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Non-Flow-Through Fuel Cell System Test Results and Demonstration on the SCARAB Rover This presentation describes the results of the demonstration of a non-flow-through PEM fuel cell as part of a power system on the SCARAB rover at the NASA Glenn Research Center. A 16-cell non-flow-through fuel cell stack from Infinity Fuel Cell and Hydrogen, Inc. was incorporated into a power system designed to act as a range extender by providing power to the SCARAB rover’s hotel loads. The power system, including the non-flow-through fuel cell technology, successfully demonstrated its goal as a range extender by powering hotel loads on the SCARAB rover, making this demonstration the first to use the non-flow-through fuel cell technology on a mobile platform. National Aeronautics and Space Administration www.nasa.gov https://ntrs.nasa.gov/search.jsp?R=20120018031 2020-04-10T12:59:57+00:00Z

Non-Flow-Through Fuel Cell System Test Results and Demonstration on … · 2013-04-10 · Non-Flow-Through Fuel Cell System Test Results and Demonstration on the SCARAB Rover Brianne

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Page 1: Non-Flow-Through Fuel Cell System Test Results and Demonstration on … · 2013-04-10 · Non-Flow-Through Fuel Cell System Test Results and Demonstration on the SCARAB Rover Brianne

Non-Flow-Through Fuel Cell System

Test Results and Demonstration on the

SCARAB Rover This presentation describes the results of the demonstration of a non-flow-through

PEM fuel cell as part of a power system on the SCARAB rover at the NASA Glenn

Research Center. A 16-cell non-flow-through fuel cell stack from Infinity Fuel Cell

and Hydrogen, Inc. was incorporated into a power system designed to act as a

range extender by providing power to the SCARAB rover’s hotel loads. The power

system, including the non-flow-through fuel cell technology, successfully

demonstrated its goal as a range extender by powering hotel loads on the

SCARAB rover, making this demonstration the first to use the non-flow-through

fuel cell technology on a mobile platform.

National Aeronautics and Space Administration

www.nasa.gov

https://ntrs.nasa.gov/search.jsp?R=20120018031 2020-04-10T12:59:57+00:00Z

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Non-Flow-Through Fuel Cell System

Test Results and Demonstration on the

SCARAB Rover

Brianne Scheidegger and Kenneth Burke

NASA Glenn Research Center

Ian Jakupca

QinetiQ North America

Power Sources Conference

Las Vegas, NV

June 11-14, 2012

National Aeronautics and Space Administration

www.nasa.gov

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National Aeronautics and Space Administration

Presentation Overview

• AMPS project overview & demonstration

goals

• SCARAB rover background

• NASA fuel cell development background

• Non-Flow-Through (NFT) Proton-

Exchange-Membrane Fuel Cell (PEMFC)

power system

• Demonstration & results

3

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National Aeronautics and Space Administration

AMPS PROJECT OVERVIEW AND

DEMONSTRATION GOALS

4

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National Aeronautics and Space Administration

AES Modular Power Systems Project

• Project Objectives: AMPS will infuse and

demonstrate modular batteries, fuel cells, and

other power modules; and, develop modular

power design concepts that will guide modular

assembly development and ultimately be realized

in exploration flight hardware

5

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National Aeronautics and Space Administration

Demonstration Requirements and

Objectives Formal Objectives

• Integrate NFT fuel cell power system onto SCARAB

rover

• Supply energy to SCARAB to extend mission duration

• Identify integration issues requiring further

development to facilitate advancing the technology

readiness level (TRL)

Formal Requirements

• Fuel cell power system must provide power to the

SCARAB rover

• Cannot damage or modify the rover

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National Aeronautics and Space Administration

SLOPE Test Facility

• Simulated Lunar Operations (SLOPE) Lab

at NASA Glenn Research Center

• Used to study traction & power

consumption of lunar vehicles operating in

soil

• Simulated lunar regolith soil tank for flat

surface operations & tilted soil tank for

sloped surface operations

7

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National Aeronautics and Space Administration

SCARAB ROVER

8

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National Aeronautics and Space Administration

SCARAB Rover

9

• SCARAB owned and operated by

Carnegie-Mellon University (CMU)

• Used in multiple field demonstrations and public relations

activities

• Mobile Platform for experiments

– ISRU

– Lunar Tire Development

– 12 Vdc NFT PEMFC

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National Aeronautics and Space Administration

SCARAB Power Requirements

• 28 VDC Power Bus

• Hotel Loads: 175 W (communications, computer,

cooling fans, etc.)

