* ARMY TM 9-1425-688-10 MARINE CORPS TM 09397B-12/1A

TECHNICAL MANUAL

OPERATORS MANUALFOR THE

JAVELIN WEAPON SYSTEMM98A1 (NSN 1430-01-433-8019) (EIC: N/A)

DISTRIBUTION STATEMENT D - Distribution authorized to Department of Defense and DoD contractors only to protect critical technical data on systems or hardware. This determination was made in 01 June 1996. Other requests shall be referred to Commander, U.S. Army Aviation and Missile Command, ATTN: SFAE-MSLS-CWS-AS-J, Redstone Arsenal, AL 35898-5000. WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec. 2751 et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25. DESTRUCTION NOTICE - Destroy by any method that will prevent disclosure of contents or reconstruction of the document.

*THIS PUBLICATION SUPERSEDES TM 9-1425-688-12, TM 09397B-12/1A DATED 24 MAY 2005 HEADQUARTERS, DEPARTMENT OF THE ARMY AND HEADQUARTERS, MARINE CORPS 10 MAY 2007

PCN 184 093971 00

TM 9-1425-688-10

WARNING SUMMARYThe warning summary contains general safety warnings that must be understood and applied during operation and maintenance. Failure to observe these warnings could result in serious injury or death to personnel. For information concerning First Aid, refer to FM 4-25.11.

WARNINGMISSILE LAUNCHING

FLYING PARTICLES Flying debris can cause serious injury. Should injury occur, get medical help at once. Do not launch the missile where obstructions such as trees, bushes, windows, doors, and/or overhangs would obstruct the missiles flight path. Do not fire the javelin over heads of friendly troops during training. Make sure all friendly troops are clear of back blast areas.

TM 9-1425-688-10

WARNING SUMMARY (Continued)WARNING

EAR PROTECTION All personnel within 25 meters (83 feet) must wear hearing protection.

TM 9-1425-688-10

WARNING SUMMARY (Continued)WARNINGMISSILE LAUNCHING Allow sufficient space for the missile to clear any possible obstruction when launching the missile. Personnel may be injured if a javelin missile is launched from enclosures without sufficient openings. Launch missile with left eye if face shield absorber (a piece between indentation and main housing) is missing. Follow instructions in WP 0007 00 for a failure to launch/fire.

FLYING PARTICLES Debris from the rocket motor may cause serious injury. Avoid looking down-range during initial missile launch without proper protection. Use the CLU to observe missile flight. Should injury occur, get medical help at once.

TM 9-1425-688-10

WARNING SUMMARY (Continued)WARNINGPRONE POSITION Keep body at a 30 angle away from the round when launching a missile from the prone position. Injury may occur if body is extended into back blast area. If injury should occur, seek medical help immediately. Ensure that gunner's body remains clear of the back blast area.

WARNINGLAUNCH TUBE ASSEMBLY Do not attempt to remove the missile from the LTA.

WARNINGCLU BATTERY

VAPOR The BA-5590/U battery contains pressurized lithium sulfur dioxide gas. It is highly toxic. Do not handle the battery in any way which may cause the battery to rupture.

TM 9-1425-688-10

WARNING SUMMARY (Continued)WARNINGCLU BATTERY Do not use the Saft America BA-5590/U batteries produced under contract DAAB07-88-C-C045 & DAAB0790-C-C020. BA-5590/U batteries made under both contracts were dead lined in December 1997 by safety of use message SOUM 97-017.

HOT AREA Power down the CLU if the battery or battery compartment becomes hot to the touch. Wait at least 60 minutes before attempting to remove the battery.

VAPOR Do not discharge batteries which show signs of bulging or cracks. Dispose of batteries as hazardous waste. Batteries which show signs of a damaged discharge switch may be unstable and could result in violent battery venting during handling or disposal. Dispose of batteries as hazardous waste.

TM 9-1425-688-10

WARNING SUMMARY (Continued)WARNINGCLU BATTERY Power down the CLU upon hearing a hissing/popping sound (battery venting). Leave the area until any smell (rotten eggs) or signs of leaking gas have been cleared from the area.

WARNINGBATTERY COOLANT UNIT

HOT AREA Hot surfaces can cause serious burns. Do not touch unshrouded BCU surfaces. If the operator experiences burns from contact with BCU, get medical help at once. The BCU contains a lithium-alloy thermal battery that is considered hazardous waste. Disposal of the BCU after use must be in accordance with TB 43-0134.

TM 9-1425-688-10

WARNING SUMMARY (Continued)WARNINGSHIPPING AND STORAGE CONTAINER

EXPLOSION Vent shipping and storage container prior to removing cover assembly. Failure to comply may result in injury to personnel.

WARNINGNUCLEAR, BIOLOGICAL, AND CHEMICAL CONTAMINATION Notify your supervisor if you think you have been exposed to nuclear, biological, or chemical contamination. FM 3-11.5 gives procedures for decontamination.

TM 9-1425-688-10 LIST OF EFFECTIVE WORK PACKAGES INSERT LATEST CHANGED WORK PACKAGES. DESTROY SUPERSEDED DATA. Dates of issue for original and changed pages/work packages are: Original 0 10 May 2007

TOTAL NUMBER OF PAGES FOR FRONT AND REAR MATTER IS 24 AND THE TOTAL NUMBER OF WORK PACKAGES IS 22 CONSISTING OF THE FOLLOWING: Page/WP No. Change No. Page/WP No. Change No.

Cover...........................0 a-g ...............................0 h Blank ........................0 A..................................0 B Blank........................0 i-vii...............................0 viii Blank ......................0 Chapter 1 Title Page ...0 WP 0001 00 ................0 WP 0002 00 ................0 WP 0003 00 ................0 Chapter 2 Title Page ...0 WP 0004 00 ................0 WP 0005 00 ................0 WP 0006 00 ................0 WP 0007 00 ................0 WP 0008 00 ................0 WP 0009 00 ................0

WP 0010 00 ................0 WP 0011 00 ................0 WP 0012 00 ................0 WP 0013 00 ................0 WP 0014 00 ................0 Chapter 3 Title Page ...0 WP 0015 00 ................0 Chapter 4 Title Page ...0 WP 0016 00 ................0 WP 0017 00 ................0 Chapter 5 Title Page ...0 WP 0018 00 ................0 WP 0019 00 ................0 WP 0020 00 ................0 WP 0021 00 ................0 WP 0022 00 ................0 Index ...........................0

A/(B Blank)

TM 9-1425-688-10 *ARMY TM 9-1425-688-10 MARINE CORPS TM 09397B-12/1A HEADQUARTERS, DEPARTMENT OF THE ARMY AND MARINE CORPS WASHINGTON, DC., 10 MAY 2007

OPERATORS MANUAL For JAVELIN WEAPON SYSTEM M98A1 (NSN 1430-01-433-8019) (EIC: N/A)REPORTING ERRORS AND RECOMMENDING IMPROVEMENTS You can help improve this manual. If you find any mistakes, or if you know of a way to improve the procedures, please let us know. Mail your letter or DA Form 2028 (Recommended Changes to Publications and Blank Forms) directly to: Commander, U.S. Army Aviation and Missile Command, ATTN: AMSAM-MMC-MA-NP, Redstone Arsenal, AL 35898-5000. A reply will be furnished to you. You may also provide DA Form 2028 information to AMCOM via email, fax, or the World Wide Web. Our fax number is: DSN 788-6546 or Commercial 256-842-6546. Our email address is: 2028@redstone.army.mil. Instructions for sending an electronic 2028 may be found at the back of this manual. For World Wide Web use: https://amcom2028.redstone.army.mil. Notice of discrepancies or suggested changes should be forwarded on NAVMC form 10772 to: Commander, Marine Corps Logistics Bases (Code ACAL) Albany, Ga 31704-1128.

i

TM 9-1425-688-10DISTRIBUTION STATEMENT D - Distribution authorized to Department of Defense and DoD contractors only to protect critical technical data on systems or hardware. This determination was made on 01 June 1996. Other requests shall be referred to Commander, U.S. Army Aviation and Missile Command. ATTN: SFAE-MSLS-CWS-AS-J, Redstone Arsenal, AL 35898-5000. WARNING - This document contains technical data whose export is restricted by the Arms Export Control Act (Title 22, U.S.C., Sec. 2751 et. seq.) or the Export Administration Act of 1979, as amended, Title 50, U.S.C., App. 2401 et. seq. Violations of these export laws are subject to severe criminal penalties. Disseminate in accordance with provisions of DoD Directive 5230.25. DESTRUCTION NOTICE - Destroy by any methods that will . prevent disclosure of contents or reconstruction of the document

*This publication supersedes TM 9-1425-688-12 and TM 09397B-12/1A dated 24 May 2005 TABLE OF CONTENTS WP Sequence No WARNING SUMMARY HOW TO USE THIS MANUAL CHAPTER 1 - GENERAL INFORMATION, EQUIPMENT DESCRIPTION AND THEORY OF OPERATION General Information ............................................... 0001 00 Equipment Description and Data ........................... 0002 00 Theory of Operation ............................................... 0003 00 CHAPTER 2 - OPERATOR INSTRUCTIONS Description and Use of Operator Controls and Indicators .................................................... 0004 00 Carry Techniques, Firing Restrictions And Selecting A Firing Position................................. 0005 00 Assembly and Preparation for Use ........................ 0006 00 Target Engageability .............................................. 0007 00

ii

TM 9-1425-688-10 TABLE OF CONTENTS (Continued) CLU Battery Installation, Removal, and Disposal ............................................................. 0008 00 BCU Removal, Installation and Disposal ...................................................... 0009 00 Operating Procedures............................................ 0010 00 CLU Round and Carry Bag Cleaning Instructions......................................................... 0011 00 Packing Instructions CLU Shipping and Storage Container....................................... 0012 00 Operation Under Unusual Conditions .................... 0013 00 Emergency Procedures ......................................... 0014 00 CHAPTER 3 - TROUBLESHOOTING PROCEDURES Operational Check Out and Troubleshooting Procedures.............................. 0015 00 CHAPTER 4 - MAINTENANCE INSTRUCTIONS Introduction to Preventive Maintenance Checks and Services ...................................................... 0016 00 Preventive Maintenance Checks and Services ..... 0017 00 CHAPTER 5 - SUPPORTING INFORMATION References............................................................. 0018 00 Components of End Items and Basic Issue Items Lists ................................................ 0019 00 Additional Authorization List (AAL) ........................ 0020 00 Expendable/Durable Supplies and Materials List............................................... 0021 00 Loose Cargo Transportation .................................. 0022 00 INDEX ALPHABETICAL LIST INDEX 1

iii

TM 9-1425-688-10

HOW TO USE THIS MANUALYou must familiarize yourself with the procedure before beginning the task. To become familiar with this manual, spend some time looking through it to see what it contains. Once you are familiar with it, you can find information in two ways: Use the table of contents Use the index at the rear of the manual

