NASA Ultra Efficient Engine Technology Project Overview · PDF fileNASA ULTRA EFFICIENT ENGINE...
Transcript of NASA Ultra Efficient Engine Technology Project Overview · PDF fileNASA ULTRA EFFICIENT ENGINE...
NASA ULTRA EFFICIENT ENGINE TECHNOLOGY PROJECT OVERVIEW
Catherine L. Peddie and Robert J. Shaw National Aeronautics and Space Administration
Glenn Research Center Cleveland, Ohio
Ultra Efficient Engine TechnologyUltra Efficient Engine Technology
NASA Ultra Efficient Engine NASA Ultra Efficient Engine Technology Project OverviewTechnology Project Overview
Joe ShawJoe ShawUEET Project ManagerUEET Project Manager
Catherine PeddieCatherine PeddieUEET Assistant Project ManagerUEET Assistant Project Manager
Enabling Technologies for 21st Century Turbine EnginesEnabling Technologies for 21st Century Turbine Engines
NASA/CP—2004-212963/VOL1 43
https://ntrs.nasa.gov/search.jsp?R=20040182400 2018-05-01T08:45:22+00:00Z
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ou
tlin
eO
utl
ine
•O
verv
iew
of
curr
ent
UE
ET
Pro
ject
• R
e in
vent
ion
of U
EE
T a
s pa
rt o
f th
e V
ehic
le S
yste
ms
Pro
gram
NASA/CP—2004-212963/VOL1 44
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Cu
rren
t U
EE
T P
roje
ctC
urr
ent
UE
ET
Pro
ject
NASA/CP—2004-212963/VOL1 45
NASA/CP—2004-212963/VOL1 46
Th
e U
EE
T P
rog
ram
will
dev
elo
p a
nd
tra
nsf
er t
o t
he
U. S
. in
du
stry
crit
ical
gas
tu
rbin
e en
gin
e te
chn
olo
gie
s w
hic
h w
ill c
on
trib
ute
to
“en
ablin
g a
saf
e, s
ecu
re, a
nd
en
viro
nm
enta
lly f
rien
dly
air
tran
spo
rtat
ion
sys
tem
”.
NASA/CP—2004-212963/VOL1 47
Env
iron
men
tally
Fri
endl
y A
ircr
aft
Sm
og
-fre
e No
imp
act
on
g
lob
al c
limat
e
No
ise
wit
hin
air
po
rt b
ou
nd
arie
sC
onst
rain
obj
ectio
nabl
e no
ise
to
with
in a
irpor
t bou
ndar
ies
Min
imiz
e th
e co
ntrib
utio
n of
air
vehi
cles
to
the
prod
uctio
n of
sm
og
Min
imiz
e th
e im
pact
of a
ir ve
hicl
es o
n gl
obal
clim
ate
NASA/CP—2004-212963/VOL1 48
Red
uce
emis
sion
s of
fut
ure
airc
raft
by
a fa
ctor
of
thre
e w
ithi
n 10
yea
rs (
2007
),(2
007)
,an
d by
a f
acto
r of
fiv
e w
ithi
n 20
yea
rs.
NA
SA T
hree
Pill
ars
for
Succ
ess-
1997
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Rev
olut
ioni
ze A
viat
ion
Goa
l
Em
issi
ons
Obj
ecti
ve
Red
uce
NO
x em
issi
ons
of f
utur
e ai
rcra
ft b
y 70
per
cent
wit
hin
10 y
ears
, and
by 8
0 pe
rcen
t w
ithi
n 25
yea
rs (
usin
g th
e 19
96 I
CA
O S
tand
ard
for
NO
xas
the
base
line.
Red
uce
CO
2em
issi
ons
of f
utur
e ai
rcra
ft b
y 25
per
cent
and
by
50 p
erce
ntIn
the
sam
e ti
mef
ram
es (
usin
g 19
97 s
ubso
nic
airc
raft
tec
hnol
ogy
as t
he b
asel
ine)
.
NA
SA A
eros
pace
Tec
hnol
ogy
Ent
erpr
ise
Stra
tegi
c P
lan-
2000
UE
ET
will
be
the
resp
onsi
ble
prop
ulsi
on p
rogr
am f
or d
eliv
erin
g o
UE
ET
will
be
the
resp
onsi
ble
prop
ulsi
on p
rogr
am f
or d
eliv
erin
g o n
this
obj
ectiv
e!
n th
is o
bjec
tive!
