Electrical Arc Ignition Testing of Spacesuit Materials

31
1 NASA White Sands Test Facility Electrical Arc Ignition Testing of Spacesuit Materials October 2006 Sarah Smith Tim Gallus Susana Tapia Elizabeth Ball Harold Beeson

Transcript of Electrical Arc Ignition Testing of Spacesuit Materials

Page 1: Electrical Arc Ignition Testing of Spacesuit Materials

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Elec

tric

al A

rc Ig

nitio

n Te

stin

g of

Sp

aces

uit M

ater

ials

Oct

ober

200

6

Sar

ah S

mith

Tim

Gal

lus

Susa

na T

apia

Eliz

abet

h Ba

llH

arol

d B

eeso

n

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Bac

kgro

und

•Te

stin

g in

resp

onse

to

fraye

d ca

ble

disc

over

ed

durin

g sp

acew

alk

•R

elia

nce

on A

pollo

-era

arc

te

stin

g–

Lim

ited

appl

icab

ility

to c

urre

nt

mat

eria

ls–

Sig

nific

ant c

hang

es in

vol

tage

an

d ci

rcui

try–

Poo

r und

erst

andi

ng o

f tes

t co

nfig

urat

ion

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Test

Obj

ectiv

es

•G

ain

bette

r und

erst

andi

ng o

f Apo

llo-e

ra d

ata

•In

vest

igat

e ne

w te

st m

etho

ds•

Cha

ract

eriz

e m

inim

um c

urre

nt le

vels

nec

essa

ry fo

r co

mbu

stio

n of

EM

U m

ater

ials

(at a

giv

en v

olta

ge)

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Test

Sam

ple

Mat

eria

ls

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Test

Met

hods

•M

ultip

le lo

catio

n in

term

itten

t arc

ing

(scr

atch

) tes

t •

Sin

gle

loca

tion

inte

rmitt

ent a

rcin

g (p

oke)

test

•S

ingl

e lo

catio

n w

ire-b

reak

arc

ing

test

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Scra

tch

Test

Obj

ectiv

es

•S

imul

ate

Apo

llo-e

ra te

stin

g•

Det

erm

ine

conf

igur

atio

nale

ffect

s•

Test

mat

eria

ls c

urre

ntly

use

d in

the

EM

U

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Page 9: Electrical Arc Ignition Testing of Spacesuit Materials

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Slit

in T

est S

ampl

e

Styl

us

Cot

ton

Scra

tch

Test

Vid

eo

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Scra

tch

Test

Res

ults

•Te

stin

g yi

elde

d re

sults

sim

ilar t

o A

pollo

-era

test

ing

•Fr

ayed

mat

eria

ls m

ore

reac

tive

•N

o di

stin

guis

habl

e di

ffere

nce

betw

een

horiz

onta

l sa

mpl

es a

nd v

ertic

al s

ampl

es•

Test

s pe

rform

ed a

t 23.

5 ps

ia10

0% O

2, 2

2.5

V–

7 m

ater

ials

test

ed–

Cur

rent

requ

ired

for i

gniti

on ra

nged

from

0

.8 A

to 1

.4 A

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Entir

e D

ata

Plot

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Clo

seup

Dat

a Pl

ot

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Scra

tch

Test

Pro

blem

s

•N

ot p

ossi

ble

to d

eter

min

e w

hich

arc

igni

ted

mat

eria

l•

Arc

ene

rgie

s va

ry w

idel

y fro

m te

st to

test

and

arc

to a

rc•

Diff

icul

t to

ensu

re th

at te

st s

ampl

e m

ater

ial i

s in

intim

ate

cont

act w

ith a

rcin

g ev

ent

•C

onfig

urat

ion

not r

ealis

tic fo

r ins

ide

spac

esui

t bec

ause

of

siz

e of

sty

lus

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Poke

Tes

t Obj

ectiv

es

•D

eter

min

e w

heth

er m

ore

seve

re to

arc

with

wire

s or

st

ylus

•D

eter

min

e w

heth

er m

ore

seve

re to

arc

in s

ingl

e lo

catio

n (p

oke

test

) or m

ultip

le lo

catio

ns (s

crat

ch te

st)