The best way to find what you want depends on how familiar you are with this manual. In most cases, the fastest way is to use the table of contents. USE THE TABLE OF CONTENTS 1. The table of contents is a list of work packages in the manual. 2. Suppose you were told to clean the CLU. 3. Using the example below, you could go directly to the table of contents. There you would see Work Package 0011 00, CLU Round and Carry Bag Cleaning Instructions. 4. The top of the page has INITIAL SETUP. This tells you what you will need to complete the procedure. 5. Following the INITIAL SETUP are illustrated procedures to clean the CLU.

iv

TM 9-1425-688-10 USE THE TABLE OF CONTENTS - ContinuedTM 9-1425-688-10 0011 00

OPERATOR INSTRUCTION JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 CLU, ROUND AND CARRY BAG CLEANING INSTRUCTIONS

INITIAL SETUP Tools Materials None Kit, Lens Cleaning, Item 2, WP 0021 00 Cloth, Cleaning, Item 5, WP 0021 00 Detergent, General Purpose Cleaning Item 6, WP 0021 00

CLU and ROUND 1. Inspect surfaces for heavy coating of dirt or mud. If dirt or mud is visible go to step 2. If slightly dirty, i.e., dust, proceed to step 3.

2. Rinse area with clean water and wipe with clean dry cloth. 0011 00-1

v

TM 9-1425-688-10 USE THE INDEX AT THE REAR OF THE MANUAL 1. The index lists, in alphabetical order, all the subjects that are in the manual. 2. Each subject is listed in two or three ways whenever possible so that you can easily find what you are looking for. For example, "List of Abbreviations" is also listed as "Abbreviations, List of". EMERGENCY PROCEDURES This manual contains EMERGENCY PROCEDURES for use by the operator if a missile fails to launch. As shown below these pages are BLACK BORDERED to allow for instant location within the book. Read the procedures in case you experience a hangfire or misfire. References within the manual refer to WP 0014 00 when immediate action may be needed.

vi

TM 9-1425-688-10 USE EMERGENCY PROCEDURES - ContinuedTM 9-1425-688-10 OPERATOR INSTRUCTIONS JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 EMERGENCY PROCEDURES JAVELIN WARNINGS AND MALFUNCTIONS (Continued) Definitions Misfire: When the fire trigger has been pulled and the missile does not launch. The ; indicator on the CLU display may or may not flash. Hangfire: When the fire trigger has been pulled and the missile does not launch. The ; indicator on the CLU display will be flashing. The missile has been activated and could possibly launch. Javelin Malfunction Indicators/Immediate Action Procedures. PROBLEM MISFIRE INDICATOR ; Red (Flashing) or NO INDICATOR ACTION (1) Release fire and seeker triggers. Keep Javelin pointed in direction of enemy. (2) Re-attempt to launch missile. If missile fails to launch, go to (3) below. (3) Set CLU power switch to OFF. 0014 00

0014 00-01

vii/(viii Blank)

TM 9-1425-688-10

CHAPTER 1 GENERAL INFORMATION, EQUIPMENT DESCRIPTION AND THEORY OF OPERATION FOR JAVELIN WEAPON SYSTEM

TM 9-1425-688-10

0001 00

GENERAL INFORMATION JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 GENERAL INFORMATIONSCOPE Type of Manual: Model Number and Equipment Name: Operators Maintenance Surface Attack Guided Missile & Launcher: FGM-148A, FGM-148B and FGM-148C Command Launch Unit: M98A1 Purpose of Equipment: To provide medium range antitank capability for the U.S. Army and U.S. Marine Corps.

MAINTENANCE FORMS, RECORDS, AND REPORTS Department of the Army forms and procedures used for equipment maintenance shall be those prescribed by DA PAM 750-8, the Army Maintenance Management System (TAMMS) Users Manual. Accidents involving injury to personnel or damage to materiel will be reported on DA Form 285, U.S. Army Accident Report, in accordance with AR 385-40, Accident Reporting and Records. Explosives and ammunition malfunctions will be reported in accordance with AR 75-1, Malfunctions Involving Ammunition and Explosives (RCS CSGLD-1961(MI)). Marine Corps Personnel will use TM 4700-15/1 Equipment Record Procedures.

0001 00-1

0001 00

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REPORTING EQUIPMENT IMPROVEMENT RECOMMENDATIONS If your Javelin needs improvement, let us know. Send us an EIR. You, the user, are the only one who can tell us what you do not like about your equipment. Let us know why you do not like the design or performance. Put it on an SF Form 368 (Product Quality Deficiency Report). Mail it to: Commander, U.S. Army Aviation Missile Command, ATTN: AMSAM-MMCMA-NM, Redstone Arsenal, AL 35898-5238. E-mail to: cfo@redstone.army.mil. We'll send you a reply. Marine Corps Personnel are encouraged to submit SF Form 368 in accordance with MCO 4855.10. CORROSION PREVENTION AND CONTROL Corrosion Prevention and Control (CPC) of Army materiel is a continuing concern. It is important that any corrosion problems with this item be reported so that the problem can be corrected and improvements can be made to prevent the problem in the future. While corrosion is typically associated with rusting of metals, it can also include deterioration of other materials, such as rubber and plastic. Unusual cracking, softening, swelling or breaking of these materials may be a corrosion problem. If a corrosion problem is identified, it can be reported using Product Quality Deficiency Report SF Form 368. Use of key words such as corrosion, rust, deterioration or cracking will ensure that the information is identified as a CPC problem. The form should be submitted to the address specified in DA PAM 750-8.

0001 00-2

TM 9-1425-688-10 OZONE DEPLETING SUBSTANCES

0001 00

The continued use of ozone depleting substances (ODS) has been prohibited by Executive Order 12856 of 3 August 1993. Ozone depleting substances are not used during operation or maintenance of the Command Launch Unit (CLU). DESTRUCTION OF ARMY AND MARINE MATERIEL TO PREVENT ENEMY USE CORPS

Destruction of Army materiel to prevent enemy use shall be in accordance with TM 43-0002-70. Marine Corps Personnel: render the CLU inoperable by smashing, scattering or burying disassembled pieces, burning or destroying by weapons fire. PREPARATION FOR STORAGE OR SHIPMENT Refer to WP 0012 00 for instructions on preparing the CLU for storage or shipment.

0001 00-3

0001 00

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NOMENCLATURE CROSS-REFERENCE LIST Simplified Nomenclature Absorber Absorber Absorber Absorber Absorber Aft End Cap Aft End Cap Membrane Bail Battery Cover BCU BCU Latch BCU Status Indicator Buckle Carry Handle CLU Interface Connector Crossbrace Daysight Daysight Lens Daysight Lens Cover Detector Dewar Cooler Diopter Adjust Ring Elapsed Time Meter Eyecup Eyepiece Face Shield Absorber Fire Trigger Flipper Mirror Official Nomenclature Afocal Absorber Battery Box Cover Absorber Battery Cover Absorber Left Handle Absorber Right Handle Absorber Aft Shock Cushion Frangible Membrane Battery Cover Retainer Assembly Battery Cover Assembly Battery Coolant Unit (BCU) Assembly BCU Latch Assembly BCU Temperature Indicator Slide Adjuster Handle Electrical Plug Connector Lower Crossbrace Assembly Visible Optics Assembly No. 1 Window Visible Optics Assembly Lens Cap Detector Dewar Cooler Assembly Diopter Grip Time Totalizing Meter Eyecup Assembly Eyepiece Assembly Top/Facial Absorber Right Trigger Assembly Display Injection Mirror

0001 00-4

TM 9-1425-688-10 NOMENCLATURE CROSS-REFERENCE LIST (Continued) Simplified Nomenclature Forward End Cap Forward End Cap Latch Guide Bar Guide Pin Guide Pin Humidity Indicator Humidity Indicator Latch Assembly Latch Release Launch Tube Assembly Left Handgrip Controls Lens Paper Locking Pin Main Housing Manual Release Button Night Vision Sight NVS Lens NVS Lens Cover Protective Cover Pylon Right Handgrip Controls Round Official Nomenclature

0001 00

Forward Shock Cushion End Cap Clamp Alignment Pin Pylon Aft Guide Pin Pylon Forward Guide Pin Desiccator Forward Desiccator Latch Base Latch Lock Launch Tube Final Assembly Left Switch Assembly Presaturated Lens Paper End Cap Lock Pin Main Housing Assembly Manual Release Button Afocal Assembly Afocal Number One Lens Lens Cap Assembly Protective Cap Pylon Assembly Right Switch Assembly Surface Attack Guided Missile: FGM-148A, FGM-148B, and FGM-148C Alignment Hooks

Round Hooks

0001 00-5

0001 00

TM 9-1425-688-10

NOMENCLATURE CROSS-REFERENCE LIST (Continued) Simplified Nomenclature Round Interface Bracket Round Interface Catch Round Interface Connector Seeker Trigger Shoulder Strap Strap Mount Strap Mount Wire Rope Official Nomenclature Missile Interface Bracket Missile Interface Catch Viking Connector Left Trigger Assembly Shoulder Strap Carrying Assembly Aft Shoulder Strap Mount Forward Shoulder Strap Mount Flexible Wire Rope

0001 00-6

TM 9-1425-688-10 LIST OF ABBREVIATIONS AND ACRONYMS

0001 00

Abbreviations and Acronyms, with their meanings, are contained in the following list: Abbreviation/Acronym AAL ASIOE BCU BII BIT CAGEC CIIC COEI CLU CPU CTA DDC DMWR DOT EIR EMI EOD ETM FOV FTT IR JTA LTA MAC Meaning Additional Authorization List Associated Support Item of Equipment Battery Coolant Unit Basic Issue Items Built-in-Test Commercial and Government Entity Code Controlled Item Inventory Code Components of End Items Command Launch Unit Corrosion Prevention and Control Common Table of Allowances Detector Dewar Cooler Depot Maintenance Work Requirements Department of Transportation Equipment Improvement Recommendations Electromagnetic Interference Explosive Ordnance Disposal Elapsed Time Meter Field-of-View Field Tactical Trainer Imaging Infrared Joint Table of Allowances Launch Tube Assembly Maintenance Allocation Chart

