Rate-end solution, continued
RESTRICTED
with the telescope quadrant and the cable passes
through
center
of the
quadrants, through the
over sheaves 3
right cardan gudgeon is attached to the
and 4 to num-
ber 5 sheave, which
telescope
cradle. The gear on
the #5 sheave shaft is in
with the gear sector on the M-6 and with the tele-
scope sector on the M-3.
The mirror or telescope
is then driven at an angular speed
proportional to
ground speed.
The telescope
is stabilized by the vertical
In the
computing
the rate end, there
angles generated
by the movements
of the
two quadrants formed by
The angles
are equal
and are equal
a line directly beneath the
plane to the ground at the instant of bomb release
and the line of sight to the ground at the instant
of bomb
release.
These angles are
DEF (telescope
quadrant) and GHI (rate quadrant). Each angle is
determined by the amount the racks are moved. When
the indices coincide each rack has
been translated
a distance proportional to actual range. There is
also an angle equal to DEF (telescope quadrant)
formed through the
telescope by the line of sight
and
the vertical.
if this
angle
were projected downward assum-
ing the sight is in an airplane, the angle would
subtend
actual
range distance on the ground.
The
small triangle formed within the sight has
for its legs the altitude vector and the
linear
distance the rate rack is driven in translation
as
the roller is displaced from the disc center by the
rate mechanism.
The acute angles of this triangle
are proportional and similar to the angles DEF and
GHI.
The rate quadrant is positioned at the range
angle determined by the point of synchronization.
The
angle formed by the rate quadrant,
as it is
positioned,
is the generated range angle and is
equal to the sighting angle and the dropping angle
at the instant of bomb release.
The
telescope quadrant is driven,
and at the
determined range angle the indices coincide and at
that point the angles DEF and GHI are equal. It is
important to remember that the position of the rate
quadrant will determine the dropping
angle comput-
ed by the sight.
If this angle is incorrect the
bomb will miss
the objective.
To ellminate errors
the sight
must be accurately calibrated and the
correct trail, etc., must be set into the sight.
111