Improved Turbine Engine Program (ITEP)Future Vertical Lift (FVL)

Mr. Rich Kretzschmar Project ManagerImproved Turbine Engine / Future Vertical Lift Project Office

10 June 2016

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

2DISTRIBUTION STATEMENT A

ITE/FVL Organization

Operations

Admin SupportKacey Stvan

Project ManagerRich Kretzschmar

Product LeadLeslie Hyatt Future Vertical Lift

Product ManagerLTC Curt Kuetemeyer Improved Turbine Engine

Tech Division ChiefMark Jeude

Logistics Division ChiefScott Harris

Business Division ChiefJoe Clegg

Deputy Project ManagerBob Sheibley

Deputy Product LeadMark Caskey Future Vertical Lift

Deputy Product ManagerBen Plummer Improved Turbine Engine

ITEP

Technical

FVL

Product Support

Business

Acquisition Support

Technical Acquisition Support

Systems Engineering Mission Equipment

ILS

Contract Mgmt Financial Execution

3DISTRIBUTION STATEMENT A

701

4011700 shp

700

1600 shp

701D2,000 shp

701C

401C1,900 shp

ITEP

3,000 shp

Legacy T700 Engine:

1. 2000 Shaft Horse Power Engine Class2. Originally designed with 1970s technology3. 30 years of evolutionary growth

4. Engine performance has been maximized

Improved Turbine Engine (ITE)

1. 3000 Shaft Horse Power Engine Class2. Will fit within the current Black Hawk and Apache engine bay at similar weight

3. Provides world wide performance to meet operational requirements at 6K/954. More power with greater fuel efficiency

5. Equal or better sustainability and reliability with growth margin

1976 1983 1987 2003 2024

Improved Turbine Engine Program (ITEP)

4DISTRIBUTION STATEMENT A

Program Objective:

Advanced Affordable Turbine Engine (AATE) was an S&T program to develop improved, 3000 hp class turboshaft engine technology providing improved operational capability for Black Hawk, Apache and other Future Vertical Lift aircraft.

Results:

Demonstrated critical technologies: Advanced Aerodynamics: Improves fuel efficiency and power

Hybrid Ceramic Bearings: Improves reliability

Inlet Particle Separator: Removes Contaminants at intake

Critical technologies assessed at Technology Readiness Level (TRL) 6 by independent

review team from Deputy Assistant Secretary of the Army for Research and Technology

What is left to do:

Design and build an engine by integrating critical technologies

Integrate engine onto the platforms (AH and UH)

Test and qualify engines and aircraft

S&T Contribution to ITEP

FY15 FY16 FY17 FY18 FY19 FY20 FY21 FY22 FY23 FY24

TM&RR EMD

RFP Released MS A PDR MS B CDR

Engine Qualification

First Engine Test MS C

5DISTRIBUTION STATEMENT A

The Best of Both Worlds (6K/95)

4K ft

6K ft

Operational Energy Savings

701D

Increases Warfighter Capability

ITE

701D: 12A/C 3 turns w/FARP; 100% on OBJ in 480 min

ITE: 12A/C 1 turn w/o FARP; 100% on OBJ in 68 min

13 Troops

5 Troops

FARP

AA

225 km radius

UH-60M Assault

Combat Configuration

13 troops (290 lbs. ea.)

MEETS 225 km Radius

UH ORD Requirement

6K/95F

UH-60M Assault

Combat Configuration

5 troops (290 lbs. ea.)

145 km Max Radius

6K/95F

13,270gal of fuel used on UH-60 (10)/AH-64 (2) air assault mission (225km) w/701D

3,341gal of fuel used on UH-60 (10)/AH-64 (2) air assault mission (225km) w/ITEP

701D ITE

1 barrel = 1,000gal

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6DISTRIBUTION STATEMENT A

FVL is a strategic advance in Vertical Lift Capabilities for the Warfighter

The Future Vertical Lift (FVL) Capability Set 3 (CS 3) Program will provide increased speed, range, maneuverability and

survivability over the Armys current Black Hawk aircraft. FVL is a Single Lead Service, Joint Participation Initiative that will provide Combatant Commanders with tactical capabilities at operational and strategic distances.

FY09 Congress NDAA directed outline of Joint

approach to development of future vertical lift aircraft

FY12 DepSecDef Approved

FVL Strategic

Plan

FY13 FVL Family of Systems ICD JROCM - Army

Designated as Lead Component

FY15 TCM FVL & PM ITE/FVL Established

FY17 MDD Planned 1QFY17

FY18 AoA Completion

FY19 RFP Decision

FY21 Milestone A

FY24 Milestone B

FY29 Milestone C

Informed by JMR-TD

Integrated IPT Structure

Family of Systems Concept

Formal Industry Participation

Single Service LedJoint Participation

Transition Focus from FoS Initiative to Acquisition of Initial

Capability Set FVL CS3 Acquisition

FVL FoS Initiative

Future Vertical Lift (FVL)

7DISTRIBUTION STATEMENT A

Why FVL?

