User's Manual Part 1
Table Of Contents
- TRANSMITTAL INFORMATION
- SECTION 1 INTRODUCTION
- SECTION 2 DESCRIPTION
- SECTION 3 SYSTEM PRE-CONFIGURATION
- SECTION 4 INSTALLATION
Page 2-7
3 Mar 2017
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
Power dissipation 260 watts maximum at transmit amplifier saturation.
200 watts maximum at maximum nominal system transmit power.
167 watts typical at maximum nominal system transmit power.
Cooling Forced air, 169.8 lb/hr (77 kg/hr) at 104°F (40°C) at sea level
Operating temperature -67°F (-55°C) to 158°F (70°C)
KRFU will mute the transmit RF signal if insufficient cooling air is
supplied.
Maintenance No scheduled maintenance required
Interfaces J1 - Aircraft power input
J2 - Control interface from KANDU
J3 - RF TX to OAE
J4 - RF RX from OAE
J5 - IF TX from Modman
J6 - IF RX to Modman
Table 2-8. TMA Leading Particulars
Characteristic Specification
Length 13.70 inches (348.0 mm) maximum
Width 12.00 inches (304.8 mm), maximum reflector sweep volume
Height 13.57 inches (344.7 mm) maximum
Weight 10 pounds (4.55 kg)
Operating voltage 38.5 VDC and 24 VDC for IMU supplied by the KANDU
Power dissipation 85 watts maximum
Cooling Natural convection and radiation only
Operating temperature -67°F (-55°C) to 158°F (70°C)
Maintenance No scheduled maintenance required
Interfaces J2 - Power/control interface from KANDU
J3 - RF TX from KRFU
J4 - RF RX to KRFU
Table 2-9. FMA Leading Particulars
Characteristic Specification
Length 23.03 inches (585 mm) maximum
Width 35.72 inches (907.3 mm), maximum reflector sweep volume
Height 9.39 inches (238.51 mm) maximum
Table 2-7. KRFU Leading Particulars (Continued)
Characteristic Specification
Draft as of 31 May 2017