Methodology for Dynamic Characterization of Fragmenting Warheads

Similar documents
NDIA Armaments Forum Indianapolis, Indiana

AVAL GENERAL PRODUCT INFORMATION ASSESSMENT OF VULNERABILITY AND LETHALITY A TRI-SERVICE VULNERABILITY / LETHALITY SIMULATION TOOL

Methodology and Results of a Safe Separation Study for Navy 5-Inch Projectiles

52 nd FUZE CONFERENCE. Presented by: Mr. Perry Salyers

FRAPPE - Multi-Function Fuze

System Modeling of a 40mm Automatic Grenade Launcher

SPACIDO 1D Course Correction Fuze 51st Annual Fuze Conference May 22-24, 2007 Nashville. Benjamin CAMPION. THALES Munitronics & Microtechnics

Curvilinear trajectory and smart fuze calculations suitable for hard target defeat modeling

Canadian Fuze Program. F. Côté and E. Gagnon TTCP TP-7 Workshop on Fuzes Kansas City, MO, 14 May 2010

40 MM x 53 AIR BURST MUNITION FOR AUTOMATIC GRENADE LAUNCHERS

ACCURACY MODELING OF THE 120MM M256 GUN AS A FUNCTION OF BORE CENTERLINE PROFILE

Electronic Safety and Arming Device for the 105 mm STAR ATO Demonstration

2012 NDIA Joint Armaments Conference. Characterizing Precision with Radial Miss Distance. Jon Peoble Dan Tulloh May 16, 2012

Modeling the Interaction of a Laser Target Detection Device with the Sea

IM Fuze Design of Fuzing Systems for GUN LAUNCHED PROJECTILES

System Modeling for Projectile Design and Optimization Presented By : Phil Brislin

Hazard and Risk Modelling for Weapon Danger Areas

3D simulations of concrete penetration using SPH formulation and the RHT material model

The Impact of High Accuracy Target Geometry in Modeling and Simulation to Support Live-Fire Test & Evaluation

MIL-STD-1760 DIGITAL LAUNCHER FOR NAVY/MARINE CORP 2.75-INCH ROCKET SYSTEM. Naval Surface Warfare Center, Indian Head Division

Determination of Naval Gun System Firing Patterns to Combat Manoeuvring Surface Targets

Development of a Soft Recovery System of Supersonic Projectiles

Analysis of the effect of target scattering on the operational effectiveness of seeker

A Framework for Vulnerability/Lethality Modeling and Simulation National Industrial Association 47 th Annual Fuze Conference April 10, 2003

ENHANCED FRAGMENTATION MODELING

Trajectory Matching Procedure/Practice for a Guided Projectile using MATLAB/Simulink

MSIAC Engineering Tools and Databases

AA Simulation: Firing Range

Coupled numerical-experimental study of an armour perforation by the armour-piercing projectiles

Test Options & Analysis Techniques:

DISTRIBUTION STATEMENT A Approved for Public Release Distribution Uniimited

AVAL 6.6. User's Manual

Simulating Underbelly Blast Events using Abaqus/Explicit - CEL

SENSITIVITY OF PROJECTILE MUZZLE RESPONSES TO GUN BARREL CENTERLINE VARIATIONS. Michael M Chen

AIR FORCE INSTITUTE OF TECHNOLOGY

III. TESTING AND IMPLEMENTATION

Maneuver Strategy in Beyond-Visual-Range Air Combat

Design and Implementation of an Inertial Measurement Unit (IMU) for Small Diameter Ballistic Applications

VERIFICATION AND VALIDATION PLAN FOR THREE-DIMENSIONAL PROBABILITY F INCAPACITATION METHODOLOGY MASONRY STRUCTURES (3DPIMMS)

Arrow Tech Course Catalog

Shrapnel Impact Probability and Diagnostic Port Failure Analysis for LLNL s Explosives Testing Contained Firing Facility (CFF)