NASA/CP—2004-212963/VOL1 49
* L
TO
*
LT
O --
Lan
din
g/T
ake-
off
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Vis
ion:
Vis
ion:
Dev
elop
and
han
d of
f re
volu
tiona
ry tu
rbin
e D
evel
op a
nd h
and
off
revo
lutio
nary
turb
ine
engi
ne p
ropu
lsio
n te
chno
logi
es th
at w
ill e
nabl
e fu
ture
en
gine
pro
puls
ion
tech
nolo
gies
that
will
ena
ble
futu
re
gene
ratio
n ve
hicl
es o
ver
a w
ide
rang
e of
flig
ht s
peed
s.ge
nera
tion
vehi
cles
ove
r a
wid
e ra
nge
of f
light
spe
eds.
Goa
ls:
Goa
ls:
Pro
puls
ion
tech
nolo
gies
to e
nabl
e in
crea
ses
in s
yste
m
Pro
puls
ion
tech
nolo
gies
to e
nabl
e in
crea
ses
in s
yste
m
effi
cien
cy a
nd, t
here
fore
, fue
l bur
n re
duct
ions
of
up to
15
effi
cien
cy a
nd, t
here
fore
, fue
l bur
n re
duct
ions
of
up to
15
% (
equi
vale
nt r
educ
tions
in C
O%
(eq
uiva
lent
red
uctio
ns in
CO
22))
Com
bust
or te
chno
logi
es (
conf
igur
atio
n an
d m
ater
ials
) C
ombu
stor
tech
nolo
gies
(co
nfig
urat
ion
and
mat
eria
ls)
whi
ch w
ill e
nabl
e re
duct
ions
in L
TO
* N
Ow
hich
will
ena
ble
redu
ctio
ns in
LT
O*
NO
xxof
70%
of
70%
re
lativ
e to
199
6 IC
AO
sta
ndar
ds.
rela
tive
to 1
996
ICA
O s
tand
ards
.
NASA/CP—2004-212963/VOL1 50
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
will
ena
ble
futu
re g
ener
atio
n ve
hicl
es o
ver
a w
ide
rang
e of
flig
will
ena
ble
futu
re g
ener
atio
n ve
hicl
es o
ver
a w
ide
rang
e of
flig
ht s
peed
s.ht
spe
eds.
Vis
ion
Vis
ion
We
sup
po
rt t
he
visi
on
an
d a
re c
om
mit
ted
to
th
e su
cces
s o
f N
AS
A’s
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
(UE
ET
) P
roje
ct.
Will
iam
s In
tern
atio
nal
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Rob
ert D
. Sou
thw
ick,
Pra
tt &
Whi
tney
Fred
Kra
use,
Gen
eral
Ele
ctri
c A
ircr
aft E
ngin
es
Dim
itri M
avri
s, G
eorg
ia T
ech
Mah
moo
d N
aim
i, B
oein
g C
omm
erci
al A
irpl
ane
Com
pany
Tom
Har
tman
n, L
ockh
eed-
Mar
tin
Scot
t Cru
zen,
Wil
liam
s In
tern
atio
nal
Ger
ald
Bri
nes,
Alli
son-
Rol
ls R
oyce
Rob
ert J
. Sha
w, N
ASA
Gle
nn R
esea
rch
Cen
ter
Will
iam
Koo
p, A
ir F
orce
Res
earc
h L
abor
ator
yV
inod
Nan
gia,
Hon
eyw
ell
Tim
Con
ners
, Gul
fstr
eam
Las
t U
pdat
e-A
pril
2003
NASA/CP—2004-212963/VOL1 51
Unm
anne
d A
eria
l V
ehic
le (
UA
V)
Non-Commercial Vehicles
Acc
ess-
to-
Spa
ce/H
igh
Mac
h P
latf
orm
Gen
eral
A
viat
ion
Air
craf
t (G
A)
4 P
AX
Commercial Vehicles
