AUSA TACTICAL MISSILES CONFERENCE

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AUSA TACTICAL MISSILES CONFERENCE DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.

Transcript of AUSA TACTICAL MISSILES CONFERENCE

Page 1: AUSA TACTICAL MISSILES CONFERENCE

AUSA TACTICAL MISSILES

CONFERENCE

DISTRIBUTION STATEMENT A: Approved for public release; distribution is unlimited.

Page 2: AUSA TACTICAL MISSILES CONFERENCE

Any Warfighter – Anywhere – All the Time… UNCLASSIFIED 2

Missiles

Rockets

Test Sets

AN/AVM-101A

TSGMS

Launcher

Test

Station

Longbow HELLFIRE

(MMW)

M260/M261Rocket Launchers

2.75-inch Hydra Rocket System

M279 Launcher

M299 Launcher

M272 Launcher

Fixed Wing

Launcher

Semi-Active

Laser HELLFIRE (SAL)

Small Guided Munitions

Joint Air-to-Ground Missile

Viper

Strike

Launchers

SALSTSMHUTS

Griffin

JAMS FAMILY OF PRODUCTS

Quad-Rail

(M299A1)

Dual-Rail

(M310A1)

UAS

(M801)

HELLFIRE VariantsF - A - K - N - M

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Aviation and Missile

Weapon System Technology

for Swift Decisive Victory

Without Casualties

JAMS STRATEGIC DIRECTION

Purpose

Values

Mission

VisionWhy we exist?

Who we are.

How we will accomplish

our Purpose & Vision.

The standards by which

we will stay true to our

purpose & mission.

What we want to

accomplish?

Rapidly provide the Joint Warfighter

with the right air to ground weapon

systems to dominate enemy forces

on the battlefield.

Build a high

performance joint

project team that excels

in all

we do.

LEADERSHIP

• Commitment

• Responsiveness

• Teamwork

Continually optimize resources to develop, field and sustain

the best air to ground munition systems capabilities.

Leadership is the capacity to transform vision into reality

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HELLFIRE ROMEO OVERVIEW

Weight = 108.5 lbs Length = 64”

• Single Multi-Purpose warhead

• PILOT selects lethality effects

• PILOT selects delays

• Increase engagement develops

• Support condition based maintenance

Description

ALL Production Deliveries in FY13 will be AGM-114R

AGM-114R

Milestones System PDR Jan 09

POP 1 Flight Aug 09

System CDR Sep 09

POP 2 Flight Jan 10

IPR (Qual/Pilotline Turn-on) Feb 10

POP 3 Firing (Ground) Apr 10

POP 4 Firing (Air) Jul 10

POP 5/6 Firings (Ground) Oct 10

PCT Firings (2) Jul 11

SQT Firings (12) Jul 12

First Production Deliveries FY13

Shaped Charge Warhead

Blast Fragmentation Warhead

Shaped Charge w/ Frag SleeveRomeo

Multi-

Purpose

WarheadFull UAS Capability Backward Compatible

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• Installed 99 CCHMs on 114N for one year demo (in

theater…8 CCHM missiles currently flying)

• CCHM demos at Ft. Rucker & SCARNG with

converted training Missile

• Data collection ongoing in

OIF/OEF (10/14 Nodes)

• R missile Health Monitor

design in process

• CCHM Version 2 - Platform discrimination, 675

fielding

HEALTH MONITORING(CCHM & Romeo HMU)

HELLFIRE II

• Scope of Effort: Qualified design to monitor

captive carry hours of individual HELLFIRE missiles.

• Methodology: Integrate commercially available

data acquisition technology attached to deployed

missiles. These devices will record the captive carry

time and other data sets for each missile.

• Participants: AMRDEC, RTC, NSWC-Crane,

JAMS PMO, and OEM Contractor.

Where We Are Now

• Install on ~2,700 inventory missiles during RESET

• Captive Carry, Power On, High/Low Temp,

Drop/Shock

• Interface with ULLS-AE (earliest fielding May 2011)

• Data sent to platform data bus for collection and

transmit to JAMS Database (Romeo HMU – ver. 2)

• New ULLS-AE Forms (Missile & MDFR)

Benefits

Path Forward

• Reduce O&M Cost

• Reduce Maintenance Burden

• Increase Reliability & Availability

• Enhance Safety

What We Are Doing Captive Carry Health Monitor

(CCHM)

Installing CCHM at depot

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AWCF

Cost

($Millions)

