User Manual Part 1

Page TC-7
16 Sep 2015
23-15-29
SYSTEM DESCRIPTION AND INSTALLATION MANUAL
JetWave™ System
© Honeywell International Inc. Do not copy without express permission of Honeywell.
LIST OF FIGURES
Figure Description Page
Figure INTRO-1. Symbols ....................................................................................................INTRO-1
Figure 1-1.Ka-Band System.............................................................................................................1-1
Figure 1-2. JetWave™ System Block Diagram ....................................................................1-8
Figure 2-1. KRFU Thermal Pads .......................................................................................2-11
Figure 2-2. TMA Installation Location ................................................................................2-14
Figure 2-3. TMA Assembly Isometric View ........................................................................2-15
Figure 2-4. KRFU and TMA Interconnect Arrangement .....................................................2-16
Figure 2-5. TMA RF TX J3 and RF RX J4 Interface Connector and Bonding Strap Locations
2-17
Figure 2-6. WR42 Waveguide to 2.92 mm Coaxial Connector Adapter ............................2-18
Figure 2-7. KRFU Bonding Strap Arrangement .................................................................2-19
Figure 2-8. View of H Plane and E Plane Bends ...............................................................2-20
Figure 2-9. FMA Install Location ........................................................................................2-26
Figure 2-10. Typical Ground Strap Arrangement for A791 Compliant Fittings ....................2-27
Figure 2-11. Aircraft Coordinate System Orientation and Fitting Layout .............................2-27
Figure 2-12. AIM Assembly Placement on Aircraft ..............................................................2-28
Figure 2-13. LAIM Assembly ................................................................................................2-29
Figure 2-14. Radome Skirt Fairing and LAIM Assembly Position on Aircraft .......................2-30
Figure 2-15. FMA Assembly ................................................................................................2-31
Figure 2-16. FMA Assembly Lifting Fixture Removal ...........................................................2-32
Figure 2-17. View of H Plane and E Plane Bends ...............................................................2-34
Figure 2-18. A791 Based AIM Assembly with FMA and KRFU Placement on Aircraft ........2-35
Figure 2-19. LAIM Assembly with FMA and KRFU Placement on Aircraft ..........................2-35
Figure 2-20. Radome Assembly Mounted on Radome Skirt Fairing (LAIM) ........................2-36
Figure 2-21. GUI Login Page ...............................................................................................2-38
Figure 2-22. GUI Calibrate Antenna Alignment Page ..........................................................2-39
Figure 2-23. GUI Antenna Alignment Calibration Page Extract ...........................................2-40
Figure 2-24.Modman Outline and Installation Drawing (Sheet 1 of 4) 2-41
Figure 2-25.APM Outline and Installation Drawing (Sheet 1 of 2) 2-49
Figure 2-26.KANDU Outline and Installation Drawing (Sheet 1 of 3) 2-53
Figure 2-27.KRFU, Conduction-Cooled 1, Outline and Installation Drawing (Sheet 1 of 3) 2-59
Figure 2-28.KRFU, Conduction-Cooled 2, Outline and Installation Drawing (Sheet 1 of 3) 2-65
Figure 2-29.KRFU, Forced Air Cooled, Outline and Installation Drawing (Sheet 1 of 3) 2-71
Figure 2-30.TMA Outline and Installation Drawing (Sheet 1 of 4) 2-77
Figure 2-31.FMA Outline and Installation Drawing (Sheet 1 of 12) 2-85