USS Cape St.George fires a tomahawk missile. Surface-ship-launched.
Section 1 : Document Organization
Section 2 : Tomahawk Weapon System
Section 3 : Tomahawk Cruise Missile
Section 4 : Torpedo Tube Launch Configuration
Section 5 : Capsule Launching System
Section 6 : Vertical Launching System Configuration
Forward :
This document consists of four volumes which provide information, data, and procedures for
operations and support of the Tomahawk Weapon System (TWS).
a. Volume 1. Tomahawk Cruise Missile System Description
This volume presents information pertinent to the submarine and surface launch Tomahawk
Weapon System (TWS) to include physical and functional descriptions of system components,
safety and security considerations, and operations aboard platforms employing TWS.
b. Volume 2. Tomahawk cruise Missile General Handling Procedures
Procedural Guides (PGs), Operations Procedures (OPs) and
Standard Inspection Procedures (SIP) to permit afloat and ashore activities to perform receipt,
handling, inspection, transfer, and reconfiguration processes for Tomahawk Cruise Missile
(TCM) configurations.
c. Volume 3. Tomahawk Cruise Missile Maintenance Procedures
Repairs Parts Breakdown
d. Volume 4. Tomahawk Cruise Missile UGM Warhead Installation/Removal and Air
Vehicle Maintenance
Handle and prepare UGM 109A All-Up-Rounds for installation or removal of the warhead.
Section 1. Document Organization
1.1 Scope
The document presents information pertinent to the submarine-launched and
surface-ship-launch Tomahawk Weapon System (TWS) to include physical and functional of the
weapon system.
1.1.1 Chapter 1.
Physical descriptions of weapon systems.
1.1.2 Chapter 2.
Security and safety requirements.
1.1.3 Chapter 3.
Functional description of TWS components and interface between the TCM and its launch
platforms.
1.1.4 Chapter 4.
Tomahawk Weapon System operations aboard launch platforms to include a description of the
launch platform and on board equipment used to land, store and launch
Tomahawk Cruise Missile.
1.2 Tomahawk Weapon System Description.
1.3 Mission
With the capability to use surface and sub-surface platforms to employ, either in independently
or in coordination with other strike capabilities, highly accurate, all-weather
Tomahawk Cruise Missile, armed with a variety of highly destructive payloads, against land
targets at stand-off ranges.
1.4 All-Up-Round
Horizontal Submarine Launch
Vertical Submarine Launch
Surface Launch
1.4.1 Tactical AUR
Used for land-attack mission to strike high-value or heavily defended targets.
A rocket motor to boost it to specified altitude after launch.
A sustaining engine for cruising to the target.
Wings and fins to affect course changes.
A guidance section and an explosive warhead.
1.4.2 Exercise AUR
1.5 Missile Identification System
1.6 Support Equipmemt
1.7 Loading and Handling Training Equipmemt
1.8 Documentation
1.8.1 Record Book
1.8.2 Procedural Documentation
1.9 Reports
Section 3. Tomahawk Cruise Missile
1.10 General
1.11 Tactical Variants
1.11.1 Land Attack 109A
A long range missile which carries a non-conventional W80 Warhead with guidance provided
by Terrain Contour Match (TERCOM) techniques. The missile has a modular construction
aluminium airframe.
Land-Attack 109A
1. Guidance Set
2. W80 Warhead
3. Fuel Expansion Bladder
4. CMA Thermal Battery (Dry Well, RH Side)
5. Wing
6. Wing Actuator
7. Standard Mission Cover
8. Lateral Through-Slot
9. Door Actuator
10. Air Data package
11. Mission Control Module
12. Pneumatic Storage Bottle Housing
13. DC Generator-Regulator
14. Sustainer Engine
15. Fin Power Switching Amplifier
16. Fin Servoactuator
17. Fin
18. Rocket Motor
19. Engine Inlet
20. Inlet Actuator
21. Pitot Head
22. Fuel Expansion Bladder
23. Fuel/Defuel Panel
24. Fuel Hopper
25. Coolant Pump (Guidance Set)
26. Radar Altimeter Antenna
27. Nose Cone Kit or Nose Fairing
1.11.1.1 Guidance Section
Positive Retention Nose Cone :
The positive retention nose cone is made of aluminium alloy and threads onto the missile
forward body payload section.
Cruise Missile Guidance Set (CMGS):
missile navigation, guidance and control functions and consists of a
Reference Measurement Unit and Computer, a Rate Gyro/Accelerometer Package (RGAP),
a Missile Radar Altimeter (MRA), an Analogy Filter Assembly (AFA),
a Warhead Interface Unit (WIU), a DC-DC Converter Module and a Batter Power Unit.
The CMGS attaches to the payload section via a mechanical hinge and link assembly using
five mounting bolts.
Cruise Missile Guidance Set
1.11.1.2 Forward Body Payload Section
1.11.1.3 Forward Body Fuel Section
Fuel and expansion bladder to accommodate changes in fuel volume due to fuel expansion
and contraction.
1.11.2 Land-Attack 109C.
A medium range missile armed with a WDU-25/B or WDU-36/B conventional warhead with
guidance provided by Terrain Contour Match (TERCOM) techniques and
Digital Scene Matching Area Correlations (DSMAC) and a
Global Positioning System Subsystem to increase terminal accuracy.
Land-Attack 109C
1. Guidance Set
2. DSMAC (Digital Scene Matching Correlation)
3. Junction Box
4. Warhead Support Wedge
5. Wing
6. Warhead Fuze-Booster
7. CMA Thermal Battery
8. Wing Actuator
9. Standard Mission Cover
10. Lateral Through-Slot
11. Door Actuator
12. Air Data Package
13. Mission Control Module
14. Pneumatic Storage Bottle Housing
15. DC generator-Regulator
16. Sustainer Engine
17. Fin Power Switching Amplifier
18. Fin Servo-actuator
19. Rocket Motor
20. Fin
21. Engine Inlet
22. Pitot Head
23. Fuel Expansion Bladder
24. Fuel/Defuel Panel
25. Fuel Hopper
26. Coolant Pump
27. Dual Air Valve (Warhead Fuze Prearm)
28. WDU-25/B
29. Illuminator Assembly
30. Radar Altimeter Antenna
31. Sensor Window Cover & Thruster
32. Nose Cone Kit or Nose Fairing
33. GPSS Receiver Processor Unit
34. GPSS Antenna Module
1.11.2.1 Forward Body Guidance Section.
No comments:
Post a Comment