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OVERVIEW OF NASA’S UEET AND TBCC/RTA PROGRAMS
National Aeronautics and Space Administration Glenn Research Center
Cleveland, Ohio
OverviewOverviewof theof the
Ultra Efficient Engine Technology (UEET) Ultra Efficient Engine Technology (UEET) ProgramProgram
Robert J. ShawRobert J. ShawCatherine L. Catherine L. PeddiePeddie
NASA Seal/Secondary Air System WorkshopNASA Seal/Secondary Air System WorkshopOctober 23, 2002October 23, 2002
NASA/CP—2003-212458/VOL1 59
Robert J. Shaw and Catherine L . Peddie
Red
uce
emis
sion
s of
futu
re a
ircra
ft by
a fa
ctor
of t
hree
with
in 1
0 ye
ars
(200
7),
(200
7),
and
by a
fact
or o
f fiv
e w
ithin
20
year
s.N
ASA
Thre
e Pi
llars
for S
ucce
ss-1
997
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Rev
olut
ioni
ze A
viat
ion
Goa
l
Em
issi
ons
Obj
ectiv
e
Red
uce
NO
x em
issi
ons
of fu
ture
airc
raft
by 7
0 pe
rcen
t with
in 1
0 ye
ars,
and
by 8
0 pe
rcen
t with
in 2
5 ye
ars
(usi
ng th
e 19
96 IC
AO S
tand
ard
for N
Ox
as th
eba
selin
e. R
educ
e C
O2
emis
sion
s of
futu
re a
ircra
ft by
25
perc
ent a
nd b
y 50
per
cent
In th
e sa
me
timef
ram
es (u
sing
199
7 su
bson
ic a
ircra
ft te
chno
logy
as
the
base
line)
.
NAS
A Ae
rosp
ace
Tech
nolo
gy E
nter
pris
e St
rate
gic
Plan
-200
1
UEE
T w
ill b
e th
e re
spon
sibl
e pr
opul
sion
pro
gram
for d
eliv
erin
g o
UEE
T w
ill b
e th
e re
spon
sibl
e pr
opul
sion
pro
gram
for d
eliv
erin
g o n
this
obj
ectiv
e!n
this
obj
ectiv
e!
NASA/CP—2003-212458/VOL1 60
The
UEE
T Pr
ogra
m w
ill d
evel
op a
nd tr
ansf
er to
the
U. S
. in
dust
ry c
ritic
al g
as tu
rbin
e en
gine
tech
nolo
gies
whi
ch w
ill
cont
ribut
e to
“en
ablin
g a
safe
, sec
ure,
and
env
ironm
enta
lly
frie
ndly
air
tran
spor
tatio
n sy
stem
”.
NASA/CP—2003-212458/VOL1 61
* LTO
* L
TO --
Land
ing/
Take
-off
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Visi
on:
Dev
elop
and
han
d of
f rev
olut
iona
ry tu
rbin
e en
gine
pr
opul
sion
tech
nolo
gies
that
will
ena
ble
futu
re g
ener
atio
n ve
hicl
es o
ver a
wid
e ra
nge
of fl
ight
spe
eds.
Goa
ls:
Prop
ulsi
on te
chno
logi
es to
ena
ble
incr
ease
s in
sys
tem
ef
ficie
ncy
and,
ther
efor
e, fu
el b
urn
redu
ctio
ns o
f up
to 1
5 %
(e
quiv
alen
t red
uctio
ns in
CO
2)
Com
bust
or te
chno
logi
es (c
onfig
urat
ion
and
mat
eria
ls)
whi
ch w
ill e
nabl
e re
duct
ions
in L
TO* N
Ox
of 7
0% re
lativ
e to
19
96 IC
AO
sta
ndar
ds.