0001 00-7

0001 00

TM 9-1425-688-10

LIST OF ABBREVIATIONS AND ACRONYMS (Continued) Abbreviation/Acronym MTOE NBC NFOV NHA NSN NVS ODS PMCS Q-D QASAS SMR SRA TAMMS TDA TMDE TOE UUT U/M WFOV Meaning Modified Table Of Organizational Equipment Nuclear, Biological, and Chemical Narrow Field-of-View Next Highest Assembly National Stock Number Night Vision Sight Ozone Depleting Substances Preventive Maintenance Checks and Services Quantity-Distance Quality Assurance Specialist Ammunition Surveillance Source, Maintenance and Recoverability Code Specialized Repair Activity The Army Maintenance Management System Table of Distribution and Allowances Test, Measurement, and Diagnostic Equipment Table of Organizational Equipment Unit Under Test Unit of Measure Wide Field-of-View

0001 00-8

TM 9-1425-688-10 QUALITY OF MATERIAL

0001 00

Material used for replacement, repair or modification must meet the requirements of this technical manual. If quality of material requirements are not stated in this technical manual, the material must meet the requirements of the drawings, standards, specifications or approved engineering change proposals applicable to the subject equipment. SAFETY, CARE, AND HANDLING CLU Safety The CLU has been assigned a Controlled Item Inventory Code (CIIC) of Category 3. Physical security provided to the CLU must be commensurate with this CIIC. The Javelin round and CLU together are CIIC Category 1. The CLU and round must never be stored at the same location. Round Safety The Javelin round is classified Quantity-Distance (Q-D) Class 1.1 when out of round shipping and storage container (1.2 when in container), Compatibility Group E, and Department of Transportation (DOT) Class A for shipping. Explosive weight: Warhead Missile motor Launch Tube Assembly 5.89 lb 2.69 lb 6.94 lb

0001 00-9

0001 00

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SAFETY, CARE, AND HANDLING (Continued) CLU Care CLU lenses require special care. Don't try to scrub lens surface, optical coating may be damaged. When cleaning the lenses, always follow the cleaning procedure in WP 0011 00. When the CLU has been in storage for long periods of time, the CLU must be powered-up in DAY mode to allow the cathode ray tube to warm up prior to applying high voltage in the Night Vision Sight (NVS) mode. Use the chart listed below to determine the warm-up time period. Storage Time 3 Months - 1 Year 1 Year or Longer Round Care Storage temperature limits for Javelin rounds are -51 to +160F (-46 to +71C). Warm-Up Time 5 Minutes 12 Hours

0001 00-10

TM 9-1425-688-10 SAFETY, CARE, AND HANDLING (Continued) CLU Handling

0001 00

CAUTION If CLU has been in storage in excess of 30 days, DO NOT power-up CLU in NVS mode of operation or place switch in TEST position. Power-up CLU in day mode for at least five minutes. Failure to comply will damage CRT. If CLU has been in storage longer than one year, CLU must be powered-up in day mode for a minimum of 12 hours. DO NOT place switch in NIGHT or TEST position sooner than 12 hours.

The Javelin CLU is shipped and stored in the CLU shipping and storage container. The CLU shipping and storage container protects the CLU during transportation, storage, and associated handling. The CLU shipping and storage container also protects the CLU from natural and induced environments, including nuclear, biological, and chemical (NBC) environments. During unit storage keep the CLU in the CLU shipping and storage container, sealed with a security seal.

0001 00-11

0001 00

TM 9-1425-688-10

SAFETY, CARE, AND HANDLING (Continued) Round Handling CAUTION The Launch Tube Assembly provides environmental and physical protection for the missile. Do not attempt to remove the missile from the Launch Tube Assembly. Do not handle the round roughly or drop it. Rough handling may damage the missile motor or missile components and cause a malfunction at launch or in flight.

The Javelin round is shipped and stored in the round shipping and storage container. The round shipping and storage container protects the round during transportation, storage, and associated handling. The round shipping and storage container also protects the round from natural and induced environments, including NBC environments.

0001 00-12

TM 9-1425-688-10 SAFETY, CARE, AND HANDLING (Continued)

0001 00

Design features of the round shipping and storage container include: A cover assembly containing a latch mechanism that provides environmental and Electromagnetic Interference (EMI) seals. Pressure and humidity control provided by a humidity indicator, 2 packages of desiccant, and a pressure release valve controlling positive and negative container pressure to two pounds per square inch differential. Four handles for lifting and tiedown and interlocking posts to provide stack stability.

Rounds may be stacked 8 high in indoor storage, and 4 high (depending on stack stability) on level, improved outdoor storage. Use 4-inch dunnage for indoor storage and 6-inch dunnage for outdoor storage. Do not use dunnage between stack layers, containers have interlocking feature. The nose end of rounds in storage must be pointed in the direction posing the least hazard to personnel and equipment in case of fire or accidental explosion. Temporary shelters (tarpaulin covered, shed, etc.). Javelin rounds may be maintained in this type of storage with storage site location in a well drained area. Tarpaulin or cover should be placed in a manner to permit free air circulation while still protecting rounds from direct sunlight. This type of storage should be used only when mission requirements dictate and should not exceed 30 days.

0001 00-13

0001 00

TM 9-1425-688-10

SAFETY, CARE, AND HANDLING (Continued) Open storage (without tarpaulin, shed etc.) will be permitted only during wartime and during firing exercises. Before storing rounds in open storage during peacetime, authorization must be first obtained from Commander, USA AMCOM, ATTN SFAE-MSLS-CWS-AS-J, Bldg 4505, Redstone Arsenal, AL 35898-5000. Open storage must be held to the absolute minimum time (not to exceed 30 days). Open storage in excess of 30 days requires waiver. Request for waiver must be submitted in accordance with AMC-R 385100 through command channels to Commander, HQ, AMC Safety Office, ATTN AMCSF-X, with a copy provided to SFAE-MSLS-CWS-AS-J. The Javelin round has been assigned a CIIC of Category 1. Physical security provided to the round must be commensurate with this CIIC. The Javelin round and CLU together are also CIIC Category 1. The round and CLU must never be stored at the same location. Refer to DA PAM 385-63 and DA PAM 385-64 for general ammunition care, handling, and safety. Refer to TB 43-0134 for the safe handling of lithium-sulfur dioxide batteries. Warning And Caution Statements WARNING and CAUTION statements have been strategically placed throughout this text prior to operating or maintenance procedures. Conditions considered essential to the protection of personnel are labeled CAUTION. A WARNING or CAUTION will apply each time the related step is repeated. Prior to starting any task, the WARNINGs or CAUTIONs included in the text for that task shall be reviewed and understood.

0001 00-14

TM 9-1425-688-10

0002 00

GENERAL INFORMATION JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 EQUIPMENT DESCRIPTION AND DATASCOPE This section shows the location and briefly describes the major components of the Javelin weapon system. Equipment characteristics, capabilities, features, differences between models, equipment data, equipment configuration, safety, care and handling are explained. EQUIPMENT CHARACTERISTICS, CAPABILITIES, AND FEATURES The Javelin is a medium range, manportable, recoilless, antitank assault weapon and is capable of defeating current and projected enemy armor, and hovering enemy helicopters. The Javelin can be used during the day, night, or degraded weather conditions, including electronic and electro-optical countermeasures. The Javelin is made up of a one-time expendable round and a Command Launch Unit (CLU). The round consists of a missile environmentally sealed inside a Launch Tube Assembly (LTA). The LTA is also used as the missile launch platform. The CLU is manportable, reusable, battery operated, and is the gunner's interface with the round. The CLU contains Builtin-Test (BIT) capability. The CLU is issued with a carry bag. The carry bag provides space to carry the CLU, lens cleaning kit, technical manual, and battery.

0002 00-1

0002 00

TM 9-1425-688-10

EQUIPMENT CHARACTERISTICS, CAPABILITIES, AND FEATURES (Continued)

Figure 1.

Major Components

0002 00-2

TM 9-1425-688-10 LOCATION AND DESCRIPTION OF MAJOR COMPONENTS CLU

0002 00

Figure 2.

CLU (Sheet 1 of 2)

Face Shield Absorber - Shields gunner's face from possible launch debris and helps protect CLU from damage during handling and movement. Absorbers - Protects the CLU from damage during handling and movement. Desiccant Plug - Contains desiccant to reduce humidity inside of the CLU. Power Switch - Four-position rotary switch used to select CLU operational modes. Seeker Trigger - Initiates seeker mode of operation and seeker lock-on after track gates are adjusted around target.

0002 00-3

0002 00

TM 9-1425-688-10

LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (Continued) Left Handgrip Controls - Consists of focus (FOC), sight select (SGT SEL), and filter (FLTR) switches. Switch functions are described in WP 0004 00.

Figure 2.

CLU (Sheet 2 of 2)

Elapsed Time Meter (ETM) - Records the total operating hours of CLU. Move cover aside to view internally mounted ETM. Round Interface Bracket - Provides the mechanical interface with round. Daysight - Optical system that works similar to a telescope. Provides a magnified, visible-light image of what the gunner sees.

0002 00-4

TM 9-1425-688-10 LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (Continued)

0002 00

DDC The Detector Dewar Cooler (DDC) provides thermal imaging for the Night Vision Sight (NVS) operation. Night Vision Sight - Optical system that converts an infrared (IR) image into a visible-light target image of what the gunner sees. Test Connector - Provides electrical interface for Field Tactical Trainer (FTT) simulator round operation and CLU testing. Battery Compartment - Provides housing for the battery. Fire Trigger - Used to initiate missile firing sequence. Right Handgrip Controls - Consists of gate adjust (GATE ADJ), contrast & brightness (CTRS & BRT), and attack select (ATTK SEL) switches. Switch functions are described in WP 0004 00. Absorbers Protect the CLU from damage during handling and movement. Round Interface Connector - Provides electrical interface with the round.

0002 00-5

0002 00

TM 9-1425-688-10

LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (Continued) Round

Figure 3. Components of the Round End Caps - The end caps are designed to protect the missile from damage during transport and handling. There are two end caps on the LTA: the forward and aft end caps. Each has a foam shock absorber to protect the round from impact if it is dropped or otherwise abused. The end caps also provide stability and support when the round is strapped in a vehicle transit rack or placed on the ground.

