Flight Termination Systems Commonality Standard
Attachment aDOCUMENT 319-19Range Safety GroupFLIGHT TERMINATION SYSTEMSCOMMONALITY STANDARDABERDEEN TEST CENTERDUGWAY PROVING GROUNDREAGAN TEST SITEREDSTONE TEST CENTERWHITE SANDS TEST CENTERYUMA PROVING GROUNDNAVAL AIR WARFARE CENTER AIRCRAFT DIVISION PATUXENT RIVERNAVAL AIR WARFARE CENTER WEAPONS DIVISION CHINA LAKENAVAL AIR WARFARE CENTER WEAPONS DIVISION POINT MUGUNAVAL SURFACE WARFARE CENTER DAHLGREN DIVISIONNAVAL UNDERSEA WARFARE CENTER DIVISION KEYPORTNAVAL UNDERSEA WARFARE CENTER DIVISION NEWPORTPACIFIC MISSILE RANGE FACILITY30TH SPACE WING45TH SPACE WING96TH TEST WING412TH TEST WINGARNOLD ENGINEERING DEVELOPMENT COMPLEXNATIONAL AERONAUTICS AND SPACE ADMINISTRATIONDISTRIBUTION A: APPROVED FOR PUBLIC RELEASE;DISTRIBUTION IS UNLIMITED
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DOCUMENT 319-19FLIGHT TERMINATION SYSTEMSCOMMONALITY STANDARDJune 2019Prepared byRANGE SAFETY GROUPPublished bySecretariatRange Commanders CouncilUS Army White Sands Missile RangeNew Mexico 88002-5110
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Flight Termination Systems Commonality Standard – RCC 319-19 June 2019Table of ContentsPreface . xiiiAcronyms . xvChapter d . 1-1Basis of Authority . 1-3Scope . 1-3Acceptability at any Test Range within the Major Range and Test Facility Bases . 1-4Lead Range Safety Office . 1-4Operational Constraints . 1-5Procurement of FTS-Peculiar Test Equipment . 1-6Tailoring. 1-6Waivers and ELS Certifications. 1-7Grandfathering . 1-7Range User-Provided Hardware . 1-8Responsibilities and Authorities . 1-8Chapter 2.2.12.2Tailoring. 2-1Tailoring Overview . 2-1Tailoring Process . 2-1Chapter .153.163.173.183.193.203.213.223.23Introduction . 1-1Common FTS and Component Performance Requirements . 3-1FTS Functional Requirements . 3-1FTS Design . 3-4Environmental Design . 3-11Command Termination System . 3-22Automatic, Inadvertent-Separation, Fail-Safe, or AFTS . 3-23FTS Safing and Arming Devices . 3-31Liquid-Propellant Shutdown . 3-32FTS Monitoring . 3-33FTS Electrical Components and Electronic Circuitry . 3-34FTS Monitor, Checkout, and Control Circuits. 3-42FTS Ordnance Path . 3-42Radio Frequency Receiving System . 3-44FTR . 3-46Wiring and Connectors . 3-60Laser-Initiated Ordnance Fiber-Optic Cable Assembly . 3-63Batteries . 3-64Electromechanical Safe-and-Arm Devices with a Low-Voltage Initiator . 3-73High-Energy Electronic Initiator Firing Unit . 3-77Laser Firing Unit . 3-79Ordnance Interrupter . 3-82Ordnance Initiators. 3-85Devices Containing Percussion Initiators . 3-89Propellant-Actuated Devices/Cartridge-Actuated Devices. 3-91iii
Flight Termination Systems Commonality Standard – RCC 319-19 June 20193.243.253.263.273.283.293.30Explosive Transfer System . 3-92Destruct/Terminate Charge . 3-93Parachute Systems . 3-95FTS Shutdown Valves . 3-95Vibration and Shock Isolators . 3-99Autonomous Flight Termination Unit . 3-99Miscellaneous Components . 3-103Chapter 74.284.294.304.314.324.334.344.354.36FTS Component Test and Analysis Requirements . 4-1Scope and Compliance . 4-1Component Tests and Analyses . 4-1Test Plans and Procedures . 4-1Test Anomalies and Failures . 4-1Failure Analysis . 4-2Test Tolerances . 4-3Test Equipment . 4-4Rework and Repair of Components . 4-10Test and Analysis Reports . 4-10Component Test and Analysis Tables. 4-11Component Examination . 4-15Acceptance Testing and Analysis . 4-17General Qualification Testing and Analysis Requirements . 4-26Qualification Non-Operating Environments . 4-28Qualification Operating Environments . 4-34Radio Frequency Receiving System . 4-53FTR - Analog/Tone-Based. 4-56EFTR . 4-71Autonomous Flight Termination Unit . 4-86FTS Shutdown Valves . 4-93Miscellaneous Components . 4-103Electrical Connectors and Harnesses . 4-105Remotely Activated Silver-Zinc Batteries . 4-107Thermal Batteries . 4-113Manually Activated Silver-Zinc Batteries . 4-119Nickel-Cadmium Batteries. 4-131Lithium-Ion Batteries . 4-148Lead-Acid Batteries . 4-163Safe-and-Arm Devices, Low-Voltage Initiators, Rotor Leads, and BoosterCharges . 4-179High-Energy Firing Units . 4-195LFUs, Fiber-Optic Cable Energy Transfer Systems, and LIDs . 4-209Ordnance Interrupters . 4-225Percussion-Initiated Device . 4-232Explosive Transfer System, Ordnance Manifolds, and Destruct Charges . 4-239Ordnance Interfaces and Manifold Qualification . 4-244Shock and Vibration Isolators . 4-246iv