NASA/CP—2003-212458/VOL1 62
Prog
ram
Tech
nica
l Obj
ectiv
esTe
chni
cal O
bjec
tives
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
15%
fuel
bur
n re
duct
ion
for
larg
e su
bson
ic a
ircra
ft
8% fu
el b
urn
redu
ctio
n fo
r sm
all s
ubso
nic,
sm
all /
larg
e su
pers
onic
70%
N0x
redu
ctio
n (b
elow
ICAO
96)
for s
ubso
nic
(larg
e/ re
gion
al) c
ombu
stor
s ov
er th
e LT
O c
ycle
Goa
lM
inim
um S
ucce
ss C
riter
ia
12%
fuel
bur
n re
duct
ion
for
larg
e su
bson
ic a
ircra
ft
4% fu
el b
urn
redu
ctio
n fo
r sm
all s
ubso
nic,
sm
all /
larg
e su
pers
onic
65%
N0x
redu
ctio
n
(larg
e/ re
gion
al) c
ombu
stor
s ov
er th
e LT
O c
ycle
(bel
ow IC
AO 9
6) fo
r sub
soni
c
CO
2G
oal
NO
xG
oal
NASA/CP—2003-212458/VOL1 63
NA
SA’s
Tec
hnol
ogy
Rea
dine
ss L
evel
(TR
L) S
cale
TRL
Gen
eral
NAS
A D
efin
ition
9Ac
tual
sys
tem
“fli
ght p
rove
n” o
n op
erat
iona
l flig
ht
8Ac
tual
sys
tem
com
plet
ed a
nd “
fligh
t qu
alifi
ed”
thro
ugh
test
and
dem
onst
ratio
n
7Sy
stem
pro
toty
pe d
emon
stra
ted
in fl
ight
en
viro
nmen
t
6Sy
stem
/sub
syst
em m
odel
or p
roto
type
de
mon
stra
ted/
valid
ated
in a
rele
vant
en
viro
nmen
t
5C
ompo
nent
and
/or b
read
boar
d ve
rific
atio
n in
a re
leva
nt e
nviro
nmen
t
4C
ompo
nent
and
/or b
read
boar
d te
st in
a
labo
rato
ry e
nviro
nmen
t
3An
alyt
ical
and
exp
erim
enta
l crit
ical
fu
nctio
n, o
r cha
ract
eris
tic p
roof
-of-
conc
ept
2Te
chno
logy
con
cept
and
/or a
pplic
atio
n fo
rmul
ated
(can
dida
te s
elec
ted)
1B
asic
prin
cipl
es o
bser
ved
and
repo
rted
Syst
em T
est a
nd O
pera
tions
Syst
em/S
ubsy
stem
Dev
elop
men
t
Tech
nolo
gy D
emon
stra
tion
Tech
nolo
gy D
evel
opm
ent
Res
earc
h to
Pro
ve F
easi
bilit
y
Bas
ic T
echn
olog
y R
esea
rch
Indu
stry
R
ole
Gov
ernm
ent
Rol
e
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
UEE
T
In p
artn
ersh
ip w
ith
DO
D, i
ndus
try
NASA/CP—2003-212458/VOL1 64
Em
issi
ons R
educ
tion
GR
C L
ead
GR
C L
ead
Inte
grat
ed C
ompo
nent
T
echn
olog
y D
emon
stra
tions
Mat
eria
ls a
nd S
truc
ture
s for
H
igh
Perf
orm
ance
GR
C L
ead
Prop
ulsi
on-A
irfr
ame
Inte
grat
ion
LaR