Implement a Condition Based Maintenance Policy

$0.0

$1.0

$2.0

$3.0

$4.0

$5.0

$6.0

Planned Cost $5.4 $5.7 $5.3 $0.0

Actual Cost $5.4 $0.6 $0.5 $0.6

FY07 FY08 FY09 FY10

Planned SG Qty 445 322 300 116

Actual SG Qty 445 38 31 20*

$5.4M$5.7M

$5.3M $0M$5.4M

$0.6M $0.5M$0.6M

$14.9M Cost

Avoidance by

not replacing

300 Missiles

with all SG

replaced

HELLFIRE II

SENSOR GROUP REPLACEMENT

* = Estimated Number

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INITIAL Capabilities

• Testing all HELLFIRE Variants in AOR

• Perform External Repairs in AOR

• Improved Materiel Availability &

Readiness

FUTURE Capabilities

• Support to All Services

• Support to Coalition Forces

• Expand to other Munition Systems

• X-Ray Capability

HELLFIRE MISSILE SYSTEMS FORWARD

TEST AND REPAIR FACILITY

Forward Test and Repair Facility

Falcon 78, Qatar

HELLFIRE Missile Systems

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WarheadSection

PropulsionSection

ControlSection

GuidanceSection

End to End Internal Electrical Test

DomeReplacement

Pin/CleaningAlignment

Intermediate ShoeReplacement

FinReplacement

AFT Plate Replacement

HELLFIRE FTRF will Operate on a Quarterly Basis and Service an average 108

HELLFIRE Missiles Per Quarter

WingReplacement

HELLFIRE II FTRF

TEST AND REPAIRS OVERVIEW

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2.75 Inch Aviation Rockets

“Hydra-70”

* PM, Aviation Rockets is the ACAT 1C, Tri-service Manager for Army, Navy and Air Force 2.75 Inch Rocket Requirements

Lessons Learned• Need Improved Reliability of the Rocket Delivery System• Need Increased Stowed Kills with a Laser Guided Rocket• Need Common Solutions in Support of the Joint Warfighter

Future Focus• Increased Warhead/Fuze Safety, IM and Reliability (SRAP

Program) • Replace Analog Rocket Launcher with Modernized Launcher• Deliver Guided Rockets for Increased Stowed Kills

Capabilities

Description

• Provide Air-to-Ground Suppression, Smoke Screening,

Illumination and Direct and Indirect Fires to Defeat

Area Materiel and Personnel Targets At Close and

Extended Ranges

• Warheads: High-Explosive Anti-Personnel, Flechette,

Multi-purpose Submunition, Smoke, Illumination,

Training

• Expenditures (Oct 01 – Present – US Army Only): Over

200,000 Tactical All Up Rounds (AURs) Consumed in

Theater (*Special Operations Expenditures Not

Included)

M261 M267 M255A1

M149

M264 M257 M278 M229

M146

M151 WTU 1/B M274 M156

Mk66 Mod-4 Rocket Motor

M260 Rocket Launcher

Milestones

JAN 10 – Tiger Team Phase One Activities Complete (OEF/OIF)

• JUN 10 – Awarded FY10-13 Hydra 70 Production Contract --

General Dynamics Armament and Technical Products (GDATP)

• 2QFY11 – Field IM Compliant, Plastic Storage and Shipping

Fastpack Container

• 4QFY12 -- Field Interim Launcher Solution – Non-Umbilical

Interface to Bridge Gap for the Modernized Rocket Launcher

(MRL)

• 2QFY13 – Field M151X IM Compliant Warhead

• FY14 - Field Modernized Rocket Launcher

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SMALL GUIDED MUNITIONS

Strategy

• React rapidly to support emerging war fighter needs

• Leverage Industries significant IRAD investments in the <50 lbs munitions class

• Execute a recurring SGM fieldable prototype munitions “Rodeo”

• “Rodeo” Concept– Provide industry with launch platforms– Provide industry with range time– Industry must be able to plug and play with

no change to A/C software– Industry must be able to field munitions– Independent evaluator produces a capability

& limitation report for all services to utilize

Current Warfighter Support

• Rapid fielding of new common configuration

GPS Viper Strike Munitions currently underway

for Hunter B – Training Drops complete May 10

• Supporting Marine Corps “Harvest Hawk” rapid

fielding program with Viper Strike and Griffin

munitions – Fielding expected by Dec 10

• Supporting SOCOM Requirements

• Viper Strike Quantities Fielded

– To the Army: 109

– Remaining in Theater: 25

– In Stock: 15

– 700 BATs munitions available for

conversion

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EMERGING TECHNOLOGIES

ITEM DESCRIPTION(<50-lb Class Munitions)