Su
bso
nic
Su
per
son
icH
yper
son
ic
Reg
iona
l Jet
T
rans
port
Lar
ge S
ubso
nic
Tra
nspo
rt
300
PA
X
50 P
AX
Hig
h Sp
eed
Civ
il T
rans
port
(H
SCT
)
300
PA
X
Supe
rson
ic
Bus
ines
s Je
t (SB
J)
10 P
AX
Ble
nded
Win
g B
ody
(BW
B)
500-
600
PA
X Mil
itar
y T
rans
port
(C
-17)
Adv
ance
d Fi
ghte
r
Bas
elin
e V
ehic
les
for
UE
ET
Tec
hnol
ogy
App
licat
ion
Stud
ies
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Thes
e ve
hicles
drive
the
tech
nology
inve
stmen
t st
rate
gy
Thes
e ve
hicles
dete
rmine
the
tech
nology
syne
rgies
NASA/CP—2004-212963/VOL1 52
Pro
gra
m T
ech
nic
al O
bje
ctiv
esP
rog
ram
Tec
hn
ical
Ob
ject
ives
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
15%
fu
el b
urn
red
uct
ion
fo
r la
rge
sub
son
ic a
ircr
aft
8% f
uel
bu
rn r
edu
ctio
n f
or
smal
l su
bso
nic
, sm
all /
larg
e su
per
son
ic
70%
N0x
red
uct
ion
(b
elow
ICA
O 9
6) f
or
sub
son
ic
(lar
ge/
reg
ion
al)
com
bu
sto
rs
ove
r th
e L
TO
cyc
le
Go
alM
inim
um
Su
cces
s C
rite
ria
12%
fu
el b
urn
red
uct
ion
fo
r la
rge
sub
son
ic a
ircr
aft
4% f
uel
bu
rn r
edu
ctio
n f
or
smal
l su
bso
nic
, sm
all /
larg
e su
per
son
ic
65%
N0x
red
uct
ion
(lar
ge/
reg
ion
al)
com
bu
sto
rs
ove
r th
e L
TO
cyc
le
(bel
ow IC
AO
96)
fo
r su
bso
nic
CO
2G
oal
NO
xG
oal
NASA/CP—2004-212963/VOL1 53
NA
SA
’s T
ech
no
log
y R
ead
ines
s L
evel
(T
RL
) S
cale
NA
SA
’s T
ech
no
log
y R
ead
ines
s L
evel
(T
RL
) S
cale
TR
LG
ener
al N
AS
A D
efin
itio
n
9A
ctua
l sys
tem
“fli
ght p
rove
n” o
n op
erat
iona
l fli
ght
8A
ctua
l sys
tem
com
plet
ed a
nd “
fligh
t qu
alifi
ed”
thro
ugh
test
and
dem
onst
ratio
n
7S
yste
m p
roto
type
dem
onst
rate
d in
flig
ht
envi
ronm
ent
6S
yste
m/s
ubsy
stem
mod
el o
r pr
otot
ype
dem
onst
rate
d/va
lidat
ed in
a r
elev
ant
envi
ronm
ent
5C
ompo
nent
and
/or
brea
dboa
rd v
erifi
catio
n in
a r
elev
ant e
nviro
nmen
t
4C
ompo
nent
and
/or
brea
dboa
rd te
st in
a
labo
rato
ry e
nviro
nmen
t
3A
naly
tical
and
exp
erim
enta
l crit
ical
func
tion,
or
cha
ract
eris
tic p
roof
-of-
conc
ept
2T
echn
olog
y co
ncep
t and
/or
appl
icat
ion
form
ulat
ed (
cand
idat
e se
lect
ed)
1B
asic
prin
cipl
es o
bser
ved
and
repo
rted
Sys
tem
Tes
t and
Ope
ratio
ns
Sys
tem
/Sub
syst
em D
evel
opm
ent
Tec
hnol
ogy
Dem
onst
ratio
n
Tec
hnol
ogy
Dev
elop
men
t
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
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