0002 00-6

TM 9-1425-688-10 LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (Continued)

0002 00

Forward End Cap - The forward end cap protects the missile from moisture, dust, etc. It is not removed unless the missile is to be launched. The forward end cap is removed from the round after the CLU is connected to the round. If the missile is not launched, the forward end cap is reinstalled to prevent missile damage. The forward end cap latch secures forward end cap to round. Locking pin locks forward end cap latch in place and prevents movement. A humidity indicator displays status of relative humidity inside the LTA. Desiccant - Prevents moisture from gathering in the missile and causing possible missile malfunctions. (Not Shown Located in Forward End Cap) CLU Interface Connector - Provides electrical interface with the CLU. Latch Assembly - Provides mechanical interface with the CLU. Shoulder Pad - Provides point of balance and support when round is placed on gunner's shoulder. Launch Tube Assembly - Serves as a handling container and launch platform for the missile. Provides environmental and electromagnetic interference (EMI) protection for the missile. Aft End Cap - The aft end cap is permanently attached to the LTA. During launch, the center of the cap is designed to be blown out by the blast of the missile launch motor. Aft End Cap Membrane - Provides environmental protection for missile. Designed to be blown out by missile launch motor blast during launch.

0002 00-7

0002 00

TM 9-1425-688-10

LOCATION AND DESCRIPTION OF MAJOR COMPONENTS (Continued) Carry Handle - Provides a means to lift and carry the round. Shoulder Strap - Provides a means of carrying the round. Battery Coolant Unit - The Battery Coolant Unit (BCU) consists of two sections: a battery section and a compressedgas coolant section. The battery section powers the missile electronics before missile launch. The coolant section cools the missile to its operating temperature before missile launch. There are two configurations of the BCU and they are functionally identical. DIFFERENCE BETWEEN MODELS This manual covers round versions, FGM-148A, FGM-148B and FGM-148C. There are two versions of the shipping and storage container. Both versions are covered in this manual. ROUND IDENTIFICATION Round Shipping and Storage Containers, PN 13305300-029, PN 13305300-039 and PN 13303015-009 are identified as indicated in Figure 4. ROUND SHIPPING AND STORAGE CONTAINER Container markings include: Storage Temperature Limits, Nomenclature, Contract Number, Serial Number, Part Number, Manufacturer, Material Stock, Center of Gravity, Direction of Flight, Explosive Markings, and United Nations Identification.

0002 00-8

TM 9-1425-688-10 ROUND SHIPPING AND STORAGE CONTAINER (Continued)

0002 00

LEFT SIDE VIEW

LEFT SIDE VIEW

RIGHT SIDE VIEW

RIGHT SIDE VIEW

TOP VIEW

TOP VIEW

FORWARD VIEW

AFT VIEW

FORWARD VIEW

AFT VIEW

PN 13305300-029 AND PN 13305300-039

PN 13303015-009341_0251

Figure 4.

Shipping and Storage Container

LAUNCH TUBE ASSEMBLY The Javelin round is marked in accordance with MIL-STD709C. Javelin rounds are identified with colored bands. Black with yellow banding signifies an armor defeating and high explosive tactical round. A round with a single gold band signifies an inert round.

0002 00-9

TM 9-1425-688-10 EQUIPMENT DATA Weight & Dimensions CLU Weight Length Height Width Carry Bag Battery Lens Cleaning Kit Round Weight Length Width

0002 00

11.44 lb (5.19 kg) 19.29 in. (49.00 cm) 13.77 in. (35.00 cm) 14.96 in. (38.00 cm) 0.60 lb (0.27 kg) 2.22 lb (1.01 kg) 0.05 lb (0.02 kg) 34.16 lb (15.49 kg) 47.60 in. (120.90 cm) 11.75 in. (29.85 cm)

Round Shipping and Storage Container for P/N 13305300-029 and P/N 13305300-039 Weight Length Height Width 40.00 lb (18.14 kg) 59.25 in. (150.50 cm) 15.00 in. (38.10 cm) 15.25 in. (38.74 cm)

Round Shipping and Storage Container for P/N 133003015-009 Weight Length Height Width Weight Length Height Width 54.00 lb (24.49 kg) 55.40 in. (140.72 cm) 18.10 in. (45.97 cm) 15.2 in. (38.6 cm) 29.00 lb (13.15 kg) 27.25 in. (69.22 cm) 16.87 in. (42.85 cm) 21.25 in. (53.98 cm)

CLU Shipping and Storage Container

0002 00-10

0002 00

TM 9-1425-688-10

EQUIPMENT DATA (Continued) Electrical Power Source CLU Round Lithium-Sulfur Dioxide battery, BA-5590/U. BCU containing gas coolant bottle and thermal battery for ground operations, internal thermal battery for flight

Voltage Required CLU Round Fields-of-View CLU: Daysight NVS NFOV NVS WFOV Missile: Seeker Magnification Daysight NVS WFOV NVS NFOV Seeker 4X 4.2X 9.2X 9X 4 by 6 (approx.) 2 by 3 (approx.) 4 by 6 (approx.) 1 by 1 24 VDC Various voltages provided by BCU and internal battery

0002 00-11

TM 9-1425-688-10 EQUIPMENT DATA (Continued) Battery Operating Time CLU: Power Conv Cambe Inc. Above 120F (49C) Below 120F (49C) Saft America Inc. Above 120F (49C) At 50F (10C) to 120F (49C) Below 50F (10C) to -20F (-29C) Round: BCU Missile Effective Range Top Attack Mode Direct Attack Mode 4.0 min 0.5 hr 4.0 hr 0.5 hr 3.0 hr 1.0 hr

0002 00

Minimum 150 m (492 ft) Maximum 2000 m (6562 ft) Minimum 65 m (213 ft) Maximum 2000 m (6562 ft)

EQUIPMENT CONFIGURATION There are three configurations of the Javelin: the M98, the M98A1, and the M98A2. This manual covers CLU M98A1. For information about CLU M98. For information about the CLU M98A2, refer to TM 9-1425-1687-10. PREPARATION FOR AIR DROP Refer to FM 10-552 for instructions on How to Prepare a Javelin for Air Drop.

0002 00-12

TM 9-1425-688-10

0003 00

GENERAL INFORMATION JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 THEORY OF OPERATIONSCOPE Javelin is made up of the CLU and a one-time expendable round. The CLU is manportable, reusable, battery operated, and is the gunner's interface with the round. The CLU provides passive day/night surveillance, target detection, classification and recognition, battlefield damage assessment, CLU status, built-in test (BIT), and missile software storage capabilities. When a round is connected, the CLU provides missile status indication, missile software download, and launch capabilities. CLU OPERATION The CLU has four modes of operation: OFF, DAY, NIGHT, and TEST. The operational modes are controlled by the power switch.

Figure 1. Power Switch 0003 00-1

0003 00

TM 9-1425-688-10

CLU OPERATION (Continued) The CLU may not power up properly the first time it is turned on. Instead of performing normally, the CLU indicators will flash. This behavior occurs when the CLU battery is not able to generate the voltage needed. Leaving the power switch in DAY position for about a minute, then cycling power will condition the battery to supply power to the CLU. The power may have to be cycled on and off several times before the battery is warm enough to begin normal operation. Off Mode. Power switch is in the OFF position. In this mode, no power is applied to the CLU. The daysight can be used for surveillance, target detection, and recognition. The NVS cannot be used and the gunner has no missile launch capability. Day Mode. Power switch is in the DAY position. In this mode, power is applied to the CLU. The day FOV can be used to acquire a target. The gunner has full missile launch capability. Night Mode. Power switch is in the NIGHT position. In this mode, NVS cooldown is initiated. NVS cooldown time is approximately 2.5 minutes. The gunner has full missile launch capability. Test Mode. Power switch is placed in the TEST position, then released. BIT can only be performed when a round is not attached to the CLU. When a round is attached, the TEST position is ignored. Results of BIT are displayed on the CLU display within about 20 seconds of initiation. If a failure is detected during BIT, the CLU BIT FAILURE 7 indicator will light.

0003 00-2

TM 9-1425-688-10

0003 00

JAVELIN OPTICAL SYSTEMS AND FIELDS OF VIEW Javelin is equipped with three optical systems; two in the CLU (daysight and NVS) and one in the round (seeker). An optical system is a series of optical elements (lenses, mirrors, filters, etc.) that gather light at the systems input and develop an image at its output. In this case, the output is to the gunner. The area of a scene that can be viewed at one time through an optical system is the FOV. An optical systems FOV is related to the systems magnification. The wider the FOVs coverage, the less magnification it has. The narrower the FOV's area of coverage, the greater magnification it has. Javelin has four FOVs. They include: day FOV, WFOV, NFOV, and seeker FOV. The daysight provides the day FOV. The Night Vision Sight provides WFOV and NFOV. The seeker, found in the missile, provides seeker FOV. Daysight. The daysight is like a telescope. It provides day FOV for the gunner. Day FOV is used when visibility is good. It is also used to engage a target when the gunner cannot wait the 2.5 minutes required for the NVS to cool down.

Figure 2. Clear/Obscure Target 0003 00-3

0003 00

TM 9-1425-688-10

JAVELIN OPTICAL SYSTEMS AND FIELDS OF VIEW (Continued) Night Vision Sight. The NVS is an imaging infrared (IR) system. It converts an infrared target into a visible target image. This allows the gunner to see during daytime and conditions of limited visibility. The NVS has two fields of view: WFOV and NFOV. Wide Field of View. The WFOV provides the gunner with a 4x magnification of the target scene. With an area of coverage approximately 6 x 4, WFOV covers a large or wide area compared to NFOV. This allows the gunner to scan a large general area to detect potential targets. However, the gunner will not be able to distinguish target detail. As a result, WFOV is used for surveillance and target detection.

Figure 3. Wide Field Of View

0003 00-4

TM 9-1425-688-10

0003 00

JAVELIN OPTICAL SYSTEMS AND FIELDS OF VIEW (Continued) Narrow Field Of View. The NFOV provides an infrared image with 9x magnification of the target scene. With an area of coverage approximately 3 x 2, NFOV covers a smaller, or narrower, area of the scene than WFOV. The gunner would have to move the CLU back-and-forth and up-and-down in NFOV to cover the same area as WFOV. The gunner only uses NFOV after locating a potential target. This lets the gunner see a potential targets details more clearly so the gunner can determine whether or not its a target. Therefore, NFOV is used primarily to classify and recognize a target, but it can be used for battle assessment also.

