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1 Aeronautics Research Mission Directorate ARMD SIP Thrust 4B (Hybrid Electric) Roadmap Rich Wahls 2 nd ODM & Emerging Av Tech Roadmap Workshop Strategic Technical Advisor, Adv Air Vehicles Program Arlington, VA Aeronautics Research Mission Directorate 9 March 2016

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1 Aeronautics Research Mission Directorate

ARMD SIP Thrust 4B (Hybrid Electric) Roadmap Rich Wahls 2nd ODM & Emerging Av Tech Roadmap Workshop Strategic Technical Advisor, Adv Air Vehicles Program Arlington, VA Aeronautics Research Mission Directorate 9 March 2016

2 Aeronautics Research Mission Directorate

Outline•  ARMD Overview – Thrusts, Programs, Projects

•  ARMD Strategic Thrust 4b – Electric/Hybrid Electric

•  ARMD FY17 President’s Budget Implications

3 Aeronautics Research Mission Directorate

U.S. leadership for a new era of flight

NASA AeronauticsNASA Aeronautics Vision for Aviation in the 21st Century

5 Aeronautics Research Mission Directorate

Aeronautics Research Mission Directorate

Advanced Air Transport Technology

(AATT)

Advanced Air Vehicles (AAVP)

Jay Dryer

Airspace Operations And Safety (AOSP) John Cavolowsky

Integrated Aviation Systems (IASP) Ed Waggoner

NASA Mission Directorate Organization

Transformative Aeronautics Concepts (TACP)

Doug Rohn

Revolutionary Vertical Lift Technology

(RVLT)

Commercial Supersonic Technology

(CST)

Advanced Composites (ACP)

Aeronautics Evaluation and Test Capabilities

(AETC)

Airspace Technology Demonstrations

(ATD)

SMART NAS – Testbed for Safe Trajectory

Operations

Safe Autonomous System Operations

(SASO)

Environmentally Responsible

Aviation (ERA)

UAS Integration in the NAS

Flight Demonstration and Capabilities

(FDC)

Leading Edge Aeronautics Research

for NASA (LEARN)

Transformational Tools and Technologies

(TTT)

Convergent Aeronautics Solutions

(CAS)

-------------------------- Mission Programs ----------------------------- Seedling Program

Coming Soon Electric content

Current Electric content

6 Aeronautics Research Mission Directorate

Outline•  ARMD Overview – Thrusts, Programs, Projects

•  ARMD Strategic Thrust 4b – Electric/Hybrid Electric

•  ARMD FY17 President’s Budget Implications

7 Aeronautics Research Mission Directorate

NASA Aeronautics ContextThrust Roadmap and other related teams

3 Mega-Drivers 6 Strategic R&T Thrusts

Safe, Efficient Growth in Global Operations •  Enable full NextGen and develop technologies to substantially

reduce aircraft safety risks

Innovation in Commercial Supersonic Aircraft •  Achieve a low-boom standard

Ultra-Efficient Commercial Vehicles •  Pioneer technologies for big leaps in efficiency

and environmental performance

Transition to Low-Carbon Propulsion •  Characterize drop-in alternative fuels

and pioneer low-carbon propulsion technology

Real-Time System-Wide Safety Assurance •  Develop an integrated prototype of a real-time safety monitoring

and assurance system

Assured Autonomy for Aviation Transformation •  Develop high impact aviation autonomy applications

Roadmap Team 2 Supersonic

Roadmap Team 3a Fixed Wing Roadmap Team 3b Vertical Lift

Roadmap Team 4a AltFuel Roadmap Team 4b Hybrid Electric

10 Aeronautics Research Mission Directorate

Thrust 4b Hybrid Electric

Thrust 4b – Team Hybrid Electric kick-off 6/12/15 Scope: Large Transport, Small Thin-haul, passenger vertical lift, unmanned aerial vehicles

(internal community – AATT, CAS (VLHA, CEPT)) Co-leads Kevin Carmichael/Rich Wahls Amy Jankowsky (AATT) Hyun Dae Kim (AFRC) Lee Kohlman (CAS/VLHA) Nateri Madavan (ARC) Mark Moore (CAS/CEPT) Jim Felder (GRC) Dell Ricks (ARMD) Dan Williams (LaRC)

Jeff Viken (TTT)

Transition to Low-Carbon Propulsion •  Characterize drop-in alternative fuels and pioneer low-carbon propulsion technology

12 Aeronautics Research Mission Directorate

Outcomes, Benefits, Capabilities

Strategic Thrust 4: Transition to Low-Carbon Propulsion Strategic Thrust 4B: Enabling Electric/Hybrid Electric Propulsion

2015 2025 2035

Com

mun

ity

Out

com

es

Introduction of Low-carbon Fuels for Conventional Engines and Exploration

of Alternative Propulsion Systems  Initial Introduction of

Alternative Propulsion Systems  Introduction of

Alternative Propulsion Systems to Aircraft of All Sizes

Ben

efits

•  Established experience and knowledge base allowing for industry investment and market growth

•  Certified operational aircraft in limited applications/markets

•  Improved fuel economy and lower carbon emissions in limited applications.

