Modelling the Ignition of Modular Charges

Similar documents
NEGATIVE DIFFERENTIAL PRESSURE BY IGNITION OF GRANULAR SOLID PROPELLANT

ROCKET - ASSISTED AMMUNITION TECHNOLOGIES for 120 mm MORTARS

Development of an Extended Range, Large Caliber, Modular Payload Projectile

BAE Systems V2C2 Program

Insensitive Munitions (IM) Testing: 25mm Target Practice, Discarding Sabot with Trace (TPDS-T), M910 Cartridge using ECL Propellant

ECL Propellant Demonstration for Extended Range in 120mm Mortar combined with Ballistic and Chemical Stability Equals Win for the Warfighter

LOW RECOIL, HEAT TRANSFER MITIGATING RAREFACTION WAVE GUN ENGINEERING, MODELING AND LARGE CALIBER SYSTEM DEMONSTRATOR DEVELOPMENT

Development, evaluation and lifetime prediction of medium and large caliber ammunition

Inductive Settable Electronic Time Fuze for Mortars

STUDIES OF IGNITION DELAY AT 40 mm CALIBRE. M. J. Taylor, S. R. Fuller, C. R. Woodley, J. I. Gransden, P. Chapman

Leap Ahead 52 cal Artillery System

Lightening Strike An Indirect Fire Concept Utilizing Combustion Light Gas Gun (CLGG) Technology to Achieve Extreme Ranges

Defense Technical Information Center Compilation Part Notice

Insensitive Propulsion Systems for Large Caliber Ammunition. Beat Vogelsanger, Alexander Huber, and Heinz Jaskolka

XM1128 Insensitive Munition High Explosive Base Burn Projectile

Caseless Ammunition & Advances in the Characterization of High Ignition Temperature Propellant

45th Annual Armament Systems: Gun and Missile Systems Conference & Exhibition Event #0610 May 17-20, 2010 Dallas, Texas

Flight and Terminal Ballistic Performance Demonstration of a Gun-Launched Medium Caliber Ramjet Propelled Air Defense Projectile

NDIA 2010 Numerical Prediction of Large Caliber Cannon Impulse. Bob Carson Mechanical Engineer Fluid Dynamics Analyst Date: 19 May 2010

High Performance BKNO 3 Igniter Formulations

Shock tube based dynamic calibration of pressure sensors

INTEGRATED HYDRO-MECHANICAL SIMULATION OF A CAM-ROCKER ARM-UNIT INJECTOR SYSTEM TO ADDRESS NOISE AND VIBRATION ISSUES

60 MM MAPAM ADVANCED MORTAR ROUND

ROTATABLE CLAMP FOR BALLISTIC TESTING OF FABRIC

ELBIT SYSTEMS - LAND AND C 4 I. ATMOS 155mm truck-mounted howitzer for increased mobility and enhanced firing capabilities

Development of a 12.7 mm Limited Range Training Ammunition (LRTA)

8 th International Symposium TCDE Choongsik Bae and Sangwook Han. 9 May 2011 KAIST Engine Laboratory

SOFT RECOVERY SYSTEM FOR 155MM PROJECTILES A. Birk 1, D. Carlucci 2, C. McClain 3, N. Gray 2

Insensitive Munitions: Pyrotechnics Substitution for Explosives at Lake City or How ATK has paid its PWRFEE

A SUCCESSFUL EUROPEAN COOPERATION POWERFUL & COMPACT 40 CTAS CASED TELESCOPED ARMAMENT SYSTEM

Comparing FEM Transfer Matrix Simulated Compressor Plenum Pressure Pulsations to Measured Pressure Pulsations and to CFD Results

Adams-EDEM Co-simulation for Predicting Military Vehicle Mobility on Soft Soil

Alliant Ammunition Systems Company LLC. Advanced Medium Caliber HEI Ammunition -Mechanically Fuzed and Delay Initiated. Presented by Mr.