CURRENT AND POSSIBLEPLATFORMS

BAE

APKWS

• Navy /Marine Corps Program of Record

• 2.75” Guided Rocket with Mid-body Guidance Section

• Lock on After Launch

• Utilizes Hydra Rocket System

• OH-58D

• AH-64D

• AH-1 W/Z

• UH-1 Y

• UAS Platforms

Raytheon

Talon

• 2.75” Guided Rocket with Nose Mounted Guidance Section

• Lock on After Launch

• Utilizes Hydra Rocket System

• OH-58D

• AH-64D

• AH-1 W/Z

• UH-1 Y

• UAS Platforms

ATK

GATR

• 2.75” Guided Rocket with Nose Mounted Guidance Section

• Lock on After Launch / Lock on Before Launch

• Utilizes Hydra Rocket System

• OH-58D

• AH-64D

• AH-1 W/Z

• UH-1 Y

• UAS Platforms

Lockheed Martin

DAGR

• 2.75” Guided Rocket with Nose Mounted Guidance Section

• Lock on After Launch / Lock on Before Launch

• Utilizes Hydra Rocket System

• OH-58D

• AH-64D

• AH-1 W/Z

• UH-1 Y

• UAS Platforms

Raytheon

Griffin

• GPS/INS + SAL Terminally Guided Munition

• Blast Frag Warhead

• Fuzing Options: Height of Burst, Point Detonate, Delay

• OH-58D

• AH-64D

• AH-1 W/Z

• UH-1 Y

• UAS Platforms

• SOCOM Platforms

• Remote Weapon Stations, ITAS, NLOS-CLU, Bi-Pod

Viper Strike E

XM-150

• GPS/INS + SAL Terminally Guided Glide Munition

• Shaped Charge Warhead

• 360 Degree Off-Axis, Steep or Shallow Attack

• No Launch Signature

• Derived From Army ATACMS BAT Subminition

• Hunter MQ-5B

• SOCOM Platforms

• Marine Corps Harvest Hawk (KC-130J)

• Can be Integrated on Any UAS Platform

GATR

DAGR

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TARGETS / COMBAT LOAD / WEIGHT / COST

Rockets Guided Rockets HELLFIRE

Area Suppression Soft Vehicles Soft Vehicles

Target Marking IED Emplacement IED Emplacement

Obscuration Field Expedient Bunkers Bunkers

MANPADS MANPADS

Mobile Air Defense

Multi-room Bldg

Armored Tanks

*Qty 7/Kiowa *Qty 7/Kiowa *Qty 2/Kiowa

(Qty 3 Mixed Load)

~ 200 Lbs ~ 260 Lbs (7 Guided) ~ 290 Lbs

~ 220 Lbs (Mixed Load)

APUC~$1k APUC~$15k APUC~$92k

Ta

rg

ets

Co

mb

at

Lo

ad

We

ig

ht

Co

st

1.3m CEPLow Collateral

Capability Continuum

* Per weapons station. Assumes one weapon station equipped with .50 cal or HELLFIRE.

Scaleable precision provides more effective and efficient fires

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JOINT AIR-TO-GROUND MISSILE

OH-58 CASUP

F/A-18E / F AH-1Z

MQ-1C

AH-64D

MH-60R

Description Milestones

• Joint Program with Navy and USMC• Provides Line of Sight (LOS) & Beyond LOS• Precision Strike, Active and Passive Fire-

and-Forget modes• Autonomous Target Acquisition (ATA)• Enhanced/Robust countermeasures

capability• Modular Missile Design• System ~ 108 lbs, 7 inch dia., 70 inch length• Range: 500 - 16,000 meters for rotary wing

2,000 - 28,000 meters for fixed wing

Capabilities

• Interoperable with fixed wing, rotary wing and UAS

platforms

• Carrier / shipboard operability

• Multi-Purpose Killer (Moving and Stationary Hard and

Non-Armored Targets, Maritime, and MOUT)

• Multi-mode seeker for maximum capability in adverse

weather, day or night, and in an obscured /

countermeasure environment

• Health Monitoring Unit (HMU) provides enhanced

supportability and reliability

Contract Awards (2) 11 Sep 08

Integrated Baseline Review 15 Dec 08

Program Management Reviews 2QFY09

• Preliminary Design Review 3QFY10

• Milestone B 1QFY11

• IOC – F/A-18E/F, AH-64D, AH-1Z FY16

• IOC – MH-60R, MQ-1C, OH-58D CASUP FY17

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JAGM CAPABILITIES

Supportable

• Single capability of joint missions

• HMU fully integrated with long service life

supports CBM approach

• Access panels

• Container provides missile condition indicator

and software upload interface

Range

• Platform survivability – JAGM provides 16 Km

• UAV range out to 28Km

Targeting

• Countermeasure robustness

• Adverse weather operations

• Fire and Forget modes

• F&F long range moving targets

• UAS capability, 360° all modes and altitudes

• Autonomous aimpoint selection

IM Compliance

• Composite rocket motor case

• Warhead design

Modularity

• Modular design using open architecture

• Enhances future upgrades and technology

insertion

• Standard interfaces provide alternatives to

the prime

• Ready for GPS and datalink upgrades

High Altitude – High Speed Fixed Wing

• Designed for the fixed wing environment

– Safety

– Performance

– 28Km

• Other platforms waiting in the wings

– JSF (threshold weapon)

– P-8A

HF is limited by Antiquated Architecture and Sole Source/Proprietary Interfaces