Figure 4.

Narrow Field Of View

0003 00-5

0003 00

TM 9-1425-688-10

JAVELIN OPTICAL SYSTEMS AND FIELDS OF VIEW (Continued) Seeker Field Of View. The seeker FOV provides an infrared image as seen through the missile with 9x magnification of the target scene. Images in seeker FOV are not as detailed due to the limitations of the optics of the seeker. This FOV is used to lock on to a target and engage it.

Figure 5. Seeker Field of View

0003 00-6

TM 9-1425-688-10 SEEKER OPERATION

0003 00

Seeker Activation. The CLU must be attached to a round before the seeker can be activated. Squeezing the seeker trigger when in DAY mode of NVS mode can activate the seeker. Once the gunner squeezes the seeker trigger, it initializes software download from the CLU to the missile. The seeker begins to cool down and the missile powers up, the 1 and < indicators will light up on the CLU display until the seeker is ready for use (10-15 seconds). The CLU display will change from either ., /, or 0 to 1. Track gates will appear and flash, the < indicator will go out and the 2 attack indicator will come on.

601127A 601127A

AFTER SEEKER TRIGGER PULL

10-15 SECONDS AFTER SEEKER TRIGGER PULL

124_0463

Figure 6. Seeker Activation

0003 00-7

0003 00

TM 9-1425-688-10

SEEKER OPERATION (Continued) Track Gate Adjustments. The gunner uses track gates to lock the seeker onto the target. Track gates are adjusted using the GATE ADJ/CTRS & BRT switch. Track gate adjustments can only be done after seeker activation and prior to lock-on.

Figure 7. Track Gates

0003 00-8

TM 9-1425-688-10 SEEKER OPERATION (Continued)

0003 00

Seeker Lock-On. After the track gates are adjusted around the target, the gunner squeezes and holds the seeker trigger. Two things happen to indicate lock-on has occurred. The track gates stop flashing and solid crosshairs appear on the CLU display.

Figure 8. Seeker Lock On

0003 00-9

0003 00

TM 9-1425-688-10

MISSILE OPERATION Missile Attack Modes. The Javelin can kill a target at two thousand meters. In addition, the missile has two gunnerselectable attack modes (top or direct). Each mode has its own peculiar flight path or "profile" for reaching the target. Top Attack Mode. In top attack, the missile comes from above the target to impact and detonate on top of the target. This capability allows you to attack a vehicle from the front, the rear or a flank position. Generally, armored vehicles have less protective armor on top. By striking the top of the vehicle, the missile penetrates the vehicle and still has enough explosive force remaining to do extensive damage inside the target vehicle. This mode greatly increases the probability of a kill. Top attack is the default missile mode when the seeker is first activated. The exact profile of the missile during flight depends on range to the target and is determined automatically by the missile on-board software. If the target is under a protective structure, using top attack may cause the missile to impact and detonate on the structure instead of the target. To avoid this, the missile can be programmed for direct attack.

Figure 9. Top Attack Mode and Flight Paths

0003 00-10

TM 9-1425-688-10 MISSILE OPERATION (Continued)

0003 00

Direct Attack Mode. In the direct attack mode, the missile impacts and detonates on the side of the vehicle. The direct attack mode flight allows the missile to reach a target that is under a protective structure at a maximum range of 2000 meters. To do this, the missile flies a more direct route from the gunner to the target vehicle. Direct attack can be selected only after the seeker is activated when the gunner pushes the ATTK SEL switch on the right handgrip. As in top attack, the exact profile of the missile flight path depends on the range to the target.

Figure 10. Direct Attack Mode and Flight Paths

0003 00-11/(12 Blank)

TM 9-1425-688-10

CHAPTER 2 OPERATOR INSTRUCTIONS FOR JAVELIN WEAPON SYSTEM

TM 9-1425-688-10

0004 00

OPERATOR INSTRUCTIONS JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 DESCRIPTION AND USE OF OPERATOR CONTROLS AND INDICATORSINTRODUCTION The controls and indicators used to operate the Javelin Command Launch Unit (CLU) and round are described and shown in this work package. Controls are switches and buttons used to perform various functions, with some having dual-purpose use. Indicators identify Javelin operational modes, conditions, and functions. Study the illustrations and descriptions of the controls and indicators before you attempt to operate the Javelin.

0004 00-1

0004 00

TM 9-1425-688-10

COMMAND LAUNCH UNIT Control Function

Figure 1. Diopter Adjust Ring Diopter Adjust Ring The diopter adjust ring is located on the CLU eyepiece. It is a hand rotated ring that the gunner uses to adjust the focus of the CLU display image. The adjustment compensates for individual differences in vision.

0004 00-2

TM 9-1425-688-10 CLU (Continued) Control Power Switch Function Four-position rotary switch. Controls CLU operation.

0004 00

Figure 2. CLU Power Switch OFF position. No power is applied to CLU. Daysight can be used for surveillance and target detection. The Night Vision Sight (NVS) is not operational and gunner has no missile launch capability. DAY position. When the power switch is in the DAY position, the Javelin is in the day mode. In the day mode, power is applied to the CLU. The gunner has use of the day field of view (FOV) but has no NVS. The gunner also has full missile capability. (The gunner can activate the seeker, lock the missile onto a target, and launch the missile).

0004 00-3

0004 00 CLU (Continued) Control Power Switch (Continued)

TM 9-1425-688-10

Function NIGHT position. When the power switch is in the NIGHT position, the Javelin is in the night mode. This mode gives the gunner full Javelin capability. Once the NVS is cool enough (approximately 2.5 to 3.5 minutes, dependent on the temperature), the gunner can select either the NVS wide field of view (WFOV), the narrow field of view (NFOV), or the day FOV. Again, the gunner has full missile capability. (The gunner can activate the seeker, lock the missile onto a target, and launch the missile). TEST position. Spring-loaded position that returns to NIGHT position after being selected and released. Initiates CLU built-in-test (BIT) when round is not attached.

0004 00-4

TM 9-1425-688-10 CLU (Continued) Control Right Handgrip Function

0004 00

124_0487

Figure 3. Right Handgrip GATE ADJ CTRS & BRT Spring-loaded, self-centering thumb switch. Moves up, down, left, and right. Switch functions differently during NVS and seeker operations. NVS Operation. - Adjusts contrast and brightness of CLU display image. Brightness is adjusted by moving switch vertically (up increases brightness /down decreases brightness). Contrast is adjusted by moving switch horizontally (left decreases contrast/right increases contrast). Seeker Operation - Adjusts size of track gates. Up moves track gates apart vertically and down moves track gates together vertically. Left moves track gates in horizontally and right moves track gates out horizontally

0004 00-5

0004 00 CLU (Continued) Control Right Handgrip - (Continued) ATTK SEL

TM 9-1425-688-10

Function

Allows gunner to select which missile flight profile (top attack or direct attack) to use for target engagement. Switch is only active after seeker activation and cool down. Top attack is the default mode. Direct attack mode can be selected by pressing ATTK SEL switch. The mode selected will be indicated by the appropriate indicator lighting on CLU display. Switch is deactivated after seeker lock-on is commanded. Sends fire signal to missile. Fire trigger disabled until seeker lock-on.

Fire Trigger

0004 00-6

TM 9-1425-688-10 CLU (Continued) Control Left Handgrip Function

0004 00

124_0486

Figure 4. Left Handgrip SGT SEL Selects FOV viewed on CLU display. Appropriate indicator (., /, 0) lights when SGT SEL switch is pressed. Switch is only active after NVS cool down and the power switch is in the NIGHT position. Pressing SGT SEL switch allows gunner to cycle through day ., /, and 0. After seeker activation, gunner can switch back to last FOV before seeker activation by pressing SGT SEL switch. 0004 00-7

0004 00 CLU (Continued) Control Left Handgrip (Continued) FOCUS

TM 9-1425-688-10

Function

Spring-loaded, self-centering thumb switch. Adjusts focus of NVS (WFOV or NFOV). Not operational in day or seeker FOVs. Moves up or down. Up. - Focus at a longer range. Down. - Focus at a closer range.

FLTR Trigger Guard Seeker Trigger

Selects NVS filter. The filter is used as field counter-counter measure. Prevents seeker from accidental activation. Lift up to access seeker trigger. Activates seeker, locks seeker onto a target, and enables fire trigger. Initial squeeze, (3-5 seconds) and release action activates Battery Coolant Unit (BCU), initiates seeker cool down, missile power up, and software download to missile. When seeker trigger is squeezed a second time and held, seeker lock-on is initiated. When seeker lock-on is achieved, fire trigger is enabled. Releasing seeker trigger after lock-on and prior to pressing fire trigger to launch missile will cause a loss of lock-on.

0004 00-8

TM 9-1425-688-10 CLU (Continued) Control Left Handgrip - (Continued) Seeker Trigger Function

0004 00

Activates seeker, locks seeker onto a target, and enables fire trigger. Initial squeeze, (3-5 seconds) and release action activates Battery Coolant Unit (BCU), initiates seeker cool down, missile power up, and software download to missile. When seeker trigger is squeezed a second time and held, seeker lock-on is initiated. When seeker lock-on is achieved, fire trigger is enabled. Releasing seeker trigger after lock-on and prior to pressing fire trigger to launch missile will cause a loss of lock-on.

0004 00-9

0004 00 CLU INDICATORS Indicator

TM 9-1425-688-10

Function

Figure 5. Elapsed Time Meter and Desiccant Plug Elapsed Time Meter Desiccant Plug Records elapsed time of CLU operation. Contains desiccant for the CLU.

0004 00-10

TM 9-1425-688-10 CLU DISPLAY INDICATORS

0004 00

Status Indicators. The status indicators surround the CLU display images, whether they are from the daysight (.), from the NVS (/ or 0), or from the seeker in the missile (1). The gunner can observe the status indicators by looking into the eyepiece. They identify Javelin operational modes, conditions, and malfunctions. There are fourteen indicators, each coded in one of three colors: green, amber, or red. All the status indicators are never lit at the same time during normal operation. However, a few may be lit simultaneously.

