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    An advanced weapon and space systems company

    1APPROVED FOR PUBLIC RELEASE OSR# 08-S-1194

    LW30mm (30 x 113mm) Spotter Charge Prototype

    2008 NDIA

    42nd Annual Armament Systems:

    Gun & Missile Systems Conference & Exhibition

    21 24 Apri l 2008

    New Orleans, LA

    Jim RothDesign EngineerMedium Caliber AmmunitionATK Medium Caliber SystemsPhone: 763-712-7722Email: [email protected]

    Contact info:

    Curtis FieldingATK Launch SystemsPEP, Research and DevelopmentPhone: 435-863-6188Email: [email protected]

    Fred StecherATK Advanced WeaponsWarheadsPhone: 763- 744-5117Email: [email protected]

    Dan NielsonATK Launch SystemsOrdnance&EnergeticsPhone: 435-863-6687Email: [email protected]

    APPROVED FOR PUBLIC RELEASE OSR# 08-S-1194

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    An advanced weapon and space systems company

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    Background and Need

    Technical Approach

    ATK Testing

    Testing at Ft. Rucker

    Acknowledgements/Contacts

    Questions & Answers

    LW30mm Spotter Charge - Outline

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    LW30 Ammunition 30mm X 113mm

    M789 HEDP

    High Explosive Dual Purpose

    M788 TP

    Training Projectile matched to M789

    Length (max): 113 mmWeight: 343 gProjectile Mass: 234 g

    Muzzle Velocity: 805 m/sMax Range: ~ 3000 mDispersion: 1.35 mils

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    30mm M230 Chain Gun Automatic Cannon

    Caliber: 30mm X 113mm - LW30 Linkless

    Max Range: ~ 4000 meters

    Rate of Fire: 625 25 Shots per Minute

    Platforms:

    AH-64 / AH64A Apache Attack Helicopters

    MH-60 Variants - SOAR

    Targets:

    Light Armored Vehicles

    Deployed Infantry

    M230 Weapon System

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    LW30mm Spotter Charge IRD Schedule Challenge

    Phase 1 Preliminary

    Design(Test 2457)

    Phase 2 DetailedDesign

    (Test 2465)

    Phase 3

    Build and Test(Ft. Rucker Demo)

    Approx. 8 month schedule from Concept Definition to Govt Demo

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    An advanced weapon and space systems company

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    LW30 Spotter Charge ATK Team

    ATK Medium

    Caliber Systems(Ammunition & Gun

    Design, Chem/Met Lab)

    ATK Launch

    Systems(Spotter Material /

    Candidate Selection)

    ATPG(Load, Test and

    Evaluation)

    ATK Advanced

    Weapons(CTH modeling,ANSYS, Rapid

    Prototype)

    LW30 Spotter

    ChargeDevelopment

    Ammunition

    Systems

    Radford(Cartridge Hardware)

    ATK Tactical

    Propulsion and

    Controls (ABL)

    (Projectile Hardware)

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    Spotter Charge Design Challenges

    M788 TP Projectile Velocity vs. Range

    0

    100

    200

    300

    400

    500

    600

    700

    800

    900

    0 500 1000 1500 2000 2500 3000 3500Range (m)

    Velocity

    (m/s)

    Solid AL NoseSteel Body

    Marking Material

    Hollow AL Nose

    Potential Spotter Fill

    Potential Spotter Fill

    Short-rangedemonstration 05

    Desired range for demonstration

    Impact velocity and target media are key parameters for Spotter Design

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    Material Selection Approach

    Technical:

    Approach driven by the desired capabilityrequirements

    Key challenges: Spotter material sensitivity

    against soft ground target and reaction againstplywood

    Schedule

    Off the shelf material currently in use at ATK-LS

    Castable material due to time constraints of loadtooling and integration with projectile geometrychanges

    Selection

    Identified 3 initial material candidates to beevaluated in ballistic capability testing

    Down selected to most viable materials forhighest probability of success on target media

    ID Description

    X-9 Magnesium powder

    Strontium Nitrate (Red

    marker)

    ATK-LS proprietary binder

    X-5 ATK-LS proprietary Flareformulation

    Potassium perchlorate

    X-8 Magnesium powder

    Sodium Nitrate (Whitemarker)

    ATK-LS proprietary binder

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    Spotter Charge Projectile Assy Configurations Phase 1

    M759 Ogive

    M759 Probe

    Cap

    M789 BodyCastable spotter material

    -101 , -102, -103

    Base Plug

    Spotter Material in Projectile Body & Nose Assembly

    Spotter Material in & Nose only

    To address the aggressive

    schedule for demonstration,

    existing M788 or M789 projectile

    hardware will be used or altered

    to accommodate spotter material

    cast loading.