C L
ead
Hig
hly
Loa
ded
Tur
bom
achi
nery
GR
C L
ead
UEE
T Pr
ojec
ts
Inte
llige
nt P
ropu
lsio
nC
ontr
ols
GR
C L
ead
GR
C L
ead
Prop
ulsi
on S
yste
ms
Inte
grat
ion
and
Ass
essm
ent
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
NASA/CP—2003-212458/VOL1 65
Unm
anne
d Ae
rial
Vehi
cle
(UAV
)
Non-Commercial Vehicles
Acce
ss-to
-Sp
ace/
Hig
h M
ach
Plat
form
Gen
eral
Av
iatio
n Ai
rcra
ft (G
A)
4 PA
X
Commercial Vehicles
Subs
onic
Supe
rson
icH
yper
soni
c
Reg
iona
l Jet
Tr
ansp
ort
Larg
e Su
bson
ic
Tran
spor
t
300
PAX
50 P
AX
Hig
h Sp
eed
Civ
il Tr
ansp
ort
(HSC
T)
300
PAX
Supe
rson
ic
Busi
ness
Jet
(S
BJ)
10 P
AX
Blen
ded
Win
g Bo
dy
(BW
B)
500-
600
PAX Milit
ary
Tran
spor
t (C
-17)
Adva
nced
Fig
hter
Bas
elin
e Ve
hicl
es fo
r UEE
TP T
echn
olog
y A
pplic
atio
n St
udie
sU
ltra
Effic
ient
Eng
ine
Tech
nolo
gyU
ltra
Effic
ient
Eng
ine
Tech
nolo
gy
Thes
e ve
hicl
esdr
ive
the
tech
nolo
gyin
vest
men
t str
ateg
y
Thes
e ve
hicl
esde
term
ine
the
tech
nolo
gysy
nerg
ies
NASA/CP—2003-212458/VOL1 66
2015
“U
ltim
ate”
Tur
bine
Engi
ne S
yste
ms
•Em
issi
ons
•Fu
el b
urn
•W
eigh
t•
Noi
se•
Safe
ty•
Rel
iabi
lity
Perio
dic
asse
ssm
ents
/re
bal
anci
ngof
por
tfolio
Inte
grat
ed c
ompo
nent
te
chno
logy
val
idat
ions
(in
cos
t-sha
ring
part
ners
hip
with
oth
er
gove
rnm
ent a
genc
ies
and/
or in
dust
ry)
The
UEE
T “R
oadm
ap”
UEET
Tec
hnol
ogie
s
•Com
pone
nts
•Mat
eria
ls a
nd s
truct
ures
•Int
ellig
ent p
ropu
lsio
n co
ntro
ls
•Pro
puls
ion-
airfr
ame
inte
grat
ion
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
NASA/CP—2003-212458/VOL1 67
Dev
elop
and
han
d of
f rev
olut
iona
ry p
ropu
lsio
n tu
rbin
e en
gine
tec
Dev
elop
and
han
d of
f rev
olut
iona
ry p
ropu
lsio
n tu
rbin
e en
gine
tec h
nolo
gies
that
hn
olog
ies
that
w
ill en
able
futu
re g
ener
atio
n ve
hicl
es o
ver a
wid
e ra
nge
of fl
igw
ill en
able
futu
re g
ener
atio
n ve
hicl
es o
ver a
wid
e ra
nge
of fl
ight
spe
eds.
ht s
peed
s.
Visi
on
We
supp
ort t
he v
isio
n an
d ar
e co
mm
itted
to th
e su
cces
s of
N
ASA
’s U
ltra
Effic
ient
Eng
ine
Tech
nolo
gy (U
EET)
Pro
gram
.
