User's Manual Part 1

Page 2-8
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
2.2 Honeywell JetWave™ System Architecture
This section describes the Inmarsat AES system that Honeywell has implemented for the following
classes of terminal:
• Class A aftermarket satellite terminal: For use on CAT types of aircraft. This uses a FMA assembly.
The terminal can also be used in the large aircraft segment of the BRS.
• Class A OEM satellite terminal: For use on CAT types of aircraft but will be designed with
consideration given to the ARINC 791 standard.
• Class B satellite terminal: For use on BRS. This uses the compact TMA.
Refer to Figure 2-2 for the JetWave™ system block diagram.
Weight 83 pounds (37.6 kg) maximum
NOTE: The lifting fixture is 5.5 pounds (2.5 kg)
Operating voltage 38 VDC and 24 VDC for IMU supplied by the KANDU
Operating temperature -67°F (-55°C) to 158°F (70°C)
Power dissipation 135 W @ steady state
Cooling Natural convection and radiation only
Maintenance No scheduled maintenance required
Interfaces P1 - Power from KANDU
P2 - Control interface from KANDU
P3 - IMU power and control from KANDU
J4 - RF RX to KRFU
J5 - RF TX from KRFU
Table 2-10. JetWave™ Fuselage Mount Radome Leading Particulars
Characteristic Specification
Length 95.472 inches (242.99 mm) (typical)
Width 43.881 inches (1,114.58 mm) (typical)
Height 11.892 inches (302.06 mm) (typical)
Weight 53.5 pounds (24.27 kg) (typical)
Table 2-9. FMA Leading Particulars
Characteristic Specification
Draft as of 31 May 2017