UE
ET
In p
artn
ersh
ip w
ith D
OD
,
indu
stry
NASA/CP—2004-212963/VOL1 54
GR
C L
ead
Inte
grat
ed C
ompo
nent
T
echn
olog
y D
emon
stra
tion
s
Em
issi
ons
Red
ucti
on
GR
C L
ead
Mat
eria
ls a
nd S
truc
ture
s fo
r H
igh
Per
form
ance
GR
C L
ead
Pro
puls
ion-
Air
fram
e In
tegr
atio
n
LaR
C L
ead
Hig
hly
Loa
ded
Tur
bom
achi
nery
GR
C L
ead
UE
ET
Ele
men
tsU
EE
T E
lem
ents
Inte
llige
nt P
ropu
lsio
nC
ontr
ols
GR
C L
ead
GR
C L
ead
Pro
puls
ion
Syst
ems
Inte
grat
ion
and
Ass
essm
ent
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
NASA/CP—2004-212963/VOL1 55
Sel
ecte
d T
ech
nic
al H
igh
ligh
tsS
elec
ted
Tec
hn
ical
Hig
hlig
hts
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
70%
LT
O N
Ox
com
bust
or s
ecto
r te
sts
2 st
age
PO
C c
ompr
esso
r ri
g de
sign
Tur
bom
achi
nery
dis
k m
ater
ial
tem
pera
ture
lim
it
Act
ive
flow
con
trol
to r
educ
e in
let
dist
orti
onC
MC
com
bust
or li
ner
for
engi
ne t
est
Rig
/eng
ine
test
s to
mea
sure
pa
rtic
ulat
es, a
eros
ol e
mis
sion
s
NASA/CP—2004-212963/VOL1 56
2015
“U
ltim
ate”
Tu
rbin
eE
ng
ine
Sys
tem
s•
Em
issi
on
s•
Fu
el b
urn
•W
eig
ht
•N
ois
e•
Saf
ety
•R
elia
bili
ty
Per
iod
ic
asse
ssm
ents
/re
bal
anci
ng
of
po
rtfo
lio
Inte
gra
ted
co
mp
on
ent
tech
no
log
y v
alid
atio
ns
(in
co
st-s
har
ing
par
tner
ship
wit
h o
ther
g
ove
rnm
ent
agen
cies
an
d/o
r in
du
stry
)
Th
e U
EE
T “
Ro
adm
ap”
Th
e U
EE
T “
Ro
adm
ap”
UE
ET
Tech
nolo
gies
•C
ompo
nent
s
•M
ater
ials
and
str
uctu
res
•In
telli
gent
pro
puls
ion
cont
rols
•P
ropu
lsio
n-ai
rfra
me
inte
grat
ion
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
NASA/CP—2004-212963/VOL1 57
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Th
e P
ath
to
Th
e P
ath
to
Re
Inve
nti
on
R
e In
ven
tio
n
of
the
UE
ET
Pro
ject
of
the
UE
ET
Pro
ject
NASA/CP—2004-212963/VOL1 58
NASA/CP—2004-212963/VOL1 59
Aer
onau
tics
Tec
hnol
ogy
–T
hree
Int
egra
ted
Prog
ram
s
Veh
icle
Sys
tem
s
Air
spac
e S
yste
ms
Avi
atio
n S
afet
y &
Sec
uri
ty
Saf
ety/
Sec
uri
ty
Air
spac
eC
apab
ility
Co
st
Veh
icle
Cap
abili
ty
En
viro
nm
ent
NASA/CP—2004-212963/VOL1 60
Exp
lore
New
Aer
osp
ace
Mis
sio
ns
Pio
neer
nov
el a
eros
pace
con
cept
s to
sup
port
ear
th a
nd s
pace
sci
ence
mis
sion
s
Pro
tect
th
e E
nvi
ron
men
t P
rote
ct lo
cal e
nviro
nmen
tal q
ualit
y an
d th
e gl
obal
clim
ate
by
redu
cing
airc
raft
nois
e an
d em
issi
ons.
