Page 62 - Radar Technology Encyclopedia
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52    ATMOSPHERE                                                                   atmospheric emission



                                                           Table A9
                              Comparison of Some Radar Astronomy Installations (from Evans and Hagfors, 1968)
               Institute     Location   Frequency  Antenna   Gain   Aper-  Average   Peak   Pulse   PRF      T s
                                          (MHz)    diameter  (dB)   ture    power   power  length   (Hz)     (K)
                                                                      2
                                                     (ft)           (m )    (kW)    (kW)    (m s)
            Cornell Univ.   Arecibo, PR    430      1,000    57.0  20,000    150    2,500   0.1–   Variable  400
                                                                                             10
            Crimean Deep   Crimea, USSR    700      8 ´ 50 *  46.8  700      60       60    CW      CW       100
            Space Tracking
            Station
            California Inst.   Goldstone   2,388      85     54.2   355      100     100    CW      CW       30
            of Tech, JPL     Lake, CA
            Manchester     Jodrell Bank,   408       250     47.3   2,300    1.5     1.5     30      1      1,200
            Univ.             U.K.
            Massachusetts   Westford, MA   1,295      84     46.5   190      150     150    0.1–4  Variable  80
            Inst. of Tech.   (Millstone)
            Lincoln Lab
            Massachusetts   Massachusetts   8,000    120     66.8   525      100     100    CW      CW       100
            Inst. of Tech.   (Haystack)
            Lincoln Lab
            *This antenna consists of an array of eight 16-m parabolas fixed to a frame.

           extends from the earth's surface to 600 to 1,500 km in space,  ically reject weather clutter through the use of coherent wave-
           but more than 75% of the atmosphere lies below about 10.7  forms and processing,  which discriminate moving targets
           km (35 kft) and it  is in this region where  most of  earth's  from clutter on the basis of a measurement of their doppler
           weather effects occur. The atmosphere can affect radar opera-  frequency.  The capability  of a radar to reject  atmospheric
           tion in several important ways: (1) by absorbing energy from  clutter is defined by the radar’s clutter attenuation factor, or
           the radar wave (attenuation), (2) by bending the path of the  clutter improvement factor. (See CLUTTER). PCH
           radar energy (refraction), (3) by contributing interfering sig-
                                                                Atmospheric ducting is a mode of anomalous propagation in
           nals (clutter) due to the radar energy reflecting off rain (back-
                                                                which specific atmospheric conditions create a confined con-
           scatter) and other forms of precipitation, and (4) by adding
                                                                duit, or  duct, that follows  the  earth’s curvature. At  certain
           noise to the radar receiver. The magnitude of these effects is
                                                                radar frequencies, the duct acts like a waveguide, permitting
           frequency (hence wavelength) dependent, and therefore the
                                                                propagation of  the radar  wave beyond that  expected under
           atmosphere is a major consideration at the design stage of a
                                                                normal atmospheric conditions and enabling the radar  to
           radar, in the selection of operational frequency. See PROPA-
                                                                detect targets beyond the radar horizon. Ducts occur as a con-
           GATION;  ATTENUATION;  atmospheric refraction;
                                                                sequence of an atmospheric inversion of either temperature,
           NOISE, antenna. PCH
                                                                humidity, or both, in which the gradient of the index of refrac-
           Ref.: Van Nostrand (1983); Blake (1982), p. 177      tion, dn/dh, increases at a rapid rate with altitude. The large
                                                                decrease in the index of refraction with altitude causes the
           Atmospheric absorption [attenuation] is the loss of radar
                                                                energy trapped within the duct formed at low altitude to prop-
           energy due to absorption in the propagation medium (air,
                                                                agate along the earth’s curvature. Ducts near the ground or
           clouds, precipitation, and the ionosphere). See  ATTENUA-
                                                                sea surface are more common than elevated ducts, supporting
           TION; LOSS, atmospheric.
                                                                only certain modes of propagation and are usually not deep in
           Atmospheric backscatter  from clouds and precipitation in  the vertical dimension. For these reasons and others, extended
           the form of rain, hail, or snow may be considered an  propagation by atmospheric ducting is more likely to be expe-
           unwanted source of interference, or clutter, to radars whose  rienced by horizon-oriented surface radars operating at the
           mission is to detect targets other than the weather itself. Rain  higher microwave frequencies (UHF and above). PCH
           clutter is especially important in that, on a global basis, it  Ref.: IEEE (1993), p. 392; Skolnik (1980), pp. 450–456.
           occurs most often, can be extended over large areas, and falls
                                                                Atmospheric emission. By virtue of its properties as a radia-
           at high rates. The magnitude of the precipitation clutter signal
                                                                tion-absorbing medium, and in accordance with the law of the
           as seen by a radar (i.e., its radar cross section), depends on
                                                           2
           several factors, including the volume clutter reflectivity (m /  conservation of energy and Boltzmann’s black-body radiation
             3
           m ) of the precipitation (a function of  the rain rate);  the  theory, the  atmosphere must  radiate  the same amount  of
                                                                energy as it absorbs for the system to be in the state of ther-
           dimensions of the radar resolution cell (DR ´ q´ q ); and
                                                      El
                                                 Az
                                                                                 a
           the number of ambiguities in the radar waveform. Radars typ-  mal equilibrium. If T  is the ambient temperature of the atmo-
                                                                sphere, the atmospheric absorption noise power available in a
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