Will
iam
s In
tern
atio
nal
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Rob
ert D
. Sou
thw
ick,
Pra
tt &
Whi
tney
Fred
Kra
use,
Gen
eral
Ele
ctric
Airc
raft
Engi
nes
Dim
itri M
avris
, Geo
rgia
Tec
h
Mah
moo
d N
aim
i, B
oein
g C
omm
erci
al A
irpla
ne C
ompa
ny
Tom
Har
tman
n, L
ockh
eed-
Mar
tin
Scot
t Cru
zen,
Will
iam
s Int
erna
tiona
l
Ger
ald
Brin
es, A
lliso
n-R
olls
Roy
ce
Rob
ert J
. Sha
w, N
ASA
Gle
nn R
esea
rch
Cen
ter
Ric
hard
Hill
, Air
Forc
e R
esea
rch
Labo
rato
ryV
inod
Nan
gia,
Hon
eyw
ell
NASA/CP—2003-212458/VOL1 68
UEE
T Pa
rtne
rshi
psU
ltra
Effic
ient
Eng
ine
Tech
nolo
gyU
ltra
Effic
ient
Eng
ine
Tech
nolo
gy
Part
ner
Com
men
tsB
oein
g, L
ockh
eed-
Mar
tin, G
E, P
&W
, H
oney
wel
l, A
AD/R
R, W
illia
ms,
Geo
rgia
Tec
hO
n tr
ack
to p
rovi
de >
$50M
of d
irect
in k
ind
cont
ribut
ions
to o
vera
ll U
EET
Prog
ram
NAS
A Q
uiet
Airc
raft
Tech
nolo
gy (Q
AT)
Prog
ram
NAS
A Ad
vanc
ed S
pace
Tra
nspo
rtat
ion
Prog
ram
(AST
P)
NAS
A Pr
opul
sion
and
Pow
er
Prog
ram
(APP
)
EPA
FAA
DO
D (I
HPT
ET/V
AATE
)
DO
E
Qin
etiQ
(UK
)
Nat
iona
l Tec
hnol
ogy
Tran
sfer
C
ente
r (N
TTC
)
Shar
ed d
evel
opm
ent o
f fan
tech
nolo
gies
Tech
nolo
gy in
sert
ion
oppo
rtun
ities
on
TBC
C/R
TA d
emon
stra
tors
Shar
ed re
spon
sibi
lity
in s
imul
atio
n to
ol
deve
lopm
ent;
revo
lutio
nary
low
er T
RL
tech
nolo
gies
Envi
ronm
enta
l com
patib
ility
of t
echn
olog
ies
Pre
cert
ifica
tion
“iss
ues”
of t
echn
olog
ies
Tech
nolo
gy in
sert
ion
on IH
PTET
/VAA
TE d
emos
; co
llabo
ratio
n on
mat
eria
ls d
evel
opm
ent/s
tudi
es;
supp
ort f
or D
ual S
pool
Tur
bine
faci
lity
(DST
F)
Tech
nolo
gy in
sert
ion
on g
roun
d po
wer
dem
os
Tech
nolo
gy tr
ansf
er to
non
aer
ospa
ce
com
mun
ity
Emis
sion
s m
odel
ing
valid
atio
n da
ta s
ets
UEE
T is
all
abou
t par
tner
ship
s!U
EET
is a
ll ab
out p
artn
ersh
ips!
NASA/CP—2003-212458/VOL1 69
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logyTh
e U
EET
Team
NASA/CP—2003-212458/VOL1 70
UEE
T In
vest
men
t Por
tfolio
(FY0
0-02
)
In-h
ouse
(30%
)
Cor
pora
te P
artn
ers
(24%
)
Uni
vers
ities
(16%
)G
rant
s an
d C
ontr
acts
Oth
er C
ontr
acto
rs (9
%)
Prog
ram
Sup
port
(21%
)
(UEE
T ta
rget
-10
to 1
5% /
yr)
(UEE
T ta
rget
-25
to 3
5% /
yr)
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
NASA/CP—2003-212458/VOL1 71
Prog
ram
Sta
tus
Oct
ober
200
2
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
15%
fuel
bur
n re
duct
ion
for
larg
e su
bson
ic22
% p
roje
cted
for 3
00 P
AX
8% fu
el b
urn
redu
ctio
n fo
r sm
all s
ubso
nic,
sm
all /
larg
e su
pers
onic
15%
for 5
0 PA
X17
% fo
r 300
PAX
HSC
T37
% fo
r 10
PAX
SSB
J
70%
N0x
redu
ctio
n (b
elow
ICAO
96)
for s
ubso
nic
(larg
e re
gion
al) c
ombu
stor
s ov
er th
e LT
O c
ycle
Initi
al in
dust
rial s
ecto
r tes
ts
give
con
fiden
ce th
at a
t lea
stth
e m
in s
ucce
ss w
ill b
e ac
hiev
ed
(TR
L =
3+)
Syst
ems
stud
ies
proj
ectio
nsof
com
bine
d im
pact
s of
U
EET
tech
nolo
gies
.