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Poke

Tes

t Res

ults

•P

oke

test

resu

lts c

onsi

sten

t with

scr

atch

test

resu

lts–

No

dete

ctab

le d

iffer

ence

bet

wee

n ar

cing

in o

ne lo

catio

n or

m

ultip

le lo

catio

ns

•Te

sts

show

ed th

at it

is m

ore

seve

re to

arc

with

a w

ire

than

a s

tylu

s

–W

ires

are

flam

mab

le a

nd c

an b

urn

in o

xyge

n–

Bur

ning

wire

s ea

sily

igni

te te

st m

ater

ials

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Poke

Tes

t Pro

blem

s

•N

ot p

ossi

ble

to d

eter

min

e w

hich

arc

igni

ted

mat

eria

l•

Arc

ene

rgie

s va

ry w

idel

y fro

m te

st to

test

and

arc

to a

rc•

Diff

icul

t to

ensu

re th

at te

st s

ampl

e m

ater

ial i

s in

intim

ate

cont

act w

ith a

rcin

g ev

ent

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Wire

-bre

ak T

est O

bjec

tives

•R

educ

e va

riabi

lity

in te

sts

•Te

st a

ll m

ater

ials

•D

eter

min

e w

heth

er ig

nitio

n is

dep

ende

nt o

n vo

ltage

or

curr

ent

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Page 20: Electrical Arc Ignition Testing of Spacesuit Materials

9.00

1550

0.00

6334

0.35

150.

0006

254

0.45

240.

0007

852

0.50

300.

0008

851

0.63

390.

001

50

0.70

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0011

49

0.83

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0012

48

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0014

47

1.10

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0.00

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1.50

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244

1.80

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0.00

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2.30

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5.00

625

0.00

438

App

roxi

mat

e C

urre

nt

Req

uire

d to

Bre

ak W

ire

(A)

% o

f Flig

ht W

ire C

ross

S

ectio

nal A

rea

Dia

met

er (i

n.)

AW

G S

ize

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Cot

ton

Wire

-Bre

ak T

est V

ideo

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Hig

h Sp

eed

Cot

ton

Wire

-bre

ak T

est V

ideo

Wire

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Typi

cal D

ata

Plot

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Clo

seup

Dat

a Pl

ot

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Wire

-bre

ak T

est R

esul

ts

•M

uch

mor

e se

vere

than

scr

atch

and

pok

e te

sts

•Te

st c

ondi

tions

–23

.5 p

sia

100%

O2,

22.

5 V

–50

psi

a50

% O

2 an

d 50

% N

2, 1

5 V

•S

ever

al m

ater

ials

faile

d te

stin

g at

the

low

est p

ossi

ble

curr

ent,

~0.3

A•

Cur

rent

requ

ired

for i

gniti

on fo

r mos

t mat

eria

ls ra

nged

fro

m <

0.3

A to

0.9

7 A

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Wire

-Bre

ak T

est R

esul

ts (c

ont.)

•G

ore-

Tex

only

igni

ted

unde

r muc

h m

ore

seve

re

cond

ition

s–

100%

O2,

54

psia

–Zi

gzag

wire

con

figur

atio

n

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Wire

-bre

ak T

ests

vs.

Scr

atch

Tes

ts

1.3

0.49

LCV

G tr

icot

1.4

0.53

LCVG

spa

ndex

1.4

0.64

Ast

rona

ut u

nder

garm

ent

1.3

0.59

Nyl

on/L

ycra

Com

mC

ap

0.700.3

0.36

Wire

Tes

t Ava

ilabl

e C

urre

nt

at Ig

nitio

n (A

)

1.4

UC

N (s

hiny

sid

e)

0.8

Mol

eski

n

0.95

Gen

eric

cot

ton

Scr

atch

Tes

t Ava

ilabl

e C

urre

nt a

t Ign

ition

(A)

Mat

eria

l

23.5

psi

a10

0% O

2, 2

2.5

V

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Ure

than

e-co

ated

Nyl

on

0510152025303540

01

23

45

67

Cur

rent

(A)

Voltage (V)

No

Igni

tion

Igni

tion

21.8

Wat

t Pow

er C

urve

2.5

V, 4

.99

A

Page 29: Electrical Arc Ignition Testing of Spacesuit Materials

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Mol

eski

n

051015202530

00.

10.

20.

30.

40.

50.

60.

7

Cur

rent

(A)

Voltage (V)

6.8

Wat

t Pow

er C

urve

Igni

tion

No

Igni

tion

1.3

V, 0

.25

A

Page 30: Electrical Arc Ignition Testing of Spacesuit Materials

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Page 31: Electrical Arc Ignition Testing of Spacesuit Materials

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Con

clus

ions

•W

ire-b

reak

test

is w

orst

-cas

e•

Fuzz

y m

ater

ials

gen

eral

ly e

asie

r to

igni

te•

Cur

rent

app

ears

to h

ave

grea

ter e

ffect

than

vol

tage

•C

ontro

lling

risk

mus

t inc

lude

bot

h–

Phy

sica

l iso

latio

n of

eas

y to

igni

te m

ater

ials

–Li

miti

ng c

urre

nt a

nd v

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ge