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ABSTRACT Inflatable Structures: Test Results and Development Progress since TransHab JSC’s TransHab project was the first successful development program to prove the viability of inflatable habitats for space applications [1][2][3]. Although TransHab was cancelled in 2000, significant progress has been made this past year by JSC engineers. Since February 2005, the following test articles have been manufactured and tested: An 88-in diameter restraint layer was pressure-tested to failure and reached an ultimate pressure of 197psi. This test article demonstrated the ability to build a 35- foot diameter inflatable with a factor of safety of 4.0 at 10.2 psi. An 88-in diameter restraint layer with a window frame incorporated into the restraint layer was tested to failure and reached an ultimate pressure of 197 psi. This test article demonstrated the ability to incorporate windows and other structural penetrations in the woven restraint layer without reducing its strength. An 88-inch diameter folding demonstrator that includes a bladder, restraint layer, and all of the MMOD shell layers was manufactured and assembled. This test article demonstrated an improved and simplified shell assembly and folding technique which installs pre-folded shell sections in a controlled manner. Fifth-scale MMOD hypervelocity test articles have demonstrated fiberglass as a viable material for a MMOD bumper shield which is cheaper and more readily available than previously used materials. In addition, four different full-scale advanced shape inflatable mockups have been manufactured and evaluated for applications such as lunar habitats, airlocks, and transfer tunnels. United States Patent, Inflatable Vessel and Method, 6,547,189, April 2003 1. TransHab: NASA's Large-scale Inflatable Spacecraft, American Institute of 2. Aeronautics and Astronautics, Inc. 2000-1822, 3/06/2000. Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space 3. Applications, Chapter 21, American Institute of Aeronautics and Astronautics, Inc., 2001, Progress In Astronautics and Aeronautics - Volume 191. https://ntrs.nasa.gov/search.jsp?R=20060022083 2020-07-04T17:14:15+00:00Z
Transcript
Page 1: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

ABSTRACT

Inflatable Structures: Test Results and Development Progress since TransHab

JSC’s TransHab project was the first successful development program to prove the viability of inflatable habitats for space applications [1][2][3]. Although TransHab was cancelled in 2000, significant progress has been made this past year by JSC engineers.

Since February 2005, the following test articles have been manufactured and tested:

An 88-in diameter restraint layer was pressure-tested to failure and reached an •ultimate pressure of 197psi. This test article demonstrated the ability to build a 35-foot diameter inflatable with a factor of safety of 4.0 at 10.2 psi.

An 88-in diameter restraint layer with a window frame incorporated into the •restraint layer was tested to failure and reached an ultimate pressure of 197 psi. This test article demonstrated the ability to incorporate windows and other structural penetrations in the woven restraint layer without reducing its strength.

An 88-inch diameter folding demonstrator that includes a bladder, restraint layer, •and all of the MMOD shell layers was manufactured and assembled. This test article demonstrated an improved and simplified shell assembly and folding technique which installs pre-folded shell sections in a controlled manner.

Fifth-scale MMOD hypervelocity test articles have demonstrated fiberglass as a •viable material for a MMOD bumper shield which is cheaper and more readily available than previously used materials.

In addition, four different full-scale advanced shape inflatable mockups have been manufactured and evaluated for applications such as lunar habitats, airlocks, and transfer tunnels.

United States Patent, Inflatable Vessel and Method, 6,547,189, April 20031.TransHab: NASA's Large-scale Inflatable Spacecraft, American Institute of 2.Aeronautics and Astronautics, Inc. 2000-1822, 3/06/2000.Gossamer Spacecraft: Membrane and Inflatable Structures Technology for Space 3.Applications, Chapter 21, American Institute of Aeronautics and Astronautics, Inc., 2001, Progress In Astronautics and Aeronautics - Volume 191.

https://ntrs.nasa.gov/search.jsp?R=20060022083 2020-07-04T17:14:15+00:00Z

Page 2: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

Infla

tabl

e S

truct

ures

JSC

Tes

t Res

ults

and

Dev

elop

men

tP

rogr

ess

sinc

e Tr

ansH

ab

Chr

is J

ohns

onG

ary

Spe

xart

h

Page 3: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

2

Ove

rvie

w

JSC

’sTr

ansH

abpr

ojec

t was

the

first

suc

cess

ful d

evel

opm

ent

prog

ram

to p

rove

the

viab

ility

of in

flata

ble

habi

tats

for

spac

e ap

plic

atio

ns.