Dust explosions using AUTODYN

On Ignition Delays in Pressure Cartridges with Loosely Packed Energetic Materials Hobin S. Lee Chemring Energetic Devices, Torrance, CA 90505

# Gun Tube Wear Reduction for 105 mm Artillery

Development of Electrically Controlled Energetic Materials for 120mm Tank Igniters

155-mm Howitzer Malfunction Investigation: A Laboratory Study of the Igniter Train Operation

Modeling of the 35-mm Rarefaction Wave Gun

Seeing Sound: A New Way To Reduce Exhaust System Noise

Modeling of the 105-mm Rarefaction Wave Gun

TEST BENCH FOR ACTIVATABLE BATTERIES

Cavitation CFD using STAR-CCM+ of an Axial Flow Pump with Comparison to Experimental Data

DESIGN OF ACTIVE FLOW CONTROL AT THE WING/PYLON/ENGINE JUNCTION

Adaptation of Existing Fuze Technology to Increase the Capability of the Navy s 2.75-Inch Rocket System

XM mm PROXIMITY FUZE EXPLOSIVE TRAIN DESIGN

THE EFFECTS OF IGNITER DESIGN ON THE INTERIOR BALLISTIC PERFORMANCE OF DETERRENT COATED PROPELLANTS

Joint Services Environmental Management (JSEM) Conference

NSWC / Dahlgren Division

New Indirect Fire Capabilities from Industry Cooperation

Product Data Sheet WokaStar Series Advanced Liquid-Fuel HVOF Spray Guns

POSIBILITIES TO IMPROVED HOMOGENEOUS CHARGE IN INTERNAL COMBUSTION ENGINES, USING C.F.D. PROGRAM

Whither Diesel? An Overview of Combustion Concepts and Research Directions for Compression Ignition Engines

The Effects of Igniter Design on the Interior Ballistic Performance of Deterrent Coated Propellants

Artillery Projectiles, Fuzes and Propellants. By: God of War

Improving knowledge of tactical rocket motor response under Insensitive Munitions threats IMEMTS PORTLAND - April 2018

SMALL ARMS AMMUNITION

The graph shows how far the car travelled and how long it took. (i) Between which points was the car travelling fastest? Tick ( ) your answer.

Inventor Fred W. Watson. Jr. NOTICE

CFD Simulation of Dry Low Nox Turbogas Combustion System

Does V50 Depend on Armor Mass?

An Evaluation of Active Knee Bolsters

History Dr. Richard Passamaneck- Inventor

Improved IM Response for Future 2.75 APKWS Rockets with Composite Case Technology

Innovative Designs to Improve Medium Calibre Ammunition Effectiveness. Parari Eelko van Meerten

Analytical and Experimental Evaluation of Cylinder Deactivation on a Diesel Engine. S. Pillai, J. LoRusso, M. Van Benschoten, Roush Industries

Porsche Engineering driving technologies

EU INTERREG CEREEV. Fuel Spray and Mixture Preparation in Split- Cycle Engine

MP-100-APS. Flame Spray Technologies SprayTech. Multi-Process Thermal Spray Centre

Universal Dual Safe Training Fuze For Mortars. Presented by: Michael De Gregorio Prepared by: Michael De Gregorio and Eugene Mogendovich

CFD Flow Analysis and Optimization of Exhaust Muffler

Integrated Simulation Technologies Pvt Ltd

Premixed combustion of blends of n-heptane and gasoline in a rapid compression machine

Comparative study of the flow within water mist and sprinkler fire protection systems by means of CFD

Experimental Testing of a Rotating Detonation Engine Coupled to Nozzles at Conditions Approaching Flight

RNLA IFV Firepower. 30 mm versus 35 mm 35 mm KETF Firing doctrine

IMPROVING BOILER COMBUSTION USING COMPUTATIONAL FLUID DYNAMICS MODELLING

A Guide to the Carriage. by Road of Detonators. with Blasting Explosive Substances

LD24 SOLID FUEL RAMJET (SFRJ) PROPULSION FOR ARTILLERY PROJECTILE APPLICATIONS CONCEPT DEVELOPMENT OVERVIEW

UNCLASSIFIED FY Exhibits Schedule Prior Years FY 2013 FY 2014 FY 2015 Base FY 2015 OCO FY 2015 Total. Total Cost ($ M)

Component and System Level Modeling of a Two-Phase Cryogenic Propulsion System for Aerospace Applications

Pyro-MEMS Technological breakthrough in fuze domain Fuze Conference 2011

Increasing Low Speed Engine Response of a Downsized CI Engine Equipped with a Twin-Entry Turbocharger

40mm Infantry Grenade Fuzes

Emissions predictions for Diesel engines based on chemistry tabulation

Unmanned Aircraft System (UAS) Engine Research at U.S. Army Research Laboratory

FLUID DYNAMICS TRANSIENT RESPONSE SIMULATION OF A VEHICLE EQUIPPED WITH A TURBOCHARGED DIESEL ENGINE USING GT-POWER

POWERTRAIN SOLUTIONS FOR ELECTRIFIED TRUCKS AND BUSES

20 x 102 Mk244 APDS. (Armor Piercing Discarding Sabot)

Stopping distance = thinking distance + braking distance.