•  Improved acoustics

•  Improved fuel economy•  Low carbon emissions•  Lower operating costs•  Enhanced safety,

Cap

abili

ties/

NA

SA O

utpu

ts

•  Electrified Turbofan designs•  HEP PAI and DEP concepts•  Advanced electric machines &

power electronics•  Integrated electric and turbine

controls•  Advanced energy storage

technology•  Advanced power transmission and

management technology•  Small aircraft and vertical lift flight

demos•  Thin haul commuter flt demo•  Power and propulsion system

integrated test beds•  Modeling, sizing, design and

analysis tools

•  Medium size Vertical lift flt demos•  Electric air vehicle certification•  Experience designing, building and

operating a variety of small electric and HEP aircraft and vertical lift vehicles

•  An array of Government and Industry development and test facilities

•  Optimized architectures•  Optimized flight operations•  Improved energy storage•  Advanced materials applied to

HEP•  High fidelity models

•  Single aisle transport flight demo•  Large vert lift flight demo•  Extensive experience designing

building and operating electric and HEP aircraft and vertical lift vehicles

•  Industry has full design and test capability

•  Increased & more flexible control

Version: 19jan2016

13 Aeronautics Research Mission Directorate

Research Themes NASA Long Term Research Areas That Will Contribute to the Community Outcomes

•  Integrated Technology Concepts (Vehicle / Synergy)–  Integration of an array of technologies to increase the overall efficiency and functionality of the

vehicle including: HEP propulsion and airframe, distributed electric propulsion, acoustics and airframe, controls and HEP propulsion, energy storage and airframe, thermal management and airframe

•  Power and Propulsion Architectures–  Researches electric, hybrid electric, turboelectric, series, parallel, configurations for both aircraft and

vertical lift vehicles. This also includes power management, distribution of power across the vehicle

•  HEP Components / Enablers–  Includes component technologies such as increased power density electric machines, higher,

superconducting machines, energy density storage, advanced fuel cells, power electronics, fault protection devices and other enablers such as flight controls

•  Modeling, Simulation, and Test Capability–  Development of modeling, simulation and design tools to aid in the design and analysis of electric/

HEP vehicles, These may also include acoustic and thermal management and flight control analysis tools. Also includes component, subsystem and system level test capabilities that are be used in development.

Version: 19jan2016

17 Aeronautics Research Mission Directorate

Prove Out Transformational Potential Hybrid Electric Propulsion

Increasingly electric aircraft propulsion with minimal change to aircraft outer mold lines

Explore and demonstrate vehicle integration synergies enabled by hybrid electric propulsion

Gain experience through integration and demonstration on

progressively larger platforms

Single Aisle Transport

Modeling Explore Architectures

Test Beds Component Improvements

Env

iron

men

tal B

enef

it

+

2040

2030

2020 Small Aircraft

Knowledge through Integration & Demonstration +

Image Credit: Joby

Image Credit: Yamaha

19 Aeronautics Research Mission Directorate

Exploration of Alternative Propulsion Systems  

Initial Introduction of Alternative Propulsion Systems  20

15

2025

2035

Mature foundation technologies, architect HEP aircraft and Vert Lift vehicles, demonstrate

subsystems and integrated prototypes  

Fly technology demonstrators, prototype subsystems and advanced components  NASA

Outputs

Community Outcomes

Explore PAI and DEP configuration

Acoustics and DEP

Wing/Fuselage BLI and DEP Split Wing with upper/lower DEP

Controls associated with DEP

DEP w/conventional or high aspect ration wings

Explore elec / hybrid / turboelectric configurations 200 KW – 10 MW

Non-Superconducting Powertrain Components

Energy Storage, Power Distribution & Mgt.

kW, MW, 10s MW Powertrain Models, Testing & Validation

Technology Integration Concepts (Vehicle/Synergy)  

Power & Propulsion Architectures  

HEP Components/Enablers  

HEP Models / Sims &Test Capability  

Small Core Turbine from 4A Leverage industry battery, fuel cell developments, wide band gap semi-conductors

Leverage DoD architecture parametric studies, industry studies and developments (DARPA, Google, Facebook, Boeing)

Advanced Turbines, Controls, Range Extenders

Superconducting Powertrain Components, including Thermal Ctr.

