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Modern space modules are susceptible to EM radiation
from both external and internal sources within the space
module. Since the EM waves for various operations are
frequently in the high-frequency domain, asymptotic raytheoretic
methods are often the most optimal choice for
deterministic EM field analysis. In this work, surface
modeling of a typical manned space module is done by
hybridizing a finite segment of right circular cylinder and
a general paraboloid of revolution (GPOR) frustum. A
transmitting source is placed inside the space module and
test rays are launched from the transmitter. The rays are
allowed to propagate inside the cavity. Unlike the
available ray-tracing package, that use numerical search
methods, a quasi-analytical ray-propagation model is
developed to obtain the ray-path details inside the cavity
which involves the ray-launching, ray-bunching, and an
adaptive cube for ray-reception.