It de

mon

stra

ted

the

man

ufac

turin

g, s

truct

ural

load

ing,

m

icro

met

eoro

id /

orbi

tal d

ebris

(MM

OD

) pro

tect

ion,

fold

ing,

an

d de

ploy

men

t cap

abili

ties

for a

n in

flata

ble

habi

tat.

Alth

ough

Tra

nsH

abw

as c

ance

lled

in 2

000,

sig

nific

ant

prog

ress

has

bee

n m

ade

this

pas

t yea

r by

JSC

eng

inee

rs

Page 4: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

3

Ove

rvie

w

•S

ince

Feb

ruar

y 20

05, t

he fo

llow

ing

dem

onst

ratio

n te

st

artic

les

have

bee

n m

anuf

actu

red

and

test

ed–

88”D

iam

eter

Res

train

t Lay

er (R

/L) T

est A

rticl

e–

88”D

iam

eter

R/L

with

Inte

grat

ed W

indo

w F

ram

e Te

st A

rticl

e–

88”D

iam

eter

She

ll Fo

ldin

g D

emon

stra

tor

–Fi

fth S

cale

MM

OD

Hyp

erve

loci

ty T

est A

rticl

es–

Adv

ance

d In

flata

ble

Stru

ctur

e S

hape

Moc

kups

•D

esig

ned

by J

SC

Eng

inee

rs

–88

”dia

met

er te

st a

rticl

es a

nd a

dvan

ced

shap

e m

ocku

ps

man

ufac

ture

d an

d te

sted

at B

igel

ow A

eros

pace

faci

litie

s–

MM

OD

hyp

erve

loci

ty te

st a

rticl

es m

anuf

actu

red

and

test

ed a

t JS

C a

nd W

hite

San

ds fa

cilit

ies

Page 5: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

4

•Th

ese

dem

onst

ratio

n te

st a

rticl

es in

crea

sed

the

deve

lopm

ent o

f the

follo

win

g:–

Res

train

t Lay

er–

Win

dow

/ R

estra

int L

ayer

Inte

grat

ion

–S

hell

Ass

embl

y, F

oldi

ng, &

Inst

alla

tion

–S

hell

MM

OD

Mat

eria

ls–

Adv

ance

d In

flata

ble

Sha

pes

Con

tent

s

Page 6: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

5

Con

tent

s

•Th

ese

dem

onst

ratio

n te

st a

rticl

es in

crea

sed

the

deve

lopm

ent o

f the

follo

win

g:–

Res

train

t Lay

er–

Win

dow

/ R

estra

int L

ayer

Inte

grat

ion

–S

hell

Ass

embl

y, F

oldi

ng, &

Inst

alla

tion

–S

hell

MM

OD

Mat

eria

ls–

Adv

ance

d In

flata

ble

Sha

pes

Page 7: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

6

•Tr

ansH

ab (1

997

–20

00)

–C

HA

LLE

NG

ES

: •

Fabr

ic te

nsile

load

incr

ease

s as

a fu

nctio

n of

dia

met

er.

•Fa

ctor

of S

afet

y (F

OS

) of 4

.0 u

sed

(per

FA

A A

irshi

p R

equi

rem

ents

)–

Bui

lt th

ree

23-fo

ot d

iam

eter

rest

rain

t lay

ers

in 8

-mon

th p

erio

d •

2 fo

r hyd

rost

atic

test

ing

–W

oven

rest

rain

t lay

er te

sted

up

to F

OS

=4.0

–**

Hig

hest

load

ed in

flata

ble

in h

isto

ry *

*•

1 fo

r fol

ding

and

dep

loym

ent i

n th

erm

al v

acuu

m

Res

train

t Lay

er

FOS

= 2

.0 o

n U

ltim

ate

(ver

ified

by

test

May

199

8)FO

S =

4.0

on

Ulti

mat

e(v

erifi

ed b

y te

st S

ept 1

998)