Lim
ited
test
dat
a (T
RL2
-3+
rang
e)
Goa
lSt
atus
Rem
arks
Initi
al s
ecto
r tes
ts c
ompl
eted
NASA/CP—2003-212458/VOL1 72
051015202530354045 051015202530354045 051015202530354045 051015202530354045
% C
O2
Red
uctio
nv.
Bas
elin
e
Mx
ML
Mn
50 P
AX
300
PAX
HSC
TSB
J
Mx
ML
Mn
Mx
ML
Mn
Mx
ML
Mn
BW
B*
Mx
ML
Mn
* Sam
e en
gine
for a
ll ca
ses
only
Act
ive
Flow
Con
trol b
enef
it va
ried
Pote
ntia
l CO
2R
educ
tion
(Usi
ng “C
ore”
Set
of T
echn
olog
ies)
-rep
rese
nts
FY01
resu
lts
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
NASA/CP—2003-212458/VOL1 73
0%10%
20%
30%
40%
50%
60%
70%
80%
90%
100%
-20
-19
-18
-17
-16
-15
-14
-13
-12
•U
EET
Prog
ram
Goa
l of -
70%
LTO
NO
xca
n be
ach
ieve
d w
ith a
100
%
conf
iden
ce w
ith th
e id
entif
ied
best
set
of t
echn
olog
ies
•U
EET
Prog
ram
Goa
l of -
15%
CO
2ca
n be
ach
ieve
d w
ith a
83%
co
nfid
ence
% B
elow
LTO
NO
xR
ule
for G
T B
est
% C
hang
e in
CO
2/ASM
from
Bas
elin
efo
r GT
Bes
t
Probability
Prob
abili
ty o
f mee
ting
Goa
l = 8
3%
Prob
abili
ty o
f mee
ting
Min
imum
Suc
cess
Crit
eria
= 1
00%
Prel
imin
ary
resu
lts
Prob
abili
ty o
f mee
ting
Goa
l = 1
00%
0%10%
20%
30%
40%
50%
60%
70%
80%
90%
100%
-82
-80
-78
-76
-74
-72
-70
0%10%
20%
30%
40%
50%
60%
70%
80%
90%
100%
-82
-80
-78
-76
-74
-72
-70
Prob
abili
ty D
istr
ibut
ion
for M
eetin
g U
EET
Prog
ram
G
oals
NASA/CP—2003-212458/VOL1 74
Eval
. of A
ctiv
e Fl
ow
Con
trol C
once
pts
BWB
Hig
h R
e N
o.
Valid
atio
n
UEE
T Le
vel I
Mile
ston
e Sc
hedu
le20
0020
0120
0220
0320
04FY
1.0
Pro
puls
ion
Syst
ems
Inte
grat
ion
and
Asse
ssm
ent
2.0
Em
issi
ons
Red
uctio
n
3.0
Hig
hly
Load
ed
Turb
omac
hine
ry
4.0
Mat
eria
ls &
Str
uctu
res
for H
igh
Perf
orm
ance
5.0
Prop
ulsi
on A
irfra
me
Inte
grat
ion
Prop
ulsi
on S
yste
m(s
) C
once
ptua
l Def
initi
on
Prel
imin
ary
Tech
nolo
gy
Bene
fits
Asse
ssm
ent
Flam
etub
e Ev
al’s
. of
70%
LTO
NO
x C
once
pts
Met
hods
D
owns
elec
t
Flow
Con
trol
Con
cept
(s)
Sele
cted
for F
anFlow
Con
trol
Con
cept
(s)
Sele
cted
for T
urbi
ne
Not
es:
1) P
CA
mile
ston
es a
re d
enot
ed b
y2)
WBS
6.0
rese
rved
for P
rogr
am M
gmt.
func
tions
2005
Inte
rim T
echn
olog
y As
sess
men
tsIn
itial
Hig
h Fi
delit
y S
yste
m S
imul
atio
nAn
nula
r Rig
Dem
os
(Lg.
Eng
.) -
70%
LTO
N0x
Con
figs.
Phys
ics
Base
d Pr
edic
tion
Cod
es V
alid
ated
(Com
b.)
