Page 242 - NAVAL SCIENCE 3 TEXTBOOK
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248      NAVAL SKILLS


         Guided Missile Trajectories                               lvlissile  trajectories  include many shapes  or types  of CllIyes.
                                                                The exact nature of the curve is  determined by the type of guid-
         The Imjee/or)' of a missile is its  p<lth  ti'OIll  lauIlch  to  impact or
                                                                allce and  the  nature of the control system  used,  A hyperbolic tra-
         destruct. There arc  two  basic  types of missile  tnljectories:  ballis-
                                                                jectory, for  instance, will  occur with  a  missile lIsing a  hyperbolic
         tic  and  aerodynamic. A number of other  trajectories  are  named
                                                                guidallCe system. The missile ",ill first climb to the desired altitude,
         according to the p<lth tr~l\'eled. such as glide, pO\\'ered flight, termi-
                                                                then follow an arc of a hyperbola before diving on its target.
         nal, and standard, among others.
                                                                   A pursuit curve  is followed  by most homing and  beam  rider
            In a ballistic trajectory, the missile is acted upon only by gr,w-
                                                                missiles. At an)' given instant, the missile is pointed directly toward
         it)' ilnd aerodynamic drag after the propulsive force  is terminated.
                                                                the target.  If sllch  a missile  pursues a crossing target, the  missile
         Gun projectiles have a purely ballistic trajectory. The major part of
                                                                must follow a curved  trajcctoq'.  In  some cases,  the extreme cur-
         the trajectory of ballistic missiles  is  of this  type.  An  C1eroriY'/{/lI/ic
                                                                vature required by the pursuit course as  the missile nears the tar-
         tmjectory is one in which aerodynamic forces (thrust, drag, weight,
                                                                get may be too sharp lor the missile to follow. In this case, <l  highly
         and lift) are used to Illaintain the flight  path.
                                                                maneu\'erablc aircraft  with  <l  proficient pilot  may be sllccessful  in
                                                                LINE  OF  SIGHT  (LOS,,>




                                                                     ,
                    TARGET  FLIGHT  P
                                      \                              r  o
                                       \                            J"             SHARP
                                        \                                          CURVATURE  CAUSES
                                         \              <0                         HIGH
                                          \             '"                         ACCELERATIONS
                                                        '\
                                                           \
                                                            \
                                                             \
                                                             \
                                                              \
                                                   \           \
                                                     \
                                                                \
                                                      \          \
                                                       \
                                                         \        \
                                                          \        \
                                                            ,
                                                           \
                                                                    \   \_----MISSILE  FLIGHT PATH
                                                             \        \
                                                               \
                                                                \
                                                                 \
                                                                 \
                                                                   \
                                                                    \        ",
                                                                     \
                                                                      \    \
                                                                        \
                                                                         \
                                                                           \
                                                                            \
                                                                             \
                                                                              \
                                                                                \
                                                                                 \







                      The  pursuit homing or zero-bearing missile intercept path  followed  by most homing and  beam  rider missiles.
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