PROJECTILE MOTION PURPOSE

THE EVOLUTION AND APPLICATION OF ASYMMETRICAL IMAGE FILTERS FOR QUANTITATIVE XCT ANALYSIS

~ Materiel Test Procedure

MAPPING EXPLOSIVE SAFETY HAZARDS (MESH) IN A GIS ENVIRONMENT: A PROGRAM UPDATE

Precision Strike SPO

Using SUE to reduce Delays and Disruptions on City of Toronto s Yonge Street Project

Development of Hoisting Load Position Sensor for Container Handling Cranes

PROJECTILE. 5) Define the terms Velocity as related to projectile motion: 6) Define the terms angle of projection as related to projectile motion:

TURBOPK USER MANUAL. March Patrick Buckley. SURVICE Engineering LLC

Targeting and Geolocation Accuracy / Electromagnetic Railgun Instrumentation

Keywords: Coanda effect, perforations, wellbore, formation, etc.

Projectile Motion. A.1. Finding the flight time from the vertical motion. The five variables for the vertical motion are:

NDIA 43 rd Annual Armament Systems: Gun and Missile Systems Conference & Exhibition. April 21-24, 2008

Purpose of the experiment

Using MODTRAN for Atmospheric Parameter Retrieval under the ASCOPE Architecture

HIGH-SPEED THEE-DIMENSIONAL TOMOGRAPHIC IMAGING OF FRAGMENTS AND PRECISE STATISTICS FROM AN AUTOMATED ANALYSIS

Simulation. Variance reduction Example

CM and DM Support to the Modeling and Simulation Process Support to Systems Engineering Functions

PRODAS Newsletter. Announcing the Release of PRODAS Version 3.6. MATLAB/Simulink Trajectory Module

Small Arms Grenade Munition Integration & Demonstration

1. FY2017 Review 2. FY2018 Action Plan 3. FY2018 FY2020 Mid-Range Plan

ABSTRACT 1. INTRODUCTION

Predictions of projectile penetration and perforation by DAFL with the free surface effect

Summary. Introduction

Missile Simulation in Support of Research, Development, Test Evaluation and Acquisition

DTRA Counter WMD Technologies Fuzing & Instrumentation Technology Overview Presented at 54th Annual NDIA Fuze Conference May 2010

Abstract number: Dynamic High g-shock Fuze Testing with support of a Reverse Ballistic Gun & Sled Track. TDW, Christian Euba

A Methodology for the Generation, Storage, Verification and Validation of Performance Data for Modelling and Simulation

qbal - v1.06 User Manual

07ATC 22 Image Exploitation System for Airborne Surveillance

Weight And Reliability Optimization Of A Helicopter Composite Armor Using Dynamic Programming

OCR Maths M2. Topic Questions from Papers. Projectiles

THREE-DIMENSIONAL ANALYSIS OF THE EXPLOSIVE INITIATION THRESHOLD FOR SIDE IMPACT ON A SHAPED CHARGE WARHEAD

TurboPK. Figure 1. Example TurboPk run.

A Practical Adaptive Proportional-Derivative Guidance Law

A400M. Flares trajectories calculation from a chase aircraft

A METHOD TO INCREASE THE TIP VELOCITY OF A SHAPED CHARGE JET. William P. Walters and Daniel R. Scheffler

Memorandum. Clint Slatton Prof. Brian Evans Term project idea for Multidimensional Signal Processing (EE381k)

L 5 Seismic Method. Courtesy of ExxonMobil. Mitchum et al., 1977b

ARDEC Fuze S&T Overview Joint Armaments Form & Exhibition Phoenix Convention Center May 15, 2014

T114E3 indicates the third modification to the development fuze number 114. Mk 415Mod3 indicates the third modification to the fuze mark number 415.

(40-455) Student Launcher

Lesson 3.1 Vertices and Intercepts. Important Features of Parabolas

ASNT Conference

EECS 428 Final Project Report Distributed Real-Time Process Control Over TCP and the Internet Brian Robinson

Referred Deflection. NOTE: Use 2800 and 0700 to avoid any sight blocks caused by the cannon. Figure Preparation of the plotting board.