Single String, Full Powertrain, Full Vehicle Modeling & Simulation

High Fidelity CFD, Integrated Turbine and Electric Controls,Power & Energy Storage Management

Modeling and Testing to support Validation & Certification

Explore elec / hybrid / turboelectric configurations 10 MW – 20 MW

Explore elec / hybrid / turboelectric configurations 20MW – 50 MW

4 PAX Vertical Lift Vehicle

Demo Research Themes

Technology Demos/Insertions

SCEPTOR Thin Haul Commuter

Demo

Medium Commuter

Demo

More Electric Turbofan Enters

Service

Regional Transport Flt Demo

Single Aisle flight Demo

8 PAX Vert Lift Vehicle

Demo

9-12 PAX Vertical

Lift enters service

Thin Haul Commuter Enters

Service

Alternative Fuels from 4A Dependencies / Opportunities  

Intro of Alternative Propulsion Systems to Aircraft of All Sizes  

Refined and optimized HEP aircraft and propulsion system concepts and components

Version: 19jan2016

20 Aeronautics Research Mission Directorate

Top 6 Risks

1.  If projected improvement in the energy sector that we expect to leverage (ex. batteries, fuel cells, power electronics) are not realized then HEP may be applicable to small aircraft, but large all electric/hybrid-electric transports cannot be achieved and the environmental impact not realized.

2.  If HEP component technologies are not realized, then the benefits of HEP vehicles will not be fully realized

3.  If industry does not agree significant savings can be achieved then they will not invest in vehicles.

4.  If electrification poses significant safety or certification hurdles, then integration into fleet will become too costly

5.  If the community can’t cost effectively change/enhance the energy infrastructure at airports, then the viability of electrically powered aircraft will not be realized

6.  If energy sources used to power electric/hybrid electric systems are not from clean energy from a life cycle perspective, the climate benefits will not be realized nor systems developed and fielded.

21 Aeronautics Research Mission Directorate

Leverage Opportunities

•  Leverage early adopter market opportunities to establish new certification criteria and accelerate industry technology investments.

•  Leverage efforts in the Energy and Transportation sectors to improve battery and fuel cell energy density. Higher energy density in these devices may enable all electric architectures and enhance hybrid electric architectures.

•  Leveraging advances in small core turbine engine technologies being developed by industry would enhance hybrid electric architectures

•  Leveraging DoD’s and DARPA’s investment and knowledge in HEP for civilian and military dual use applications will allow NASA to explore a wider range of configurations.

•  Leverage lessons learned from electric/hybrid aircraft propulsion efforts by Google, Facebook, and Boeing to learn how to design, build, integrate and operate vehicles

23 Aeronautics Research Mission Directorate

Outline•  ARMD Overview – Thrusts, Programs, Projects

•  ARMD Strategic Thrust 4b – Electric/Hybrid Electric

•  ARMD FY17 President’s Budget Implications

26 Aeronautics Research Mission Directorate

New Aviation Horizons Flight Demo Plan

Design & Build Flight Test

Design & Build Flight Test

Design & Build Flight Test

Design & Build

FY17 FY18 FY19 FY20 FY21 FY22 FY23 FY24 FY25 FY26

Preliminary Design

“Purpose-Built” UEST Demonstrators

Hybrid Electric Propulsion Demonstrators

Fully integrated UEST Demonstrator

Design & Build Flight Test

Preliminary Design

Preliminary Design

Design & Build Flight Test Design & Build Flight Test

Ground Test Risk Reduction

Ground Test Risk Reduction

Potential Candidates

Ground Test Risk Reduction Flight Test Small Scale “Build, Fly, Learn”

Transport Scale Preliminary Design

Total Demonstration Cost ROM: $700M

Life Cycle Cost Est: $430M

Life Cycle Early Cost Est: $850M

Life Cycle Cost ROM: $400-500M

Life Cycle Cost ROM: $400-500M

www.nasa.gov 26

Images Credit: Lockheed Martin

DP

DP

DP

DP

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Validated ability for U.S. Industry to Build Transformative Aircraft that use 50% less energy and produce less than half of the perceived noise

Validated HEP Concepts, Technologies And Integration for U.S. Industry to Lead the Clean Propulsion Revolution

Enables Low Boom Regulatory Standard and validated ability for industry to produce and operate commercial low noise supersonic aircraft

27 Aeronautics Research Mission Directorate27  Your  Title  Here