadir= 0.03 at 336 nm), dust loading leads to significant decreases in the UV brightness of the Mars atmosphere. This effect is most strongly exhibited on the atmospheric limb of Mars, where the optical columns of molecular scattering and dust absorption are enhanced. Figure 5 shows an equatorial cross section of the observed 336 nm limb radiance of the Mars atmosphere as observed by HST on December 13, 1990 (from James et al., 1994). Multiple scattering radiative transfer calculations are presented for two cases incorporating simple surface and atmospheric molecular scattering (solid line) and surface and atmospheric molecular scattering with a dust opacity of 0.2 (dashed line). Note that ozone absorption is not present at 336 nm (see below). These model calculations only extend to emission angles of 65°, and have been normalized to the observed radiances at the Mars disk center, to reflect the uncertain calibration of the WF/PC I UV imaging (James et al., 1994). At visible wavelengths, dust appears as distinct atmospheric limb brightening rather than absorption, because the dust single scattering albedo is high (~0.9) and Rayleigh scattering is minuscule (e.g., Clancy and Lee, 1991). As a consequence, strong discriminations of dust versus cloud aerosols are provided from the combined visible/UV limb observations. Given the spatial resolution of the MARCI limb measurements (~ 4 km, versus ~50 km for the HST images, e.g. see cover), sensitivities to minimum dust column opacities of 0.05, as well as the 0-50 km profile of dust opacity during high dust loading (tau >1, with approximately 10 km vertical resolution) should be obtained. However, dust loading in the lower 10 km of the atmosphere must be derived at non-limb tangent viewing owing to the > unity dust/Rayleigh limb optical depths for the lower scale height.


Figure 5: UV Reflectance and the Effects of Dust

3.3.1.3. Ozone Opacities

High latitude determinations of ozone columns are presented in Figure 3, where the dashed line curve of 230 nm brightness models the effect of Hartley band ozone absorption on the observed 230 nm brightnesses. MARCI will use a wavelength of 250 nm, which is more optimally placed within the Hartley ozone band. Since ozone absorption is negligible at 330 nm, the determination of Mars atmospheric ozone opacities will be obtained from the ratio of the observed 255 and 330 nm radiances. The observed airmass dependence of the 250 to 330 nm brightness ratio leads to a determination of the ozone opacity that is fairly insensitive to calibration and modeling uncertainties. The variation of this ratio on the atmospheric limb provides for ~one scale height (10 km) resolved profiles of the ozone absorption over the 0-40 km altitude range, although ozone retrievals in the lowest scale height must rely on viewing airmasses below the limb tangent (path lengths of 2-4). MARCI will have the sensitivity to measure ozone columns of 1 µ m-atm, sufficient to observe the smaller ozone abundances at low latitudes (~2 µ m-atm, Espenak et al., 1991) as well as the larger high latitude ozone levels (e.g., Figure 3). Mars atmospheric ozone is photochemically tied to atmospheric water vapor, such that it varies inversely with atmospheric water (e.g., Nair et al., 1994). Hence, the observed variations of ozone provide key information on the seasonal and spatial variations of Mars atmospheric water. Furthermore, recent observations of low altitude water vapor saturation around Mars aphelion (Clancy et al., 1995a) have been correlated with large increases in atmospheric ozone, from HST 1995 Faint Object Spectrograph observations (Clancy et al., 1995b). These key aphelion changes in Mars ozone behavior can be measured in much greater detail by MARCI.


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Figure 6: "Worst Case" Daily Global Map Resolution (bottom) compared to "Best" HST (top)

3.3.2. Wide Angle Studies

The primary dataset for study of atmospheric processes on Mars will be provided by the wide angle camera. Regularly repeated global maps produced by the low resolution camera will also be the primary data set used for monitoring dust storm activity and variable features. Frequent multispectral observations will enhance the science return in all areas of atmospheric and surface/atmospheric investigations. Wide angle data will be used to characterize the dominant zonal wave numbers, phase speeds, and meridional structure of baroclinic systems in both hemispheres by direct measurement of their location on a daily basis. Likewise, it will be possible to provide daily estimates of wind speed and direction at locations where clouds and aerosols form, by tracking their motion on a daily basis in mid- and equatorial latitudes, and on a hourly basis for latitudes poleward of 60° . Opacity and cloud data should reveal areas that are persistently dustier and cloudier than others, as predicted by GCMs. These models also predict that the martian Hadley cell is much more longitudinally variable than previously thought. In particular, the meridional flow in the lower branch of the Hadley cell should be channeled into narrow currents along the eastward flanks of major topographic rises such as Tharsis. Again, this is a model prediction that will be tested using wide angle data.

3.3.3. Medium Angle Studies

The medium angle camera provides the opportunity to examine specific areas and phenomena at higher spatial and spectral resolution. It will be used to provide data on the local structure within dust clouds and, if a planet encircling storm should occur, within that. For dust storm studies, regions in which dust storms are frequently observed in the historical record (such as Solis Planum, Isidis Planitia/Syrtis Major, Hellas Planitia, and Hellespontis) or where MGS or MARCI have observed storm activity will be targeted. Repeated imaging at several seasons will be acquired both to establish a baseline for future changes, and to look for changes since previous missions observed these areas.

The medium angle camera will be used to study particular clouds, such as the W cloud system in Tharsis/Valles Marineris and the spiral storms (Hunt and James, 1979), in order to understand their structure and evolution. The residual polar caps will be monitored in order to study the fractional coverage of the surface and to estimate the thickness of the frost deposits. In addition, these medium resolution images will enable detailed comparisons with Viking, Mariner 9, and MGS images at identical seasonal dates in order to address the issues of interannual differences and evolution of the residual caps. Various regions near the edge of the seasonal caps will be observed on consecutive days at medium resolution in order to observe the sublimation (and condensation) processes as the edge of the cap passes the particular point, and regions in the cap interior will be observed to test the hypothesis that albedo variations within the cap are due to fractional coverage of the surface. Specific locations within the cap such as the Mountains of Mitchel, craters with frost streaks, and craters with dunes within them will be studied using data from the medium resolution camera in order to correlate the special behavior of these regions with local topography and surface properties.

Selected regions poleward of 75° N and 70° S will be photographed both with single and multiple strips of 4 color coverage. In other areas, morphological mapping with one color will suffice. Coverage will occasionally be repeated of certain areas, such as after initial loss of frost. Much of the polar investigation will be performed in the absence of seasonal frost, which limits the higher latitude images to short seasons.

For studies of variable features, swaths through a number of regions of noted variability will be acquired. Candidate locations include swaths through the center and east and west margins of Syrtis Major Planitia, Cerberus, Solis Planum, Oxia Palus, and the dark collars surrounding the Tharsis volcanoes. Multi-season coverage will be necessary to relate observed albedo variability to any variations in the surface morphology.

To study mid- and low latitude eolian materials, imaging strips taken through at least 4 filters and up to 200 km long are needed at several dozen locales. Multi season imaging of half of these areas will be used to establish the relation of current activity to the underlying deposit characteristics, and to insure that data include periods of minimal dust covering and atmospheric interference. Similar strips of non-eolian morphology will also be acquired.


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