    As-mixed

    Dispensing guninto Projectiles

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    PRODAS Modeling for Ballistic Match to M788/M789

    Baseline M789 Model in PRODAS Library

    Baseline M788 Model in PRODAS Library

    Initial LW30 Spotter Charge Model

    Projectile Assy (grams) -Measured - All Samples Config 1 and Config 2

    LW30 Spotter Charge Demonstration Projectile Build

    215

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    Serial Number

    Mass(grams)

    Spotter ChargePrototype Projectile

    Mass~222 grams

    M788 / M789 ProjectileMass 234 grams typical

    PRODAS Trajectory Comparison for 1500m &3000m

    1500m: QE 31.4 Gunners Mils

    3000m: QE 148.8 Gunners Mils

    Muzzle Velocity 805 m/sec for all projectiles

    0

    50

    100

    150

    200

    250

    300

    0 500 1000 1500 2000 2500 3000

    Range (m)

    Altitude(m)

    M788 TP Baseline

    Design 4 LW30 Spotter DL-Q219

    M788 TP Baseline (Muz Vel 805m/sec)

    Design 4 LW30 Spotter DL-Q219 (MuzVel 805 m/sec)

    Trajectory at 3000m short for same QE and 805m/s muzzle velocity; increase MV to attain

    match for spotter to 3000m

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    An advanced weapon and space systems company

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    PRODAS Trajectory Comparison for 1500m - QE 31.4 Gunners MilsMuzzle Velocity 805 m/sec

    Muzzle Velocity 833 m/sec for match to 1500 for Design 4 (~220 gram projectile)

    0

    5

    10

    15

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    0 100 200 300 400 500 600 700 800 900 1000 1100 1200 1300 1400 1500

    Range (m)

    Altitude

    (m)

    M788 TP Baseline (MuzVel 805 m/sec)

    Design 4 LW30 SpotterDL-Q219 (Muz Vel 805m/sec)

    Design 4 LW30 SpotterDL-Q219 (Muz Vel833m/s)

    Ballistic Match PRODAS Trajectory Plots for 1500m

    M788 at Standard

    temp conditions,QE#1

    For same QE set for M788,trajectory of spotter if targetingsame muzzle velocity

    Spotter at Standardtemp conditions,

    sameQE#1,increasedMuzzle Velocity

    PRODAS modeling used to establish muzzlevelocity needed to attain match to 1500mand 3000m.

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    ANSYS Stress Analysis for Ogive

    Von MisesStress (psi)

    Max. PrincipalStress (psi)

    Max. ShearStress (psi)

    Plastic Equiv.StrainC

    L

    InitialGeometry Ogive wall thickness will survive gun launch loads

    Ground Impact Trajectory Plots

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    An advanced weapon and space systems company

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    Ground Impact Trajectory Plots1500m / 2000m / 3000m Gun at 0 vs. Altitude

    Firing at Ground Elevation(Ft. Rucker Demo)

    Firing fromAltitude

    PRODAS Output for M788 TP

    Angle of impact at

    3000m similar forboth ground and

    altitude firingscenarios

    1500m 3000mShallow Angle of impact at1500m for ground firing

    CTH M d li f G d I t 1500

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    An advanced weapon and space systems company

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    CTH Modeling of Ground Impact 1500m

    DRY CLAY

    Time=3 sec Time=3sec

    Time=40 sec

    DRY CLAY

    Time=40 sec

    75 0 C

    14.5 ksi

    1500m test at Ft. Rucker fired from ground-mount will produce shallowangle of impact that will make it difficult to initiate spotter fill.