Hig
hly
Load
ed M
ultis
tage
Va
lidat
ion
-Com
pres
sor
Phys
ics
Base
d Pr
edic
tion
Cod
es V
alid
ated
(T/M
)
Con
figur
atio
n X
Valid
atio
n
Eval
. of A
ctiv
e Fl
ow
Con
trol A
ppro
ache
s
Hig
hly
Load
ed H
P/LP
Va
lidat
ion
-Tur
bine
Fina
l Tec
hnol
ogy
Asse
ssm
ent
Flow
Con
trol
Con
cept
(s)
Sele
cted
for C
ompr
esso
r
7.0
Inte
llige
nt P
ropu
lsio
n C
ontr
ols
Engi
ne A
rchi
tect
ure/
Payo
ff St
udie
s
Activ
e C
ombu
stio
n C
ontro
l Stu
dies
8.0
Inte
grat
ed C
ompo
nent
Te
chno
logy
D
emon
stra
tions
ICTD
Pla
n fo
r Sm
all
Thru
st C
lass
Eng
ines
2200
ºF C
MC
Lin
er D
emo
Aspi
ratin
g Se
al D
emo
May
200
2 R
ebas
elin
e
Cer
amic
The
rmal
Bar
rier
Coa
ting
(TBC
) C
once
pt(s
) Se
lect
ion
Mat
’l S
ys. f
or C
MC
Tu
rbin
e Va
ne
Hig
h Te
mp.
Mat
’ls.
Cap
abilit
ies
Dem
os.
EPM
Allo
y U
pper
Te
mp.
Lim
it
Low
Con
duct
ive
Cer
amic
TBC
S
yste
m S
elec
ted
Con
cept
s Se
lect
ed fo
r 300
0ºF
CM
C M
at’l
Sys
tem
Feas
ibilit
y of
300
0ºF
CM
C M
at’l
Sys
tem
Es
tab’
d.
Com
p. T
ools
Ava
il. fo
r D
esig
n of
Sin
gle
Cry
stal
N
icke
l-bas
e Al
loys
70%
LTO
N0x
Red
. D
emo’
d -S
ecto
r Rig
Init.
Low
N0x
Sec
tor
Rig
Dem
o.
Dow
nsel
ect R
egio
nal
Eng.
Con
tract
or
Dow
nsel
ect L
arge
En
g. C
ontra
ctor
Sim
ulat
e Be
nchm
ark
Com
b.
Expe
rimen
t w/ L
iqui
d Sp
ray
Inje
ctor
Con
trols
Arc
hite
ctur
e/Pa
yoff
Stud
ies
Inte
grat
ed C
ompo
nent
Tec
hnol
ogy
Dem
onst
ratio
ns P
lan
--> f/
Lg. T
hrus
t Cla
ss E
ng.
ICTC
Pla
n fo
r Acc
ess
to S
pace
En
gine
s
2006
Flow
Con
trol
Proo
f-of-C
once
pts:
-Fan
-Com
pres
sor
CM
C V
ane
Dem
o.
Dem
o H
i Tem
p (6
00C
) W
irele
ss D
ata
Com
mun
icat
ion
Dem
o. P
roto
type
R
otat
ing
Mac
hine
ry
Cle
aran
ce M
gmt.
Feas
ibilit
y of
UH
TC a
s >
3000
ºF -
Stru
ctur
al o
r Fun
ctio
nal C
oatin
g M
at’l.
NASA/CP—2003-212458/VOL1 75
Educ
atio
n/O
utre
ach
Act
iviti
es
Wrig
ht B
roth
ers
Gam
e fo
r the
Web
Targ
eted
to g
rade
s 5-
8, th
is e
duca
tiona
l gam
e en
cour
ages
st
uden
ts to
bro
wse
the
mus
eum
and
lear
n fa
cts
abou
t the
Wrig
ht
Brot
hers
and
thei
r jou
rney
to d
isco
ver t
he s
ecre
t of p
ower
ed fl
ight
, th
en a
nsw
er q
uest
ions
for p
oint
s on
Kill
Dev
il H
ills n
ear K
itty
Haw
k.