Minimizes Strategic Lift Requirements. Expands the Reach of Army Aviation to Support Global

Requirements. Rapidly Builds Combat Power on the Objective. Extends Operational Reach of the CAB. Reduces MEDEVAC Requirements (Larger 1hr Rings). Enables Support Efficiencies.

Benefits

Speed Range

Payload Maneuver

FVL

Capabilities

FVL Aligns with Strategic Guidance and Operational Need

AviationCore Competencies

Agile

Flexible

Global

Sustainable

Deployable

Advanced

Responsive

Adaptable

Range

Speed

Payload

Develop Situational Understanding.

Shape the Security Environment.

Conduct Homeland Operations.

Enhance Training.

Improve Soldier, Leader and Team Performance.

Develop Agile and Adaptive Leaders.

Conduct Air-Ground Reconnaissance.

Conduct Entry Operations.

Conduct Wide Area Security.

Ensure Interoperability.

Conduct Combined Arms Maneuver.

Integrate Fires.

Deliver Fires.

Exercise Mission Command.

Develop Capable Formations.

Provide accurate and timely Combat Information about the Enemy, Terrain & Local Populations.

Provide Reaction Time and Maneuver Space.

Destroy, Defeat or Disrupt Enemy Forces.

Air Assault Ground Maneuver Forces.

Air Move Personnel, Equipment and Supplies.

Evacuate Wounded or Recover Isolated Personnel.

Enable Mission Command over Extended Ranges and Complex Terrain.

Warfighting ChallengesStrategic Guidance Threats

Threats to Maneuver Force

Long-range artillery

Anti-ship missiles

Threats to Aircrew/Platform

Small Arms

RPGs

Shoulder-Fired Missiles

Integrated Air Defense

Information Operations

8DISTRIBUTION STATEMENT A

FVL Key Technologies

FY16 FY17 FY18 FY19 FY20 FY21 FY22 FY23 FY24 FY25 FY26 FY27 FY28 FY29 FY30

RFP Decision MS CMS BMS AMDD

TM&RR Phase EMD Phase LRIPMSA PhaseRFP DecisionRFP Decision

Advanced Drive / Rotor System

Advanced Flight Controls

Advanced Structures

Advanced Engines

Advanced Survivability

Advanced Maintainability / Reliability

Modular Based Design

Situational Awareness & Flight Management

Open System Architecture

TRA

FVL POR

Advanced Aircraft Design, Reconfigurable Rotors, Durable and Active Power, Variable Speed Transmission, Lightweight Generators

Autonomous Flight Controls, Adaptive Engine Controls, Advanced Control Laws, Individual Blade Control

Advanced Materials, Advanced Affordable Manufacturing Techniques, Advanced Design/Modeling/Analysis Tools

Variable Speed Turbine, Adaptable, Fuel Efficient, High Power to Weight

Aircraft/Aircrew Protection (Ballistic), Precision Navigation Timing (PNT), Global Positioning System (GPS) in Contested Environment, Signature Reduction, Balanced Survivability Suite, Real-Time 3D Route Planner

Self Healing Structures, Advanced Material Repair, Embedded Diagnostics/Prognostics & Advanced Health Monitoring

Electrical Architecture and Electromechanical Actuation

Pilotage in all Degraded Visual Environments (DVE), Manned-Unmanned Teaming, Optionally Piloted, Mission Adaptive Autonomy, Coupled Symbology

Reference Architecture; Mission Systems Architecture

Key

Capabilities

Spe

ed

Ran

ge

Pay

load

Surv

ivab

ilit

y

Aff

ord

abil

ity

All Key Technologies link to S&T efforts and mature before MS B

Key Technologies

FVL Technology Maturation through

JMR TD and other S&T Initiatives

Key Attributes

Man

eu

ver

Inte

rop

era

bili

ty

Technology Readiness Assessment

6

6

6

6

6

6

6

6

6

TRL

9DISTRIBUTION STATEMENT A

Advanced Systems Engineering Initiatives

Open Architecture Design Multi-service effort to define standards &

implement architecture designs

Enabled by Army Mission Systems Architecture Demonstration and US Navy Avionics Architecture efforts

Enables system commonality in FVL fleet; extends opportunities to legacy fleet

Reduces sustainment costs through faster upgrades

Model Based Systems Engineering Efficiently documents complex system

requirements

Improves requirements traceability & definition of relationships between requirements

Improves design process risk evaluation & management

Vision for Open Architecture

Model Based Systems Engineering (MBSE) Approach

ITE/FVL is implementing advanced systems engineering initiatives early for maximum benefit

Requirements

Integrated System Model

Must Address MultipleAspects of a system

Behavior/Functional Architecture

Structure/Physical Architecture Dynamic Performance

Mass

Cost

Manufacturing

Reliability

System

Model

Engine Transmission Rotor Control

InputPow er

Equation

s

Vehicle

Dynamic

s

Start Takeoff Cruise Land

10DISTRIBUTION STATEMENT A