    (ksi)

    14.5

    1.45

    0.145

    (ksi)

    14.5

    1.45

    0.145

    (ksi)14.5

    1.45

    0.145

    (ksi)14.5

    1.45

    0.145

    PyrophoricfillCase

    CTH M d li f G d I t 3000

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    CTH Modeling of Ground Impact 3000m

    Time=3 usec

    Time=120 usec

    Pressure Fringes

    Temperature Fringes

    Time=3 usec

    Time=120 usec

    Increased angle of impact at 3000m may provide increased shear orthermal stress upon impact; however the impact velocity is reduced

    DRY CLAY

    (ksi)14.5

    1.45

    0.145

    (ksi)14.5

    1.45

    0.145

    (ksi)

    14.5

    1.45

    0.145

    (ksi)

    14.5

    1.45

    0.145

    1800

    C

    Pyrophoricfill

    Case

    2000 T t R t ATPG

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    An advanced weapon and space systems company

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    2000m Test Range at ATPG

    500 m

    2000 m

    2000m

    Gun Pad

    Target Area

    Aerial ViewSource: Google Earth

    View from high-speed camerato target

    ATPG Test Setup Photos Gun to Target

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    ATPG Test Setup Photos Gun to Target

    500m Gun Firing Position Viewpoint

    2000m Observation Viewpoint

    Target

    LW30mm Spotter Charge IR&D

    M788 TP Drift vs. Range - PRODAS Eval for Cross-Wind

    Firing at 2000m vs 16' wide RHA plate

    -12-10

    -8-6

    -4-202468

    10121416182022242628303234363840424446485052545658606264666870

    0 200 400 600 800 1000 1200 1400 1600 1800 2000

    Range (m)

    Drift(ft)

    0 cross-wind-10mph cross-wind

    -5mph cross-wind

    -3mph cross-wind

    +3mph cross-wind

    +5mph cross-wind

    PRODAS Modeling for cross-winds showed risk

    for missing test target at 2000m; thereforeconducted initial capability testing at 500m

    ATPG Hi h S d Vid 500 t ti i t t l t t

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    ATPG High Speed Video 500m testing against steel target

    Serial Number: 2-101-1Material:X5Projectile Config: Nose only9/4/07 (Frame 100)

    Serial Number: n/aHEDP baseline/ CartLot NRE07B001S9089/4/07 (Frame 150)

    Serial Number: 2-102-1Material:X-8Projectile Config: Nose only9/4/07 (Frame 140)

    Serial Number: 2-103-1Material:X-9Projectile Config: Nose only9/4/07 (Frame 50)

    ATPG High Speed Video 500m testing against steel target

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    ATPG High Speed Video - 500m testing against steel target

    Serial Number: n/aHEDP baseline/ CartLot NRE07B001S9089/4/07 (Frame 150)

    Serial Number: 2-103-2Material:X-9Projectile Config: Nose only9/4/07 (Frame 55)

    Serial Number: 6-103-1

    Material:X-9Projectile Config: Nose&Body9/5/07 (Frame 420)

    Serial Number: 6-103-2

    Material:X-9Projectile Config: Nose&Body9/5/07 (Frame 200)

    ATPG High Speed Video - 500m testing vs plywood target

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    An advanced weapon and space systems company

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    ATPG High Speed Video - 500m testing vs. plywood target

    These 2 tests were conducted at 500m with full propellant load andshow reaction on plywood in high-speed video, but not visible to unaided

    eye at gun (500m).

    When fired at 500m with 40% propellant load (simulating 1500m impact)there was no reaction seen on high speed video.

    Demonstration Test Plan Example of 27-Round test block

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    Demonstration Test Plan Example of 27-Round test block

    Day or

    Night

    Firing

    Distance

    Viewing

    Distance

    Apache Gunner

    View

    Apache Pilot

    View TargetConfig 1 Config 2

    Day 1 Day 1500m 1500m Unaided Unaided Steel X

    Day 1 Day 1500m 1500m Unaided Unaided Steel X

    Day 1 Day 1500m 1500m Unaided Unaided Steel X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Steel X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Steel X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Steel X

    Day 1 Day 1500m 1500m TADS FLIR Unaided Steel XDay 1 Day 1500m 1500m TADS FLIR Unaided Steel X

    Day 1 Day 1500m 1500m TADS FLIR Unaided Steel X

    Day 1 Day 1500m 1500m Unaided Unaided Plywood X

    Day 1 Day 1500m 1500m Unaided Unaided Plywood X

    Day 1 Day 1500m 1500m Unaided Unaided Plywood X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Plywood X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Plywood X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Plywood X

    Day 1 Day 1500m 1500m TADS FLIR Unaided Plywood X

    Day 1 Day 1500m 1500m TADS FLIR Unaided Plywood X

    Day 1 Day 1500m 1500m TADS FLIR Unaided Plywood X

    Day 1 Day 1500m 1500m Unaided Unaided Earth X

    Day 1 Day 1500m 1500m Unaided Unaided Earth X

    Day 1 Day 1500m 1500m Unaided Unaided Earth X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Earth X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Earth X