Analysis of Vehicle Door Closing Effort Dimensional Issues

Computer Simulation on Structural Plane of Ore-rock By Monte-Carlo Method Pan Dong 1,2, a, Li XiBing 1,b, WangYu 1, c

Radar Tomography of Moving Targets

/DDD. Stypes. JUL 103 ;il BEST AVAILABLE COPY. 1 July 1971 Materiel Test Procedure Aberdeen Proving Ground

Vector Decomposition

Trajectory Planning for Reentry Maneuverable Ballistic Missiles

(ii) Calculate the maximum height reached by the ball. (iii) Calculate the times at which the ball is at half its maximum height.

Industrial Energy Efficiency

Recitation 1-6 Projectile Motion

Tracking Trajectories of Migrating Birds Around Tall Structures

ICSI Addressable Disconnect Tool (ADT) Overview

9.8 Application and issues of SZ phase coding for NEXRAD

COMPUTATIONAL AND EXPERIMENTAL INTERFEROMETRIC ANALYSIS OF A CONE-CYLINDER-FLARE BODY. Abstract. I. Introduction

Transcription:

Methodology for Dynamic Characterization of Fragmenting Warheads Jason Angel - U.S. Army Research Laboratory April 22, 2008 Guns & Missiles symposium New Orleans, LA

OUTLINE BOTTOM LINE UP FRONT 1 - PROPOSED METHOD TO ASSESS FRAGMENTATION FOR DYNAMIC EVENT 2 QUESTIONING EXISTING METHODOLOGY FOR FRAGMENTATION LETHALITY Background/Issues Approach Test Set-up Results/discussion Conclusions

BACKGROUND/ISSUES CURRENT METHOD TO ASSESS FRAGMENTATION Static ARENA test Statistical representation of the fragmentation Fragmentation File (Z-data file) Lethality models use Z-data and dynamic impact conditions Impact velocity, orientation, etc Predict number of impacts on personnel α V i Determine probability of incapacitation, P I HOB Flight Trajectory Currently no method to correlate to Dynamic testing just a probability of achieving a level of Incapacitation

GMLRS as an EXAMPLE Z-data file established P I for impact condition computed Performed dynamic event mannequins assessed for lethality all personnel fell within bands (P I +/-) ISSUE - no statistical correlation to fragment spray

APPROACH Goal: Demonstrate method to collect fragmentation data in a dynamic event to produce higher statistical confidence in results Evaluation Concept: Use warhead with well established Z-data file Collect fragment spray via metallic witness panels located in an arena arrangement Compare perforations in the panels from the detonated warheads to those predicted using the static arena file Static event no projectile velocity, serves as a baseline Dynamic event - incoming velocity will be applied

TEST ARTICLES 105mm HEP round inventory since 1970s new Z-data file recently produced Metallic Witness panels Statically detonated from Platform One side of Panel Arrangement

TEST OVERVIEW Test Setup: Collect fragmentation with metallic panel array in arena Dynamic fire 105mm HEP projectile through wood to detonate Static statically detonate HEP projectile Measurements: Panel array surveyed prior to test Photograph panels, use image software to record position of impacts Dynamic use radar and video to determine impact velocity and location of warhead when it burst High Speed Video Cameras Radar #1 #2 #3 1-12 Firing Platform Bursting Board 13-25 Panel Array & Camera Configuration 1/32 Mild Steel Panels