The
gam
e ha
s be
en p
oste
d to
the
UEE
T W
ebsi
te:
http
://w
ww
.uee
t.nas
a.go
v/St
uden
tSite
UEE
T O
utre
ach
Dis
play
This
8ft
x 10
ft di
spla
y w
as c
reat
ed to
re
pres
ent U
EET
to th
e te
chni
cal c
omm
unity
an
d th
e ge
nera
l pub
lic.
It w
as d
ebut
ed a
t th
e In
tegr
ated
Hig
h Pe
rform
ance
Tur
bine
En
gine
Tec
hnol
ogy
(IHPT
ET) S
ympo
sium
in
Day
ton,
Ohi
o on
Sep
tem
ber 9
, 200
2.
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
NASA/CP—2003-212458/VOL1 76
Inte
llect
ual P
rope
rty
Man
agem
ent H
andb
ook
Inte
llect
ual P
rope
rty
Man
agem
ent H
andb
ook
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
•H
andb
ook
sign
ed J
uly
2002
afte
r ex
tens
ive
inte
ract
ions
with
indu
stry
•Tr
aini
ng m
odul
e ha
s be
en d
evel
oped
in
co-
oper
atio
n w
ith N
atio
nal
Tech
nolo
gy T
rans
fer C
ente
r (N
TTC
) fo
r NA
SA e
mpl
oyee
s (in
clud
ing
on
site
PB
C’s
)
•Tr
aini
ng m
odul
e (a
nd tr
aine
rs) h
ave
been
offe
red
to c
orpo
rate
par
tner
s
NASA/CP—2003-212458/VOL1 77
Robe
rt C
. Byr
d N
atio
nal T
echn
olog
y Tr
ansf
er C
ente
r
We
are
com
mitt
ed to
wor
king
toge
ther
in p
artn
ersh
ip to
act
ivel
y se
ek o
ut n
on a
eros
pace
oppo
rtun
ities
for
tran
sfer
and
com
mer
cial
izat
ion
of a
ll ap
prop
riat
e te
chno
logi
es b
eing
dev
elop
edth
roug
h pr
ogra
ms a
nd p
roje
cts b
eing
man
aged
by
the
Ultr
a E
ffic
ient
Eng
ine
Tec
hnol
ogy
(UE
ET
) Off
ice.
____
____
____
_R
ober
t J. S
haw
Chi
ef, U
EE
T O
ffic
eN
ASA
Gle
nn R
esea
rch
Cen
ter
____
____
____
_Jo
seph
Alle
nPr
esid
ent,
Nat
iona
l Tec
hnol
ogy
Tra
nsfe
r C
ente
rW
heel
ing
Jesu
it U
nive
rsity
____
____
____
_L
arry
Vite
rna
Chi
ef, C
omm
erci
al T
echn
olog
y O
ffic
e N
ASA
Gle
nn R
esea
rch
Cen
ter
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Tech
nolo
gy T
rans
fer P
artn
ersh
ip
NASA/CP—2003-212458/VOL1 78
Fina
l Maj
or T
echn
olog
y D
eliv
erab
les
(1)
Fina
l Maj
or T
echn
olog
y D
eliv
erab
les
(1)
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Prop
ulsi
on S
yste
ms
Asse
ssm
ent a
nd In
tegr
atio
n:Sy
stem
s st
udie
s as
sess
men
t of i
mpa
ct o
f UEE
T te
chno
logi
es to
war
ds
mee
ting
NO
X an
d C
O2
goal
s.
Emis
sion
s:An
nula
r rig
val
idat
ion
test
(TR
L5) o
f com
bust
or c
onfig
urat
ions
that
will
mee
t or
exce
ed 7
0 %
Lan
ding
Tak
e-O
ff N
Ox
goal
.Va
lidat
ed p
hysi
cs b
ased
sim
ulat
ion
tool
s. (
TRL4
)
Hig
hly
Load
ed T
urbo
mac
hine
ryW
ind
tunn
el v
alid
atio
n of
wak
e flo
w c
ontr
ol c
once
pt fo
r effi
cien
t, lo
w n
oise
fa
n. (
TRL4
) D
one
in p
artn
ersh
ip w
ith Q
AT.
