User Manual Part 3

Page E-3
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
NOTE:
• All zenith view (from above) angles, except for “e,” are measured from the aircraft longitudinal
axis, being 0 degrees at the stern.
• All side view angles are measured from the aircraft longitudinal axis, being 0 degrees at the
plane where the antenna emitter is located.
• Refer to ARINC Characteristic 791 Mark I Aviation Ku-band and Ka-Band Satellite Communica-
tion System, Part 1- Physical Installation and Aircraft Interfaces for Aircraft blockage map
parameters.
Blockage Angle c Angle "c" refers to the point of the wing, where an
antenna radiating at -10 degrees elevation would
find the wing’s leading edge.
Blockage Angle d Angle "d" refers to the outer, aft-most tip of the
wing (including vortex eliminators, if present).
Blockage Angle e Angle "e" provides the azimuth range of the
Vertical Tail Plane (VTP) region of blockage in its
broadest case.
Blockage Angle f Angle "f" is between the fuselage centerline and
the outer, forward-most tip of the HTP.
Blockage Angle h Angle “h” provides the Vertical Tail Plane (VTP)
region of blockage in elevation from -10 degrees
up.
Blockage Angle i Angle "i" is between the horizontal plane where
the antenna emitting point is located and upper,
forward-most part of the fuselage.
Blockage Angle k Angle "k" is the angle between the horizontal
plane where the antenna emitting point is located
and the aft-most tip of the HTP.
Blockage Angle m Angle "m" is between the horizontal plane where
the antenna emitting point is located and the HTP
leading edge root (forward-most joint to fuselage).
Blockage Angle p Angle "p" is from the emitter point to upper,
aft-most wing tip (including vortex eliminators, if
present).