TEST RESULTS - STATIC

TEST RESULTS - DYNAMIC

TEST RESULTS Test Number Detonation Condition Velocity Muzzle/Striking (m/s) Test Objective Result 1 Dynamic LOST Verify fuze function on the selected target material. Proper fuze function 2 3 4 5 7 8 9 11 Dynamic Dynamic Dynamic Dynamic Dynamic Dynamic Static Static 759 / 746 763 / 751 758 / 744 758 / 747 754 / 744 762 / 749 N/A N/A Verify fuze function on the selected target material Collect dynamic distribution of fragments from the witness panels Collect dynamic distribution of fragments from the witness panels Collect dynamic distribution of fragments from the witness panels Collect dynamic distribution of fragments from the witness panels Collect dynamic distribution of fragments from the witness panels Collect static distribution of fragments from the witness panels Collect static distribution of fragments from the witness panels Proper fuze function All Evaluated a 90 o Attack Angle and 0 o Azimuth

TEST RESULTS Test Number Detonation Condition Velocity Muzzle/Striking (m/s) Test Objective Result 2 Dynamic 774 / 761 Collect dynamic distribution of fragments from the witness panels 3 4 Dynamic Dynamic 761 / 749 759 / 746 Collect dynamic distribution of fragments from the witness panels Collect dynamic distribution of fragments from the witness panels 5 Static N/A Collect static distribution of fragments from the witness panels 6 Static N/A Collect static distribution of fragments from the witness panels All Evaluated a 90 o Attack Angle and 0 o Azimuth

DATA REDUCTION Dynamic shot Panel Array 1 3 10m 8 25 5m 13 12 Panel 4 2.4 2.2 2 1.8 1.6 Distance (m) 1.4 1.2 1 0.8 0.6 0.4 0.2 0 0 0.2 0.4 0.6 0.8 1 1.2 Distance (m)

PREDICTED FRAGMENTATION 270 degrees PANELS 1-12 ACTUAL PANEL POLAR ANGLE 180 degrees POLAR ANGLE 0 & 360 degrees PANELS 13-25 90 degrees POLAR ANGLES DEFINED

Normalized # of Impacts on Panels 1.0 0.8 0.6 0.4 0.2 STATISTICAL ANALYSIS (STATIC) R R*2 Ave Impacts Estimated Impacts (with 3 sigma STND DEV) 0.0 Polar Angle (0-front of Warhead) FRONT REAR FRONT

STATISTICAL ANALYSIS (STATIC) Good Correlation Between the Mean Static Estimate and The Mean Recorded Value. GOOD AGREEMENT BETWEEN ESTIMATED & ACTUAL

Normalized # of Impacts on Panels 1.0 0.8 0.6 0.4 0.2 STATISTICAL ANALYSIS (DYNAMIC) R R*2 Ave Impacts Estimated Impacts (with 3 sigma STND DEV) 0.0 Polar Angle (0-front of Warhead) FRONT REAR FRONT

STATISTICAL ANALYSIS (DYNAMIC) Overestimate of fragments in the beam spray. Underestimate of fragments in the nose and tail regions. NOT AS GOOD AGREEMENT BETWEEN ESTIMATED AND ACTUAL

SUMMARY Static evaluation - good agreement Dynamic estimates show less fragments in the front Implications of differences in results Interaction of warhead expansion with wood during the dynamic detonation Parasitic debris from warhead is hitting panels in front for dynamic event Accuracy of fragment velocities of Z-data file more of an effect on dynamic event - May need a new format for Z-data (3-dimensional) Need to evaluate other warheads under same controlled conditions to prove theory

CONCLUSIONS Method collects data over a much larger range than previously gathered for dynamic events This wider area results in a much greater confidence in verifying performance of fragmenting warhead Review Current Z-data (arena) methodology SUGGESTIONS: 1) Add metallic witness panels on Live-Fire evaluations 2) Include an intermediate evaluation with metallic witness panels prior to Live-Fire evaluations 3) Review fragmentation Evaluation methodolgy

BOTTOMLINE DEMONSTRATED SIMPLE METHOD THAT VERIFIES THE OVERALL SPREAD OF FRAGMENTS IN DYNAMIC EVENT OBSERVED ISSUES WITH CURRENT Z-DATA FILE METHODLOGY QUESTIONS????