Full-

scal

e Th

erm

al-V

acTe

st A

rticl

e(1

999)

Page 8: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

7

•JS

C D

evel

opm

ent (

2004

–Pr

esen

t)–

GO

AL:

Pre

ssur

ize

a w

oven

rest

rain

t lay

er to

failu

re to

und

erst

and

the

failu

re

mod

es, s

afet

y m

argi

ns, a

nd o

ther

asp

ects

of d

esig

n–

Des

igne

d an

d bu

ilt a

n 88

”dia

met

er R

estra

int L

ayer

test

arti

cle

–H

ydro

stat

ic T

est,

Nov

embe

r 200

5•

Faile

d at

197

psi

(exc

eeds

FO

S=4

.0 fo

r 30-

ft di

am

odul

e at

10.

7 ps

i)–

Impr

oved

Des

ign

Tool

s an

d M

anuf

actu

ring

Pro

cess

es

Res

train

t Lay

er

Page 9: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

8

Res

train

t Lay

er

Page 10: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

9

Pre

dict

ed fa

ilure

mod

e an

d lo

catio

n.

0.00

0 se

c.

0.03

3 se

c.

0.06

6 se

c.

Res

train

t Lay

erPr

essu

re =

197

psi

Page 11: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

10

Res

train

t Lay

er

•R

ES

ULT

S–

Dem

onst

rate

d R

estra

int L

ayer

Cap

abili

ty•

Exc

eeds

FO

S=4

.0 fo

r 30-

ft di

am

odul

e at

10.

7 ps

i•

Ena

bled

cor

rela

tion

to a

naly

sis

•E

nabl

ed u

nder

stan

ding

of k

nock

dow

n fa

ctor

s•

Dem

onst

rate

d re

peat

abili

ty o

f man

ufac

turin

g•

Dem

onst

rate

d fir

st p

redi

cted

failu

re m

ode

–B

igel

ow A

eros

pace

pla

ns to

use

this

des

ign

on G

alax

y cl

ass

vehi

cles

•P

lann

ed la

unch

mid

to la

te 2

007

Page 12: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

11

Con

tent

s

•Th

ese

dem

onst

ratio

n te

st a

rticl

es in

crea

sed

the

deve

lopm

ent o

f the

follo

win

g:–

Res

train

t Lay

er–

Win

dow

/ R

estra

int L

ayer

Inte

grat

ion

–S

hell

Ass

embl

y, F

oldi

ng, &

Inst

alla

tion

–S

hell

MM

OD

Mat

eria

ls–

Adv

ance

d In

flata

ble

Sha

pes

Page 13: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

12

Win

dow

Fra

me

/ Res

train

t Int

egra

tion

•Tr

ansH

ab (1

997

–20

00)

–C

HA

LLE

NG

ES

: •

Inst

all a

win

dow

fram

e or

“pa

ss-th

roug

h”in

an

infla

tabl

e st

ruct

ure.

•M

inim

ize

Impa

ct to

Bla

dder

/ R

estra

int L

ayer

–D

esig

ned

Con

cept

ual W

indo

w•

Nev

er M

anuf

actu

red,

Nev

er T

este

d

Page 14: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

13

Win

dow

Fra

me

/ Res

train

t Int

egra

tion

•JS

C D

evel

opm

ent (

2005

–Pr

esen

t)–

GO

AL:

Pre

ssur

ize

a w

oven

rest

rain

t lay

er w

ith a

win

dow

to fa

ilure

•D

eter

min

e w

indo

w e

ffect

s on

bla

dder

and

rest

rain

t lay

er.