    Day 1 Day 1500m 1500m Day TV PNVS FLIR Earth X

    Day 1 Day 1500m 1500m TADS FLIR Unaided Earth X

    Day 1 Day 1500m 1500m TADS FLIR Unaided Earth XDay 1 Day 1500m 1500m TADS FLIR Unaided Earth X

    ATK Projectile Config

    3 TargetTypes

    Day &Night

    firing

    3 viewingscenarios

    1500 & 3000mviewing range

    1500 & 3000mfiring range

    Total of 170 cartr idges shipped for Demo

    LW30 Spotter Charge - Ft Rucker Demonstration Test Setup

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    An advanced weapon and space systems company

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    LW30 Spotter Charge Ft. Rucker Demonstration Test Setup

    Source: Google Earth

    3000m

    3000m

    Target

    Area

    1500m

    1500m

    TargetArea

    Fixed

    Gun Pad

    Location

    Apache

    viewingControltower

    ATK M230 LF Gun / ROI Raven system used at Ft. Rucker

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    An advanced weapon and space systems company

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    ATK M230 LF Gun / ROI Raven system used at Ft. Rucker

    3000m target

    1500m target

    Recon Optical's RAVEN R-400

    is used for common remotelyoperated weapon station(CROWS) program.

    Example of Steel Impact Day and Night Testing

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    Example of Steel Impact Day and Night Testing

    Camera #54

    Day Testing

    Camera #54

    Night Testing

    Summary

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    An advanced weapon and space systems company

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    Summary

    A prototype spotter charge for the 30x113mm LW30mm Ammunition family was

    evaluated against multiple target media and ranges of trajectory

    Modeling tools were used for analysis of mass properties, aeroballistic performance,stress analysis and impact thermal stress.

    PRODAS modeling provided ballistic match that was verified with radar tracking in ATK

    test. CTH hydrocode modeling indicated that predicted reaction of spotter material on ground

    impact would be marginal depending on impact angle and velocity.

    ANSYS stress analysis modeling provided design safety that was verified in structuralintegrity ballistic tests.

    Demonstration testing conducted at Ft. Rucker tracked with the results from ATKtesting:

    Reliable visible reaction when impacting Steel target, day and night at 1500m, and night at 3000m. Dayimpact at 3000 not available.

    Impact on Plywood target showed delay reaction behind target; at times was evident and scored by pilotas sufficiently visible allowing for adjustment. More evident at night.

    Limited frequency / Marginal short duration visible day / night when impacting ground at 1500m.

    3000m testing did not reliably impact visible target area due to drift from cross winds (PRODAS)

    Further development efforts on hold pending government evaluation of thedemonstration testing and updated User need assessment.

    Acknowledgements

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    Acknowledgements

    OPM-MASMaj. Glenn Dean

    Bill Wong

    Scott Bryan

    ARDEC

    John Hirlinger

    Jeff Darbig

    Rich Schrum

    Anthony CorteseDameon Gabriel

    Ft. Rucker

    Maj. Kevin BeldenBob Smithson

    Joe Webers

    CW3 Patrick Backmann

    ATK MCS Design

    Larry DoumaJim Lamb

    Linda Heuer

    Gary Wittmer

    Don GloudeVince Martinez

    Recon OpticalDoug Hagie

    ATK ATPG LAP

    John KraljicDennis Martinson

    Scott Larson

    Rich Johnson

    Clayton Weitnauer

    John KraljicTony Teale

    Sandy Ohotto

    George Berning

    Eric Severson

    ATK ATPG Test

    Bret George

    Dave Steffenhagen

    Don Newman

    Jim Raivala

    Cary Whetstone

    Tom Lorentz

    Joe Lamon

    Mike Cypher

    ATK MCS Programs / BDScott Teigen

    Rodney Ward

    Butch Nery

    Chris Stewart

    Ellis Clark

    Matt Berg

    ATK LSCurtis Fielding

    Dan Nielson

    Rick Tanner

    Steve Glaittli

    ATK AW

    Fred StecherWayne Hierlmaier

    Mark Krueger

    Dave Fehr

    ATK ABL

    Dave Starr

    Annette Staggs

    ATK AW

    Dave Geiss

    Dave Darden