Dual Fuel Engine Charge Motion & Combustion Study

AECC Clean Diesel Euro 6 Real Driving Emissions Project. AECC Technical Seminar on Real-Driving Emissions Brussels, 29 April 2015

PRODUCT OPTIMIZATION SUPPORT 40 MM HV ABM. Federica Valente, H. Huisjes, T. Soullié, A. M. Kruse

Holistic Energy Analysis of Various Drivetrain Topologies Close to Reality

European GT-SUITE Conference 2009 page 1. European GT-SUITE Conference Frankfurt, State-of-the-art and Future Requirements for

Planned Revisions to the NIJ Ballistic Resistant Body Armor Test Standard

Statement of Jim Schoppenhorst, Director, DD(X) BAE Systems / Armament Systems Division. Before the

Saft s Xcelion 6T 28V Lithium Ion Battery for Military Vehicles

Advancements in PAR modelling: Major results of a national project performed at RWTH Aachen and JÜLICH

Modeling a Phlegmatized Diesel-Engine in a Hybrid Electric Vehicle Using a Transient Predictive Model Michael Auerbach, October 25th, 2010, Frankfurt

Transcription:

Modelling the Ignition of Modular Charges Clive Woodley & Steve Fuller A presentation to: 42 nd Guns & Missiles Conference April 2007 QinetiQ/D&TS/WPNS/PUB0701309

Contents 01 Background 02 Validation 03 Simulations 04 Conclusions & future work 2

01 Background 3

01 Charge design why UPCS? Existing inventory replaced with 1 module 4

01 Charge design advantages of UPCS Current charges Not fully IM compliant Not cleared for A1/C2 climatic conditions Wasteful decremental system Costly & L10 can t routinely be used for training Often remain in WMR until they life out With UPCS Same charges are used in training as are deployed for war fighting Training simplified/more realistic Substantial cost savings can be achieved through incremental system Logistic burden reduced Autoloader compatible 5

01 Modular charges the problem being addressed Safety & performance are important requirements linked to ignition Pressure waves eliminated or minimised and consistent Simultaneous ignition along length of charge Combustible cartridge cases present barrier to flamespread along the propellant bed Modules act as projectiles! Pressure difference (MPa) 30 20 10 0-10 -20 0 5 10 15 20 25 Time (ms) 6

01 Modelling approach - QIMIBS 2D mortar code Developed initially with MOD funding Developed further using QinetiQ funding Details presented at 22 nd International Symposium on Ballistics Ability to represent internal solid boundaries 7

02 Validation 8

02 Primer only single module initial geometry 9

02 Primer only single module Pressure (MPa) 0.25 0.20 0.15 0.10 0.05 0.00 QIMIBS P1 QIMIBS P2 Round 1 P1 Round 1 P2 0 2 4 6 8 10 Pressure (MPa) 0.40 0.35 0.30 0.25 0.20 0.15 0.10 0.05 0.00 QIMIBS P1 QIMIBS P2 Round 4 P1 Round 4 P2 0 2 4 6 8 10 Time (ms) Time (ms) 1.43g black powder Max velocity measured: 1.5m/s Max velocity predicted: 3.2m/s 1.25g NC Max velocity measured: 2.0m/s Max velocity predicted: 5.0m/s Correct trend predicted for pressure and module velocity Module velocities overpredicted but no account taken of sliding resistance 10

02 5 modules - flamespread Time of first visible light (ms) 6 5 4 3 2 1 0 Test 1 Test 2 Simulation 0 0.2 0.4 0.6 0.8 1 Distance from breech (m) 11