Figure 6. Status Indicators

0004 00-11

0004 00

TM 9-1425-688-10

CLU DISPLAY INDICATORS Green Status Indicators. Seven of the fourteen status indicators are green. Green signifies that the monitored function is in a satisfactory condition and that it is all right to proceed with normal operations. Indicator Function

Figure 7. Green Status Indicators

. /

The DAY indicator is located at the top of the CLU display and at the far left. It lights when the day FOV is selected when the power switch is either in the Day or Night mode. The WFOV indicator is located at the top of the CLU display and to the left of center. Solid ON indicates the CLU is in WFOV. When it flashes, it indicates the NVS has reached a focus limit.

0004 00-12

TM 9-1425-688-10 CLU DISPLAY INDICATORS (Continued) Indicator Function

0004 00

0

The NFOV indicator is located at the top of the CLU display and to the right of center. When it is steadily lit, it indicates that the CLU is in NFOV. When it flashes, it indicates that a focus limit has been reached. The SEEK indicator is located at the top of the CLU display at the far right. It lights within 3 seconds after gunner pulls the seeker trigger. When the SEEK indicator lights, the gunner releases the seeker trigger. The gunner sees 1 approximately 10 seconds later.

1

0004 00-13

0004 00

TM 9-1425-688-10

CLU DISPLAY INDICATORS Indicator Function

Figure 8. CLU Display Indicators

2 3 4

The TOP indicator is located in the right side of the CLU display at the top. It lights when the missile is in the top attack mode. This is the default mode. The DIR indicator is located in the right side of the CLU display in the center. It lights when the missile is in the direct attack mode. The FLTR indicator is located on the right side of the CLU display at the bottom. It lights when the filter is selected.

0004 00-14

TM 9-1425-688-10 CLU DISPLAY INDICATORS (Continued)

0004 00

Amber Status Indicators. Two of the status indicators are amber. Amber is used to advise the gunner that a marginal condition exists. It also alerts the gunner to situations where caution, a recheck, or an unexpected delay is necessary. Indicator Function

Figure 9. Amber Status Indicators

Figure 10. Amber Indicator for Caution, Recheck or Delay 0004 00-15

0004 00

TM 9-1425-688-10

CLU DISPLAY INDICATORS (Continued) Indicator Function The NVS NOT COOL indicator is located on the left side of the CLU display at the top. It lights when the NVS is selected but the detector dewar cooler (DDC) has not cooled down to its operating temperature. The indicator goes out when the NVS is cooled down to its operating temperature. If the DDC warms up again, this indicator lights. The MISSILE NOT READY indicator is located at the bottom of the CLU display at the far right. Solid ON indicates the missile flight information is not downloaded from the CLU, missile BIT is not complete, or seeker not cooled. The MISSILE NOT READY indicator flashes to indicate the missile electronics are close to an overheat condition. Missile will shut down a minimum of 30 seconds after flashing starts.

+

,

0004 00-16

TM 9-1425-688-10 CLU DISPLAY INDICATORS (Continued)

0004 00

Red Status Indicators. Five of the status indicators are red. Red has two meanings depending on whether it is flashing or solid. A flashing red indicator is used to warn the gunner of an emergency condition where action must be taken. A solid indicator is used to alert the gunner that the system or any portion of the system is inoperative or that a successful Javelin engagement is not possible until corrective action is taken. Indicator Function

Figure 11. Red Status Indicators

;

The MISSILE BIT FAILURE indicator is located at the bottom of the CLU display and to the right of center. Solid ON indicates the missile BIT has detected a failure within the missile. The MISSILE BIT FAILURE indicator flashes to indicate a misfire occurred when the gunner squeezed the fire trigger and the missile did not launch. 0004 00-17

0004 00

TM 9-1425-688-10

CLU DISPLAY INDICATORS (Continued) Indicator Function The HANGFIRE indicator is located on the bottom of the CLU display and to the left of center. The HANGFIRE indicator flashes to indicate a missile hangfire occurred when the gunner squeezed the fire trigger.

:

0004 00-18

TM 9-1425-688-10 CLU DISPLAY INDICATORS (Continued) Indicator Function

0004 00

Figure 12. Battery Coolant Unit (BCU) Low Indicator

9

The BATTERY COOLANT UNIT LOW indicator is located at the bottom of the CLU display at the far left. During system operation, after seeker activation, the 0 indicator will flash to indicate the BCU has approximately 30 seconds (or more, depending on the ambient temperature) of operating time remaining. When it lights solid, the BCU is spent, the CLU reverts to the last CLU FOV, all missile functions stop, and the missile cannot be launched.

0004 00-19

0004 00

TM 9-1425-688-10

CLU DISPLAY INDICATORS (Continued) Indicator Function The CLU BATTERY LOW indicator is located on the left side of the display at the bottom. The indicator flashes to indicate the CLU battery is low and has approximately 2 to 5 minutes of operating time remaining. When the CLU battery power is too low to operate the CLU, the CLU display automatically reverts to day FOV (. does not illuminate), the CLU BATTERY LOW indicator goes solid and the 7 illuminates. The missile cannot be launched until the CLU battery is replaced.

8

0004 00-20

TM 9-1425-688-10 CLU DISPLAY INDICATORS (Continued) Indicator Function

0004 00

Figure 13. CLU BIT FAILURE Indicator

7

The CLU BIT FAILURE indicator is located on the left side of the CLU display in the center. The CLU BIT FAILURE lights to indicate the CLU has failed its BIT.

0004 00-21

0004 00

TM 9-1425-688-10

ROUND CONTROLS Control Function

Figure 14. Round Controls BCU Latch Releases BCU from round when pulled upward (BCU P/N 13303250) or when pressed down (BCU P/N 13303844). Secures BCU to round when BCU is properly mounted. Secures forward end cap to round. After locking pin is removed, forward end cap latch is rotated counterclockwise to release forward end cap. Secures CLU to round when CLU is properly mounted. Releases CLU from round when pressed

Forward End Cap Latch Latch Release

0004 00-22

TM 9-1425-688-10 ROUND CONTROLS (Continued) Control Function

0004 00

Figure 15. Manual Release Button Manual Release Button Equalizes pressure between the outside atmospheric pressure and the air space between the seeker dome and the forward end cap when pushed. (May make a hissing sound when pressed while equalizing pressure.). 0004 00-23

0004 00

TM 9-1425-688-10

ROUND CONTROLS (Continued) Indicator Function

Figure 16. BCU Status Indicator BCU Status Indicator Displays status of BCU. Indicator changes from a white spot to a dark spot to indicate when BCU is expended. 0004 00-24

TM 9-1425-688-10 ROUND CONTROLS (Continued) Indicator Function

0004 00

Figure 17. Humidity Indicator Humidity Indicator Located on the forward end cap. Monitors humidity of round during longterm storage. It does not determine serviceability of the round.

0004 00-25/(26 Blank)

TM 9-1425-688-10

0005 00

OPERATOR INSTRUCTIONS JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 CARRY TECHNIQUES, FIRING RESTRICTIONS AND SELECT A FIRING POSITIONSCOPE This work package contains instructions for operating the Javelin weapon system under usual conditions. Carry techniques, firing restrictions, selecting a firing position, target engageability, engage a target, engage multiple targets, target engagement during limited visibility conditions, malfunction procedures, and troubleshooting are explained. The tasks are organized to make it as easy as possible for you to complete what is required. Review this work package, WP 0007 00 and WP 0010 00 to make sure that you are familiar with the procedures for each task before attempting to perform a task. Refer to WP 0006 00 for unpacking instructions for the Javelin Command Launch Unit (CLU). Refer to WP 0006 00 for preparation for issue and use of the round. CARRY TECHNIQUES There are three recommended carry techniques that the soldier can use to transport the CLU and round: short distance, long distance, and tactical. Marine Corps Personnel may use the missile carry bag (not shown) in the same position as the Launch Tube Assembly (LTA) in the Short Distance and Long Distance Carry.

0005 00-1

0005 00

TM 9-1425-688-10

CARRY TECHNIQUES (Continued)

CAUTIONDamage to CLU and round could occur if shoulder strap comes free from strap mounts. To prevent damage to CLU and round, ensure that shoulder strap is properly routed through buckles. Check routing of shoulder strap through buckle. If necessary, redo as shown.

Figure 1. Shoulder Strap Buckle Routing Short Distance Carry. In the short distance carry technique, the round can be carried in one of two ways: 1. The round may be carried on the gunners right side with the shoulder strap over the right shoulder. The round is parallel to the ground, waist high with the forward end cap pointed in the direction of movement. The right hand may be placed on the shoulder strap to help keep the strap on the shoulder.

0005 00-2

TM 9-1425-688-10 CARRY TECHNIQUES (Continued)

0005 00

2. The round may be carried on the gunners right side with the shoulder strap over the right shoulder. The forward end cap is pointed down with the round behind the right shoulder, parallel to the gunners body. The gunners right hand may be placed on the shoulder strap to help keep the strap on his shoulder.

124_0412

124_0413 120_0413

Figure 2.

Carry Techniques

0005 00-3

0005 00

TM 9-1425-688-10

CARRY TECHNIQUES (Continued) Long Distance Carry. The long distance carry technique is used when contact is not likely and the Javelin is not required for immediate use.

124_0432Figure 3. Long Distance Carry Technique

0005 00-4

TM 9-1425-688-10 CARRY TECHNIQUES (Continued)

0005 00

Tactical Carry. The tactical carry technique is used when moving between firing locations and enemy contact is likely.

Figure 4. Tactical Carry Technique

0005 00-5

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TM 9-1425-688-10

FIRING RESTRICTIONS

WARNING

FLYING PARTICLES Flying debris can cause serious injury. Should injury occur get medical help at once. Don't launch the missile where obstructions such as trees, bushes, windows, doors, and/or overhangs would obstruct the missile's flight path. Do not fire the javelin over heads of friendly troops during training.

0005 00-6

TM 9-1425-688-10 FIRING RESTRICTIONS (Continued)

0005 00

Figure 5. Danger Areas Rear Danger Area. The area primarily to the rear of the round. In this area, fatalities or serious injury could occur because of the blast, flame, and flying debris. The rear danger area is divided into the primary danger zone and three caution areas. Primary Danger Zone. The primary danger zone is a 60 included sector, with the apex of the sector at the aft end of the missile Launch Motor. The primary danger zone radius of curvature is 25 meters. Serious injury or fatality is possible for personnel in the primary danger zone during a firing. A portion of the primary danger zone has been extended forward to the firing line. This portion is within the range of 1 through 5 meters left and right of the launch tube centerline. This extended portion is an area affected by activation of the flight motor relief system.