–D

esig

ned

and

built

an

88”d

iam

eter

R/L

with

inte

grat

ed w

indo

w fr

ame

test

arti

cle

•D

emon

stra

te in

tegr

atio

n of

win

dow

fram

e in

to re

stra

int l

ayer

& c

apab

ility

–Im

prov

ed w

indo

w fr

ame

desi

gn–

Dev

elop

ed re

stra

int l

ayer

mod

ifica

tion

–D

evel

oped

man

ufac

turin

g &

inst

alla

tion

proc

esse

s

–H

ydro

stat

ic T

est,

Mar

ch 2

006

•Fa

iled

at 1

97 p

si(s

ame

as w

ithou

t win

dow

)•

No

loss

in p

erfo

rman

ce d

ue to

dis

cont

inui

ty

Page 15: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

14

Win

dow

Fra

me

/ Res

train

t Int

egra

tion

•R

ES

ULT

S–

Dem

onst

rate

d w

indo

w fr

ame

/ res

train

t cap

abili

ty•

Rea

ched

sam

e ul

timat

e ca

pabi

lity

of re

stra

int w

ithou

t win

dow

•E

nabl

ed c

hara

cter

izat

ion

of lo

ad d

istri

butio

n ar

ound

win

dow

fram

e•

Dem

onst

rate

d fir

st p

redi

cted

failu

re m

ode

–B

igel

ow A

eros

pace

pla

ns to

use

this

des

ign

on fu

ll sc

ale

clas

s ve

hicl

es•

Pla

nned

laun

ch T

BD

Page 16: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

15

Con

tent

s

•Th

ese

dem

onst

ratio

n te

st a

rticl

es in

crea

sed

the

deve

lopm

ent o

f the

follo

win

g:–

Res

train

t Lay

er–

Win

dow

/ R

estra

int L

ayer

Inte

grat

ion

–S

hell

Ass

embl

y, F

oldi

ng, &

Inst

alla

tion

–S

hell

MM

OD

Mat

eria

ls–

Adv

ance

d In

flata

ble

Sha

pes

Page 17: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

16

•Tr

ansH

ab (1

997

–20

00)

–C

HAL

LEN

GE:

Fold

12,

000

lbs

of m

ulti-

laye

r fab

ric•

Com

poun

d cu

rved

sha

pe m

ust b

e fo

lded

into

a c

ylin

der s

hape

to fi

t in

to la

unch

veh

icle

–S

hell

inst

alle

d on

veh

icle

in d

eplo

yed

conf

igur

atio

n–

Veh

icle

def

late

d, s

hell/

rest

rain

t fol

ded

usin

g G

roun

d S

uppo

rt E

quip

men

t (G

SE

)•

Fold

Lin

es d

eter

min

ed fr

om s

cale

d m

odel

–P

robl

ems

•C

umbe

rsom

e te

chni

que

due

to h

eavy

mat

eria

l•

Inad

equa

te G

SE

/ ve

rtica

l con

figur

atio

n•

Diff

icul

t to

fold

in c

ompo

und

curv

ed re

gion

She

ll A

ssy,

Fol

ding

, Veh

icle

Inst

alla

tion

1998

Tran

sHab

JSC

Eng

inee

ring

Uni

t

Res

trai

nt L

ayer

MLI

AO

Cov

er

MM

OD

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ldin

g

Bag

ged

Foam

Bum

per M

ater

ial

Bla

dder

Page 18: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

17

She

ll A

ssy,

Fol

ding

, Veh

icle

Inst

alla

tion

•JS

C D

evel

opm

ent (

2005

–Pr

esen

t)–

GO

AL:

Dem

onst

rate

sim

plifi

ed d

esig

n, a

ssem

bly,

and

in

stal

latio

n of

she

ll –

rega

rdle

ss o

f siz

e an

d/or

mas

s.–

Des

igne

d an

d bu

ilt a

n 88

”dia

met

er S

hell

Fold

ing

Dem

onst

rato

r

–D

evel

oped

new

fold

con

figur

atio

n•

Gor

e pa

ttern

s an

d fo

ld li

nes

mat

hem

atic

ally

def

ined

Sim

plifi

ed th

e de

sign

•S

impl

ified

the

asse

mbl

y &

inst

alla

tion

(min

imal

GS

E)