Test
rig
valid
atio
n of
com
pres
sor f
low
con
trol
/man
agem
ent c
once
pt. (
TRL4
)Te
st ri
g va
lidat
ion
of tu
rbin
e flo
w c
ontr
ol/m
anag
emen
t tec
hniq
ues.
(TR
L4)
Valid
ated
phy
sics
bas
ed s
imul
atio
n to
ols.
(TR
L4)
Mat
eria
l and
Str
uctu
res
Rig
test
val
idat
ion
of h
igh
tem
pera
ture
turb
ine
airf
oil m
ater
ials
sys
tem
s. (
TRL3
)R
ig te
st v
alid
atio
n of
270
0 de
g F
Cer
amic
Mat
rix C
ompo
site
mat
eria
l sys
tem
. (T
RL3
)D
evel
op a
nd v
alid
ate
com
puta
tiona
l mat
eria
ls to
ols.
(TR
L2)
NASA/CP—2003-212458/VOL1 79
Fina
l Maj
or T
echn
olog
y D
eliv
erab
les
(2)
Fina
l Maj
or T
echn
olog
y D
eliv
erab
les
(2)
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Prop
ulsi
on-A
irfra
me
Inte
grat
ion
Win
d tu
nnel
val
idat
ion
of a
dvan
ced
flow
and
sha
pe c
ontr
ol te
chno
logi
es fo
r pr
opul
sion
sys
tem
app
licat
ion.
(TR
L3)
Valid
ated
adv
ance
d C
FD b
ased
des
ign
met
hods
. (T
RL4
)
Inte
llige
nt P
ropu
lsio
n C
ontr
ols:
Valid
ated
app
roac
hes
for p
ropu
lsio
n sy
stem
act
ive
clea
ranc
e m
anag
emen
t. (T
RL3
-6?)
Det
erm
ine
thro
ugh
labo
rato
ry te
sts
attr
activ
e ap
proa
ches
for h
igh
tem
pera
ture
wire
less
dat
a co
mm
unic
atio
ns fo
r pro
puls
ion
syst
em a
pplic
atio
ns. (
TRL3
)
Inte
grat
ed C
ompo
nent
Tec
hnol
ogy
Dem
onst
ratio
nsD
emon
stra
te th
roug
h en
gine
test
s (T
RL6
) in
part
ners
hip
with
indu
stry
te
chno
logy
read
ines
s fo
r 220
0°F
Cer
amic
Mat
rix C
ompo
site
Com
bust
or li
ner
and
aspi
ratin
g se
al.
NASA/CP—2003-212458/VOL1 80
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
Ultr
a Ef
ficie
nt E
ngin
e Te
chno
logy
•Th
e U
EET
Prog
ram
is c
ompr
ised
of a
por
tfolio
of t
echn
olog
ies
whi
ch a
re m
atur
ed to
a T
RL
of 3
-6 a
nd tr
ansi
tione
d to
indu
stry
for
thei
r use
in fu
ture
aer
ospa
ce v
ehic
les
desi
gns.
•Th
e pr
ogra
m g
oals
/obj
ectiv
es a
re s
atis
fied
thro
ugh
syst
ems
stud
ies
asse
ssm
ents
of t
he c
ombi
ned
impa
ct o
f the
tech
nolo
gies
on
four
veh
icle
cla
sses
.-
Larg
e su
bson
ic tr
ansp
orts
-R
egio
nal s
ubso
nic
tran
spor
ts-
Larg
e co
mm
erci
al s
uper
soni
c tr
ansp
ort
-Su
pers
onic
bus
ines
s je
t
•Th
e ul
timat
e m
easu
re o
f suc
cess
of t
he U
EET
Prog
ram
will
be
the
impa
ct o
f the
tech
nolo
gies
.
Con
clud
ing
Rem
arks
NASA/CP—2003-212458/VOL1 81