0005 00-7

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TM 9-1425-688-10

FIRING RESTRICTIONS (Continued) Caution Area 1. Caution Area 1 is an area extending radially 25 meters (82 feet) from each side of the primary danger zone to the firing line. Serious hearing impairment or damage from frequent exposure could occur to personnel in this area during firings. Approved hearing protection and eye protection should be worn by personnel positioned in this area. Caution Area 2. Caution Area 2 is an extension to the rear of the primary danger zone and is identified as a 10 meter (32.9 feet) radius, aft of the launcher and within 60 sector. Approved hearing protection and eye protection should be worn by personnel who are positioned in this area. Caution Area 3. Caution Area 3 is an extension to the rear of the primary danger zone and is identified as a 100 meter (329 feet) radius, aft of the launcher and within 60 sector. This is the area affected by activation of the flight motor pressure relief system. Approved hearing protection and eye protection should be worn by personnel who are positioned in this area.

0005 00-8

TM 9-1425-688-10 FIRING RESTRICTIONS (Continued)

0005 00

WARNINGPersonnel may be injured if a javelin missile is launched from enclosures without sufficient openings.

Figure 6. Minimum Enclosure Example

0005 00-9

0005 00

TM 9-1425-688-10

FIRING RESTRICTIONS (Continued) Enclosure. When launching a missile from an enclosure, the enclosure must meet the following minimum requirements: Room dimensions must be at least 15 feet by 12 feet by 7 feet high. Window opening must be at least 2 feet by 2 feet, 6 inches. Door opening must be at least 2 feet, 11 inches by 6 feet, 7 inches. When firing from a room, the gunner should assume a kneeling position at window. This allows the gunner to extend the end of the round past the window. The gunner may rest either his elbows or the CLU handgrips on the window frame. Also, remember that the end of the round must extend out at least as far as the outer-most overhang to prevent the missile from hitting any structures when it is launched.

Figure 7. Launching From an Enclosed Area

0005 00-10

TM 9-1425-688-10 FIRING RESTRICTIONS (Continued)

0005 00

WARNING Dont launch the missile where obstructions such as trees, bushes, windows, doors, and/or overhangs would obstruct the missiles flight path. Allow sufficient space for the missile to clear any possible obstruction when launching the missile. Do not fire the javelin over heads of friendly troops during training. Obstructions. Survey the area surrounding the fighting position for obstructions which may interfere with missile launch or flight. Sight along top of round to check for clearance. If no obstructions, such as tree limbs, buildings, power lines, etc. can be seen, the gunner has sufficient clearance to launch the missile. Refer to WP 0003 00 for Missile Attack Mode trajectory.

Figure 8. Required Clearance 0005 00-11

0005 00

TM 9-1425-688-10

FIRING RESTRICTIONS (Continued)

GUNNER SIGHTING ALONG TOP OF ROUND

CLEAR FLIGHT PATH

OBSTRUCTED FLIGHT PATH

Figure 9. Clear and Obstructed Flight Paths

0005 00-12

TM 9-1425-688-10 SELECT A FIRING POSITION

0005 00

There are four recommended positions the gunner can use to launch a missile. Sitting Position Kneeling Position Standing Supported Position Prone Position

Sitting Position

124_0410

Legs Crossed

Knees Bent

Figure 10. Sitting Firing Position 1. Sit or kneel on the left side of the Javelin facing in the direction of fire. 2. Check the back blast area. Ensure no one is located in the back blast area. 3. Grasp the left handgrip with your left hand. Place your right hand under the round near the shoulder pad.

0005 00-13

0005 00

TM 9-1425-688-10

SELECT A FIRING POSITION (Continued) 4. Lift the Javelin in a single, smooth motion and position the shoulder pad on your right shoulder. 5. Adjust your body while holding the CLU to get into a comfortable sitting position. 6. Check the overhead flight path between the target and your firing position. To do this, sight along the top of the round. As long as all obstacles are above the line of the round, the missile has a clear path when it is launched. 7. After assuming a sitting position, ensure the forward end cap is on the ground, in front of and slightly to the right of right leg or foot. This ensures that it is out of the back blast area and that it is within easy reach to set the front end of the round on the end cap when you remove the Javelin from your shoulder.

0005 00-14

TM 9-1425-688-10 SELECT A FIRING POSITION (Continued) Kneeling Position

0005 00

Figure 11.

Kneeling Firing Position

1. Kneel on left side of the Javelin at the forward end, facing in the direction of fire. 2. Check the backblast area. Ensure no one is located in the backblast area. 3. Grasp the left handgrip with the left hand. Place right hand under the round near the shoulder pad. Lift the Javelin in a single, smooth motion and position the shoulder pad on the right shoulder.

0005 00-15

0005 00

TM 9-1425-688-10

SELECT A FIRING POSITION (Continued) 4. Hold the CLU by the right handgrip and adjust your body into the more comfortable position, with one knee or both knees on the ground. 5. Check the overhead flight path between the target and the firing position. To do this, sight along the top of the round. As long as all obstacles are above the line of the round, the missile has a clear path when it is launched. 6. After assuming the kneeling position, ensure the forward end cap is front of and slightly to the right of right leg or foot. This ensures that it is out of the back blast area and that it is within easy reach to set your front end on the end cap if removing the Javelin from your shoulder.

0005 00-16

TM 9-1425-688-10 SELECT A FIRING POSITION (Continued) Standing Supported Position

0005 00

Figure 12. Standing Supported Firing Position

1. Kneel on the left side of the Javelin at the forward end. 2. Check the backblast area (Specific requirements to be determined). 3. Grasp the left handgrip with your left hand. Place your right hand under the round near the shoulder pad. 4. Lift the Javelin in a single, smooth motion and position the shoulder pad on your right shoulder.

0005 00-17

0005 00

TM 9-1425-688-10

SELECT A FIRING POSITION (Continued) 5. Carefully rise to a standing position with legs spread apart. 6. Hold the CLU by the right handgrip and place your elbows on the edge or rim of the fighting position. 7. Check the overhead flight path between the target and your firing position. To do this, sight along the top of the round. As long as all obstacles are above the line of the round, the missile has a clear path when it is launched. 8. After assuming the firing position, ensure that the forward end cap is on the ground, and slightly to the right of your foot.

0005 00-18

TM 9-1425-688-10 SELECT A FIRING POSITION (Continued) Prone Position

0005 00

1. Set round on the ground with the flat sides of the end caps face down. The CLU interface connector and latch assembly should face up. 2. Ensure that the round points toward the target area. 3. Place the carry bag (with CLU) on the left side of the round by the forward end. 4. Lay on your left side along the left side of the round next to the carry bag. Maintain a low profile to limit observation of your movements.

124_0491

Figure 13. Prone Position 0005 00-19

0005 00

TM 9-1425-688-10

SELECT A FIRING POSITION (Continued) 5. Remove the CLU from the carry bag. Turn the power switch to the NIGHT position. Connect the CLU to the round. 6. Remove forward end cap and place it directly under the open end of the Javelin.

CAUTIONWith the forward end cap removed, the seeker is exposed. Use extreme caution when tipping the Javelin forward to ensure no foreign material (rocks, mud, etc.) comes in contact with the seeker. 7. Open the NVS and daylight lens covers. 8. Check the back blast area. Ensure that no personnel are located in the primary danger or caution areas. 9. Position your body so it is parallel with the Javelin and place left hand tightly on the left handgrip.

0005 00-20

TM 9-1425-688-10 SELECT A FIRING POSITION (Continued)

0005 00

10 Tilt the Javelin and your body to the left side and at the same time reach out with your right hand to secure the forward end cap.

124_0492

Figure 14.

Grasping Forward End Cap

0005 00-21

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TM 9-1425-688-10

SELECT A FIRING POSITION (Continued) 11. Grasp the forward end cap, hold it with the inside of the forward end cap facing toward the CLU, the outside facing toward the ground, and the flat side of the forward end cap facing up.

Figure 15.

Javelin Resting on the Forward End Cap

0005 00-22

TM 9-1425-688-10 SELECT A FIRING POSITION (Continued)

0005 00

12. Slowly lower the Javelin until it rests on the forward end cap. Slide your body forward so that your right shoulder is against the forward end cap and the right handgrip is within reach.

WARNING Injury may occur if body is extended into back blast area. If injury should occur seek medical help immediately. Keep body at 30 angle away from the round when firing from the prone position. Ensure that gunners body remains clear of the back blast area.

NOTE Dont balance the round on your shoulder while in the prone position. Use the forward end cap to balance the round and to keep the aft end cap off the ground.

0005 00-23

0005 00

TM 9-1425-688-10

SELECT A FIRING POSITION (Continued) 13. Place your body at a 30 angle to the length of the round. This prevents your legs from extending into the backblast area.

Figure 16. Javelin at 30 Angle from Body END OF WORK PACKAGE 0005 00-24

TM 9-1425-688-10

0006 00

OPERATOR INSTRUCTIONS JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 ASSEMBLY AND PREPARATION FOR USEINITIAL SETUP Tools Materials UNPACKING None None

WARNING

EXPLOSION Vent shipping and storage container prior to removing cover assembly. Failure to comply may result in injury to personnel. 1. Press pressure release valve on CLU shipping and storage container, hold until hissing stops. 2. Remove security seal. 3. Grasp latch handles and turn counterclockwise.

0006 00-1

0006 00

TM 9-1425-688-10

UNPACKING - (Continued) 4. Pull out and down from container and unhook four latches from rim of top cover.

Figure 1.

CLU Shipping and Storage Container

0006 00-2

TM 9-1425-688-10 UNPACKING - (Continued)

0006 00

5. Open top cover on CLU shipping and storage container.

Figure 2.

CLU Shipping and Storage Container Open

6. Ensure that CLU, carry bag, lens cleaning kit, desiccant, and technical manual are present. Place battery (BA-5590/U) in shipping container.

0006 00-3

0006 00

TM 9-1425-688-10

UNPACKING - (Continued)

Figure 3.

CLU, Battery, Lens Cleaning Kit, Technical Manual and Carry Bag

7. Close top cover on CLU shipping and storage container. 8. Hook four latches on rim of top cover and turn latch handles clockwise to secure.

NOTERetain CLU shipping and storage container and all packing materials for reuse. 9. When issuing CLU to gunner, place all items in carry bag and retain shipping container with desiccant.