• Locomotion –

Stationary (elevation hold): 6 W (Total = 181 W)

Driving, level: 85 W (Total = 255 W)

Driving, turn: 200 W (Total = 375 W)

Elevating body: 225 W (Total = 400 W)

Peak Transient: 590 W (Total = 765 W)

10

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National Aeronautics and Space Administration

SCARAB Power

• SCARAB has on-board battery bank to provide power

during normal operation

• Demonstration of NFT PEMFC power system on

rover will act as a range extender by providing power

to hotel loads while rover is stationary

• Rover not currently capable of power sharing, so

power is provided by either SCARAB battery bank or

fuel cell power system, but not both simultaneously

11

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National Aeronautics and Space Administration

NASA PEMFC BACKGROUND

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National Aeronautics and Space Administration

NASA PEMFC Background

• PEM fuel cells convert hydrogen

and oxygen gases into water, waste

heat, and electricity

• A fuel cell can provide power as

long as reactants are available

• NASA NFT technology differs from

traditional flow-through technology

which operates in terrestrial

environments and uses air as a

reactant

• NASA missions operate in reduced

and zero-gravity environments, and

use pure oxygen as a reactant

13

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National Aeronautics and Space Administration

Flow-

Through

NFT PEMFC Development

Non-Flow-Through PEMFC technology

characterized by dead-ended reactants and

internal product water removal

• Tank pressure drives reactant feed; no

recirculation

• Water separation occurs through internal cell

wicking

Develop “non-flow-through” proton exchange membrane fuel cell

technology to improve system-level mass, volume, reliability, and

parasitic power Flow-Through components eliminated in Non-

Flow-Through system include:

• Pumps or injectors/ejectors for recirculation

• Motorized or passive external water

separators

an

od

e

ca

tho

de

co

ola

nt

MEA

H2O

gas

recirculation

pump

active water

separator

H2 O2

H2OH2O

O2

O2 / H2O

Non-Flow-

Through a

no

de

ca

tho

de

H2O

MEA

H2O

H2 O2

H2O

H2O

coo

lan

t

hyd

rop

hili

c m

em

bra

ne

14

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National Aeronautics and Space Administration

NFT PEMFC POWER SYSTEM

15

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National Aeronautics and Space Administration

16-Cell NFT PEMFC Stack Overview

16

• Developed by Infinity Fuel Cell and Hydrogen, Inc.

• TRL 4/5 technology

• Active Area: 50 cm2

• Number of cells: 16

• Nominal Stack Voltage: 12Vdc

• Nominal Stack Power: 100 Watts

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National Aeronautics and Space Administration

NFT PEMFC Power System

17

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National Aeronautics and Space Administration

Demonstration Setup • Power system

mounted on Al plate

secured to SCARAB

18

• Stack & reactants

above plate

• Electronics drawer

mounted below plate

Hydrogen

Fuel Cell Stack

Oxygen

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National Aeronautics and Space Administration

NFT PEMFC Power System on SCARAB

19

Electronics Drawer

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National Aeronautics and Space Administration

NFT PEMFC SYSTEM

DEMONSTRATION & RESULTS

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National Aeronautics and Space Administration

SCARAB Power Interface Concept

SCARAB

Battery

SCARAB

Power

Control and

Distribution

Fuel Cell and

Fluidics

Electronics

Battery

Bank

Ground

Support Power

NFT PEMFC Power System

Wire

less

Ground Support

Fuel Cell

Computer

Legend

Power

Instrumentation/Control/Data

Wireless Communication

NFT PEMFC system E-stop

Or

Reactant

Supply

Re

ch

arg

e/

Au

xili

ary

Recharge/

Auxiliary

E-stop

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National Aeronautics and Space Administration

Demonstration

• Tests performed to verify system

connectivity, stationary operation, and

mobile operation

• Fuel cell power system successfully

powered hotel loads during stationary

operation

• 16-cell fuel cell stack is undersized for the

SCARAB rover

• An actual mission requiring fuel cells would

match the fuel cell power capability with the

mission requirements

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National Aeronautics and Space Administration

Mobile Demonstration Power Profiles

Fuel Cell Stack Output Power

Power System Parasitic Power

Rover

Power

2 1 2 1

Notes:

1 – Open Stack Contactor & Close Scarab Contactor

2 – Close Stack Contactor & Close Scarab Contactor

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National Aeronautics and Space Administration

Summary

• Successfully integrated NFT fuel cell

technology onto ground demonstration

• Advances TRL of NFT PEMFC technology

• First demonstration of NFT PEMFC

technology for a mobile application

• NASA continues to work to develop

advanced NFT PEMFC systems to reduce

mass, volume, and parasitic power

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National Aeronautics and Space Administration

Future Activities for NFT PEMFC Power

Systems

• Miniaturized electronics

• Advanced thermal & water management

systems

• Advanced, custom interface plates with

integrated balance-of-plant

25

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National Aeronautics and Space Administration

BRIANNE SCHEIDEGGER

[email protected]

KENNETH BURKE

[email protected]

IAN JAKUPCA

[email protected]

Thank you. Questions?

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