–D

evel

oped

des

ign

softw

are

tool

–D

evel

oped

des

ign

of s

hell

with

inte

grat

ed w

indo

w

–Fo

ldin

g an

d de

ploy

men

t dem

onst

ratio

n, F

eb. 2

006

Page 19: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

05-1

9-06

Chr

is J

ohns

on, G

ary

Spe

xarth

18

She

ll A

ssy,

Fol

ding

, Veh

icle

Inst

alla

tion

•R

ES

ULT

S–

Dem

onst

rate

d ne

w fo

ld c

onfig

urat

ion

•P

rove

d th

e si

mpl

ified

des

ign

conc

ept

•D

esig

n is

sca

labl

e to

larg

er s

ize

infla

tabl

es•

Ena

bled

cor

rela

tion

to s

tow

ed th

ickn

ess

pred

ictio

n

–B

igel

ow A

eros

pace

pla

ns to

use

this

des

ign

on G

alax

y cl

ass

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cles

•P

lann

ed la

unch

mid

to la

te 2

007

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Chr

is J

ohns

on, G

ary

Spe

xarth

19

Con

tent

s

•A

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plis

hmen

ts o

ver p

ast 1

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Res

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t Lay

er–

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ayer

Inte

grat

ion

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hell

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ing

Dem

onst

ratio

n–

She

ll M

MO

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estin

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Adv

ance

d S

hape

s

Page 21: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

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Chr

is J

ohns

on, G

ary

Spe

xarth

20

•Tr

ansH

ab (1

997

–20

00)

–C

HA

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NG

E:

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n a

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ble

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/ or

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l deb

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at c

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lded

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ified

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ove

r 100

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)•

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NA

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irem

ent

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top

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cle

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km

/sec

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icle

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TransHab Interior

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ll M

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Page 22: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

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Chr

is J

ohns

on, G

ary

Spe

xarth

21

•JS

C D

evel

opm

ent (

2005

–Pr

esen

t)–

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AL:

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ine

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ate

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ial

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w c

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ater

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sted

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ing

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rmed

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natio

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lect

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form

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onal

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listic

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ns to

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ll M

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estin

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Chr

is J

ohns

on, G

ary

Spe

xarth

22

•A

ccom

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ast 1

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elow

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ston

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ility

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ion

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hell

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onst

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She

ll M

MO

D T

estin

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Adv

ance

d S

hape

s

Page 24: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

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Chr

is J

ohns

on, G

ary

Spe

xarth

23

Adv

ance

d S

hape

s

•N

ew In

flata

ble

Sha

pe D

evel

opm

ent

–La

rge

Dia

met

er, S

hort

Hei

ght I

nfla

tabl

e S

truct

ures

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ffici

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n pr

essu

re lo

adin

g•

Des

irabl

e fo

r gra

vita

tiona

l env

ironm

ent a

rchi

tect

ure

–Lu

nar a

nd/o

r pla

neta

ry h

abita

t

–“C

orel

ess”

Infla

tabl

e S

truct

ures

•N

o in

tern

al ri

gid

core

stru

ctur

e•

Des

irabl

e fo

r sm

all s

tow

ed p

acki

ng v

olum

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itatio

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ck

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sfer

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nels

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o in

tern

al ri

gid

core

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ctur

e•

Not

a b

ody

of re

volu

tion

Page 25: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

BA

CK

UP

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Chr

is J

ohns

on, G

ary

Spe

xarth

25

JSC

Pas

t Inf

lata

ble

Dev

elop

men

t Pro

ject

s

•Tr

ansH

ab–

Tran

sit H

abita

tion

Mod

ule

–IS

S H

abita

tion

Mod

ule

•H

yper

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Cha

mbe

r

•A

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k–

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ell d

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n un

der N

AS

A c

ontra

ct

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igel

ow D

evel

opm

ent A

eros

pace

Par

tner

ship

Page 27: ABSTRACT - NASA · – Restraint Layer – Window / Restraint Layer Integration – Shell Assembly, Folding, & Installation – Shell MMOD Materials – Advanced Inflatable Shapes

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Chr

is J

ohns

on, G

ary

Spe

xarth

26

App

licat

ions


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