0006 00-4

TM 9-1425-688-10 ASSEMBLY

0006 00

CAUTION The Launch Tube Assembly (LTA) provides environmental and physical protection for the missile. Do not attempt to remove the missile from the LTA. Do not handle the round roughly or drop it. Rough handling may damage the missile motor or missile components and cause a malfunction at launch or in flight. 1. Using two persons, place the round shipping and storage container in a suitable area.

NOTE Perform steps 2 thru 5 below, for shipping and storage containers PN 13305300-029 and PN 1330530-039. Perform step 6 below, for shipping and storage containers PN 13303015-009. 2. Remove cover assembly as follows:

0006 00-5

0006 00

TM 9-1425-688-10

ASSEMBLY - (Continued)

WARNING

EXPLOSION Vent shipping and storage container prior to removing cover assembly. Failure to comply may result in injury to personnel. a. Press pressure release valve, hold until hissing stops. b. Remove security seal.

Figure 4.

Round Shipping and Storage Container (FWD) 0006 00-6

TM 9-1425-688-10 ASSEMBLY (Continued) c.

0006 00

Press spring and rotate latch handle until it contacts cover.

d. Rotate locking shaft clockwise until free. e. Remove cover assembly.

NOTERetain round shipping and storage container and all packing materials for reuse. 3. Remove round as follows: a. Pull foam cushion from round shipping and storage container. b. Open foam cushion and lift out round. The round is now ready for issue and use.

0006 00-7

0006 00

TM 9-1425-688-10

ASSEMBLY (Continued) 4. Place foam cushion into round shipping and storage container.

Figure 5.

Foam Cushion

0006 00-8

TM 9-1425-688-10 ASSEMBLY (Continued) 5. Install cover assembly as follows:

0006 00

a. Position cover assembly on round shipping and storage container ensuring markings are aligned.

Figure 6.

Round Storage and Shipping Container Alignment Markings

b. Rotate locking shaft counter-clockwise to engage ends of locking shaft with round shipping and storage container. c. Lower latch handle onto spring and press until secured.

0006 00-9

0006 00

TM 9-1425-688-10

ASSEMBLY (Continued)

WARNING

EXPLOSION Vent shipping and storage container prior to removing cover assembly. Failure to comply may result in injury to personnel. 6. Remove Javelin round from shipping and storage container with PN 13303015-009 as follows: a. On removable endcap assembly (8), turn vent valve (10), counter-clockwise to the open position until hissing stops. b. Break security seals (9). c. Open four latch assemblies (11) on removable endcap assembly and remove assembly from missile container.

d. Remove endcap foam (6) and desiccant (7).

NOTEWhen removing round cushion container assembly, ensure grooves remain aligned and round does not rotate. e. Using strap (4), slide round cushion container assembly (2) out of missile container. f. Open securing straps (5).

0006 00-10

TM 9-1425-688-10 ASSEMBLY (Continued)

0006 00

Figure 7.

Round Removal

0006 00-11

0006 00

TM 9-1425-688-10

ASSEMBLY (Continued) g. Open round cushion container assembly and remove Javelin round (3) from round cushion container assembly. h. Close round cushion container assembly and secure with straps. i. Align grooves and slide round cushion container assembly into missile container, aft end first.

NOTEReplace desiccant as required (TM 9-1427-68723). j. k. l. Place removable end cap foam and desiccant into removable end cap assembly. Place removable end cap assembly on missile container and close four latch assemblies. Turn vent valve clockwise to the closed position and tighten securely.

END OF WORK PACKAGE

0006 00-12

TM 9-1425-688-10

0007 00

OPERATOR INSTRUCTIONS JAVELIN WEAPON SYSTEM M98A1 NSN 1430-01-433-8019 TARGET ENGAGEABILITYTARGET ENGAGEABILITY The gunner uses the stadia in CLU display to determine if a target is in-range of the Javelin missile. The stadia are based on the size of an average main battle tank approximately 10-feet wide and 20-feet long. A tank approximately 20 feet (6 meters) in length, when seen in a flank aspect, bridges the gap between the stadia at the Javelin's maximum range (2,000 meters), exceeds the stadia at closer ranges, and does not bridge the stadia at longer ranges. An approaching or retreating tank (front or rear aspect) is approximately 10 feet (3 meters) wide, and bridges half the stadia gap at maximum range. The turret of the main battle tank is approximately 10 feet (3 meters) in length and width and is judged in the same way as a front/rear target. Two different stadia methods are used to determine if targets are in-range. The stadia method used is based upon target aspect. The two methods are full-stadia and half-stadia. FULL-STADIA METHOD The full-stadia method uses the full distance between the stadia to determine if a target is in-range. The full-stadia method is applied equally for the day FOV, WFOV, and NFOV stadia. Day FOV Stadia. The full distance between the day FOV stadia is represented by the day FOV upper stadia. Apply the day FOV full-stadia method as follows:

0007 00-1

0007 00

TM 9-1425-688-10

FULL-STADIA METHOD (Continued) 1. Move the day FOV upper stadia to the target, keeping the target between the day FOV upper stadia.

Figure 1.

Day FOV Upper Stadia

2. Place one side of the day FOV upper stadia on one edge of the target. If the opposite edge of the target touches or exceeds the other side of the day FOV upper stadia, the target is in-range.

Figure 2.

Day FOV In-Range Target 0007 00-2

TM 9-1425-688-10 FULL-STADIA METHOD (Continued)

0007 00

3. If the opposite edge of the target does not touch or exceed the other side of the day FOV upper stadia, the target is out-of-range.

Figure 3.

Day FOV Out-Of-Range Target

0007 00-3

0007 00

TM 9-1425-688-10

FULL-STADIA METHOD (Continued) WFOV Stadia. Apply the WFOV full-stadia method as follows: 1. Move the WFOV stadia to the target, keeping the target between the WFOV stadia.

Figure 4. 2.

WFOV Stadia

Place one of the WFOV stadia on one edge of the target. If the opposite edge of the target touches or exceeds the other WFOV stadia, the target is inrange.

Figure 5.

WFOV In-Range Target 0007 00-4

TM 9-1425-688-10 FULL-STADIA METHOD (Continued) 3.

0007 00

If the opposite edge of the target does not touch or exceed the other WFOV stadia, the target is out-ofrange.

Figure 6.

WFOV Out-of-Range Target

NFOV Stadia. Apply the NFOV full-stadia method as follows:

Figure 7.

NFOV Stadia

0007 00-5

0007 00

TM 9-1425-688-10

FULL-STADIA METHOD (Continued) 1. 2. Move the NFOV stadia to the target, keeping the target between the NFOV stadia. Place one of the NFOV stadia on one edge of the target. If the opposite edge of the target touches or exceeds the other NFOV stadia, the target is inrange.

Figure 8. 3.

NFOV In-Range Target

If the opposite edge of the target does not touch or exceed the other NFOV stadia, the target is out-ofrange.

Figure 9.

NFOV Out-Of-Range Target

0007 00-6

TM 9-1425-688-10 HALF-STADIA METHOD

0007 00

Figure 10.

Day FOV Lower Stadia

The half-stadia method uses half the distance between the stadia to determine if a target is in-range. The half-stadia method is applied differently for the day FOV, WFOV, and NFOV stadia. Day FOV Stadia. Half the distance between the day FOV stadia is represented by day FOV lower stadia. Apply the day FOV half-stadia method as follows: 1. Move the day FOV lower stadia to the target, keeping the target between the day FOV lower stadia.

0007 00-7

0007 00

TM 9-1425-688-10

HALF-STADIA METHOD (Continued) 2. Place one side of the day FOV lower stadia on one edge of the target. If the opposite edge of the target touches or exceeds the other side of the day FOV lower stadia, the target is in-range.

Figure 11.

Day FOV Lower Stadia In-Range Target

3.

If the opposite edge of the target does not touch or exceed the other side of the day FOV lower stadia, the target is out-of-range.

Figure 12.

Day FOV Lower Stadia Out Of-Range Target

0007 00-8

TM 9-1425-688-10 HALF-STADIA METHOD (Continued)

0007 00

Figure 13.

WFOV Half Stadia Method

WFOV Stadia. Half the distance between the WFOV stadia is represented by an imaginary line mentally drawn by the gunner. Apply the WFOV half-stadia method as follows: 1. Move the WFOV stadia to the target, keeping the target between the WFOV stadia.

0007 00-9

0007 00

TM 9-1425-688-10

HALF-STADIA METHOD (Continued) 2. Place one of the WFOV stadia on one edge of the target. If the opposite edge of the target touches or exceeds the imaginary line, the target is in-range.

Figure 14. 3.

WFOV Half-Stadia In-Range Target

If the opposite edge of the target does not touch or exceed the imaginary line, the target is out-ofrange.

Figure 15.

WFOV Half-Stadia Out-Of-Range Target

0007 00-10

TM 9-1425-688-10 HALF-STADIA METHOD (Continued)

0007 00

Figure 16.

NFOV Half Stadia Method

NFOV Stadia. Half the distance between the NFOV stadia is represented by the upper reticle line. Apply the NFOV half-stadia method as follows: 1. Move the NFOV stadia to the target, keeping the target between the NFOV stadia.

0007 00-11

0007 00

TM 9-1425-688-10

HALF-STADIA METHOD (Continued) 2. Place one of the NFOV stadia on one edge of the target.

Figure 17. 3.

NFOV In-Range Target

If the opposite edge of the target does not touch or exceed the upper reticle line, the target is out-ofrange.

Figure 18.

NFOV Out-Of-Range Target

0007 00-12

TM 9-1425-688-10 TOP ATTACK

0007 00

In top attack, both stadia methods are used. The stadia method applied is determined by the target aspect. Front/Rear and Front/Rear-Oblique. Apply the halfstadia method using the front/rear edges of the target. Flank and Flank-Oblique. Apply the full-stadia method using the flank edges of the target. Hull Defilade. Apply the half-stadia method using the turret edges of the target. DIRECT ATTACK Direct attack should be used on targets under cover, hovering helicopters, and bunkers. Front/Rear and Front/Rear-Oblique Targets Under Cover. Apply the half-stadia method using the front/rear edges of the target. Flank and Flank-Oblique Targets Under Cover. Apply the full-stadia method using the flank edges of the target. Frontal Hovering Helicopters. Apply the full-stadia method using the weapons pylon wing edges of the target.

0007 00-13

0007 00

TM 9-1425-688-10

DIRECT ATTAC