Flight Termination Systems Commonality Standard – RCC 319-19 June 2019Chapter 5. FTS Component, Subsystem, and System Pre-launch Test andLaunch Requirements . 5-15.15.25.35.45.55.6General . 5-1Pre-flight Component Tests . 5-4Pre-launch Subsystem and System-Level Tests . 5-10Range and Vehicle Compatibility . 5-16Special Tests . 5-17Post-Mission Data Analysis . 5-17Chapter 6. FTS Ground Support and Monitoring Equipment DesignRequirements. 6-16.16.26.36.46.5General . 6-1Ordnance Initiator Simulator . 6-1Laser Test Equipment . 6-2Range Safety Console . 6-2Ground Support Equipment Provided by the Range User . 6-4Chapter .157.167.177.187.197.20General . 7-1System Reliability . 7-1Single-Point Failure . 7-1Fratricide . 7-1Bent Pin. 7-2Radio Frequency Link. 7-2Sneak Circuit . 7-2Software and Firmware . 7-2Battery Capacity. 7-3Component Maximum Predicted Environment . 7-3Failure Analysis . 7-4Qualification-by-Similarity Analysis . 7-4Vehicle Power Analysis . 7-5Radio Frequency Radiation Analysis. 7-5FTS Breakup Analysis . 7-5Tip-Off Analysis . 7-5Automatic Destruct System Timing Analysis. 7-6Ordnance Initiator Simulator Analysis . 7-6In-Flight FTS Analysis . 7-6FTS Laser-Initiated Detonator Heat Dissipation Analysis . 7-6Chapter 8.8.18.28.38.48.58.6FTS Analysis . 7-1Documentation . 8-1General . 8-1FTSR . 8-1FTSR Submittal Process . 8-1Final Approval . 8-2FTSR Format . 8-2Telemetry Measurement . 8-5v
Flight Termination Systems Commonality Standard – RCC 319-19 June 20198.7FTSR Appendixes . 8-5Appendix A.A.1A.2A.3A.4A.5A.6Introduction . A-1Scope . A-1Software Safety Considerations . A-2Safety-Critical Software Requirements for Partitioned and Non-PartitionedSystems . A-6Support-Critical Software Requirements for Partitioned Systems . A-21Assessment (IV&V) Level of Effort Determination Guidance . A-22Appendix 6C.17C.18Electronic Piece-Part Derating Requirements . C-1General . C-1Capacitors . C-2Connectors Reliability Application Derating Guidelines . C-6Crystal Reliability Application Derating Guidelines . C-7Diode Reliability Application Derating Guidelines . C-8Electromagnetic Interference Filters - Reliability Application DeratingGuidelines . C-9Fuses - Reliability Application Derating Guidelines . C-10Inductor and Transformer Reliability Application Derating Guidelines . C-11Integrated Circuits . C-12Motors - Derating Criteria . C-14Printed Wiring Boards and Printed Circuit Boards
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This report assesses the consequences of commonality and pro- . 40 CHAPTER FOUR The Effects of Commonality on Logistics. 45 CHAPTER FIVE An Aid to Commonality . 2.1. Stoner 63A Weapon System. 15 3.1. Variability in Selected Engine .
demand-side factors. Further, it is expected that commonality in liquidity across futures and option contracts with the same underlying assets should be stronger. Two hypotheses are defined: Hypothesis 1: liquidity commonality across derivative markets - there exist systematic patterns across the liquidities of stock futures and options markets;
Flight Operation Quality Assurance (FOQA) programs are today customary among major . EASA European Aviation Safety Agency F/D Flight Director . FAF Final Approach and Fix point FCOM Flight Crew Operating Manual FCTM Flight Crew Training Manual FDAP Flight Data Analysis Program FDM Flight Data Monitoring FLCH Flight Level Change FMC Flight .
59. Notice of sale of residential premises by landlord 60. Recognition of certain persons as tenants 61. Death of co-tenant Part 8 Termination of Residential Tenancy Agreements Division 1 -General 62. Circumstances of termination of residential tenancies 63. Termination notices 64. Termination Orders 65. Withdrawal of termination notices 66.
Fiber optic termination - ModLink plug and play fiber optic solution 42 Fiber optic termination - direct field termination 42 Fiber optic termination - direct field termination: Xpress G2 OM3-LC connector example 43 Cleaning a fiber optic 45 Field testers and testing - fiber optic 48 TSB-4979 / Encircled Flux (EF) conditions for multimode fiber .
TABLE OF CONTENTS Foreword iii Acknowledgements v INTRODUCTION 1 Termination of Employment Convention, 1982 (No. 158) 1 Termination of Employment Recommendation, 1982 (No. 166) 2 Caribbean Community Model Law on Termination of Employment 3 Status of Legislation on Termination of Employment in the Caribbean 4 Objective of the Digest 4
Using ASA’s Flight Planner A flight log is an important part in the preparation for a safe flight. The flight log is needed during flight to check your groundspeed and monitor flight progress to ensure you are staying on course. The Flight Planner has two sections; the Preflight side is used for pre-
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