03 Simulations 12

03 Simulations Single module Igniter mass & location Flash tube diameter & vent hole size Three modules Five modules 13

03 Single module igniter mass (5g top, 15g bottom) 0.5ms 1.0ms 14

03 Single module igniter mass (5g top, 15g bottom) 1.5ms 2.0ms 15

03 Single module igniter mass (5g top, 15g bottom) 2.5ms 3.0ms 16

03 Single module igniter mass (5g top, 15g bottom) 3.5ms 4.0ms 17

03 Single module igniter mass (5g top, 15g bottom) 4.5ms 5.0ms 18

03 Single module igniter mass (5g top, 15g bottom) 5.5ms 6.0ms 19

03 Single module igniter mass (5g top, 15g bottom) 6.5ms 7.0ms 20

03 Single module igniter mass 1800 1600 Temperature (K) 1400 1200 1000 800 600 400 200 5g P6 5g P5 5g P4 15g P6 15g P5 15g P4 0 5 10 15 Time (ms) 21

03 Single module effect of igniter position 1800 1600 1400 Outside P6 Outside P5 Outside P4 Inside P6 Inside P5 Inside P4 1800 1600 1400 Outside P6 Outside P5 Outside P4 I/O P6 I/O P5 I/O P4 Temperature (K) 1200 1000 800 600 400 200 Temperature (K) 1200 1000 800 600 400 200 0 0 2 4 6 8 10 12 14 16 0 0 2 4 6 8 10 12 14 Time (ms) Time (ms) Outside = outside module but inside flash tube Inside = inside module but outside flash tube Modelling indicates better ignition if igniter material is both sides of the flash tube 22

03 Single module effect of flash tube diameter 1600 1400 52mm P6 52mm P5 52mm P4 26mm P6 26mm P5 26mm P4 1400 1200 20mm P6 20mm P5 20mm P4 26mm P6 26mm P5 26mm P4 Temperature (K) 1200 1000 800 600 Temperature (K) 1000 800 600 400 400 200 0 2 4 6 8 Time (ms) 200 0 1 2 3 4 5 6 7 8 Time (ms) Modelling indicates better ignition for 26mm flash tube diameter 23

03 Single module effect of flash tube hole size 1400 1200 14mm P6 14mm P5 14mm P4 10mm P6 10mm P5 10mm P4 1400 1200 6mm P6 6mm P5 6mm P4 10mm P6 10mm P5 10mm P4 Temperature (K) 1000 800 600 Temperature (K) 1000 800 600 400 400 200 0 2 4 6 8 Time (ms) 200 0 2 4 6 8 Time (ms) Modelling indicates better ignition for 6mm flash tube holes 24

03 Three modules initial geometry 25

Temperature (K) QinetiQ Proprietary 03 Three modules 10g black powder per module 1800 1600 1400 1200 1000 800 600 400 200 P1 P2 P3 P6 P5 P4 0 2 4 6 8 10 12 Time (ms) Taking 600K as the propellant ignition temperature, propellant in 2 nd & 3 rd modules ignited 0.8ms & 1.7ms after the 1 st module Temperature (K) 1800 1600 1400 1200 1000 800 600 400 200 P9 P8 P7 P12 P11 P10 0 2 4 6 8 10 12 Time (ms) Use another internal ballistics code to predict pressure waves 26

03 Five modules initial geometry 27

03 Five 10g black powder per module Temperature (K) 1800 1600 1400 1200 1000 800 600 400 200 P1 P2 P3 P6 P5 P4 0 2 4 6 8 10 12 14 Time (ms) Igniter in last module not ignited Module 2 might ignite first Taking 600K as the propellant ignition temperature, propellant in 2 nd, 3 rd & 4 th modules ignited 1ms, 2ms & 5ms after the 1 st module use another internal ballistics code for ΔP Temperature (K) Temperature (K) 1800 1600 1400 1200 1000 800 600 400 200 1600 1400 1200 1000 800 600 400 200 P9 P8 P7 P12 P11 P10 0 2 4 6 8 10 12 14 Time (ms) P15 P14 P13 P18 P17 P16 0 2 4 6 8 10 12 14 Time (ms) 28

04 Conclusions & future work 29

04 Conclusions & further work QIMIBS has much of the functionality required to model MCS Validated for two primers for 1 & 5 modules Parameter studies showed 5g black powder per module not likely to ignite Best position of igniter is both sides of flash tube 26mm diameter flash tube better than 52mm and 20mm Reducing flash tube vent area predicted to produce better ignition Predictions for 5 modules show Primer and igniter insufficient to ignite (5 th ) module adjacent to the projectile Module 2 might ignite before module 1 Possibility of significant ignition delay for 4 th module 155mm gun firings planned & further modelling Conclusions likely to be very dependent on primers and geometries used in this study 30