Incr
ease
Mo
bili
ty
Ena
ble
mor
e pe
ople
and
goo
ds to
trav
el fa
ster
and
fart
her,
any
whe
re, a
nytim
e w
ith fe
wer
del
ays
Su
pp
ort
Nat
ion
al S
ecu
rity
Leve
rage
NA
SA
aer
onau
tics
tech
nolo
gy in
vest
men
ts in
par
tner
ship
with
D
OD
to s
uppo
rt th
eir
role
of p
rote
ctin
g th
e N
atio
n
Aer
onau
tics
The
me
Obj
ectiv
es f
or th
e Pu
blic
Goo
dO
bjO
utco
me
Vis
ion
Goa
ls
Veh
icle
Con
cept
s
Tec
hnol
ogy
Por
tfolio
Inve
stm
ent S
trat
egy
NASA/CP—2004-212963/VOL1 61
Env
iron
men
tally
F
rien
dly
Air
craf
t Sm
og
-fre
e No
imp
act
on
g
lob
al c
limat
e
No
ise
wit
hin
air
po
rt b
ou
nd
arie
sC
onst
rain
obj
ectio
nabl
e no
ise
to
with
in a
irpor
t bou
ndar
ies
Min
imiz
e th
e co
ntrib
utio
n of
air
vehi
cles
to
the
prod
uctio
n of
sm
og
Min
imiz
e th
e im
pact
of a
ir ve
hicl
es o
n gl
obal
clim
ate
Obj
Out
com
e
Vis
ion
Goa
ls
Veh
icle
Con
cept
s
Tec
hnol
ogy
Por
tfolio
Inve
stm
ent S
trat
egy
NASA/CP—2004-212963/VOL1 62
Air
craf
t fo
r P
ublic
Mob
ility
Mo
re C
on
ven
ien
tM
ore
Aff
ord
able
Exp
and
acce
ss to
avi
atio
n to
mor
e lo
catio
ns a
nd m
ake
it av
aila
ble
on-
dem
and
Mak
e ai
r tr
avel
ava
ilabl
e to
the
entir
e po
pula
tion
Fas
ter
Incr
ease
the
spee
d of
air
trav
el…
with
out c
ompr
omis
ing
safe
ty
Obj
Out
com
e
Vis
ion
Goa
ls
Veh
icle
Con
cept
s
Tec
hnol
ogy
Por
tfolio
Inve
stm
ent S
trat
egy
NASA/CP—2004-212963/VOL1 63
Inno
vati
ve V
ehic
le C
once
pts
to I
dent
ify
Key
T
echn
olog
y R
equi
rem
ents
Cle
an T
rans
port
Min
imum
en
viro
nmen
tal
impa
ct, m
axim
um
effic
ienc
y
Pla
neta
ry F
light
Veh
icle
s
Con
duct
ext
ende
d sc
ienc
e an
d ex
plor
atio
n m
issi
ons
Glo
bal S
trik
e
Str
engt
hen
natio
nal
secu
rity
thro
ugh
rapi
d de
ploy
men
t an
d gl
obal
rea
ch
San
ta M
onic
a at
Mid
nigh
t
All
hour
acc
ess
to a
ny lo
catio
n w
ithou
t noi
se
dist
urba
nce
Per
sona
l Air
Veh
icle
Rur
al, r
egio
nal,
and
intr
a-ur
ban
tran
spor
tatio
n
Glo
bal R
each
Tra
nspo
rt
Glo
bal r
each
and
on
-dem
and
deliv
ery
Hea
rtla
nd E
xpre
ss
Rur
al a
nd r
egio
nal
econ
omic
gro
wth
, tim
e cr
itica
l tr
ansp
ort
V/S
TO
L C
omm
uter
Ena
bles
city
ce
nter
acc
ess
in
all w
eath
er
Tan
ker
Aut
omat
ed r
efue
ling
capa
bilit
y, u
ltra-
long
en
dura
nce,
wid
e
spee
d ra
nge
Ext
rem
e S
TO
L T
rans
port
Exp
ands
the
use
of e
xist
ing
airp
ort
infr
astr
uctu
re
Sup
erso
nic
Ove
rland
Red
uce
pass
enge
r fli
ght
time
by a
t lea
st a
fa
ctor
of 2
Hig
h A
ltitu
de L
ong
End
uran
ce
Hig
h al
titud
e ob
serv
atio
ns fo
r sc
ienc
e an
d de
fens
e
NASA/CP—2004-212963/VOL1 64
Proj
ect E
volu
tion
with
in R
epla
nned
Veh
icle
Sy
stem
s St
rate
gic
Focu
s A
reas
0405
0607
0809
1011
1213
1415
1617
1819
2021
2223
2425
Qu
iet
Air
craf
t fo
r C
om
mu
nit
y F
rien
dly
Ser
vice
QA
T4x
Noi
se R
educ
tion
4X D
emo
(F&
SD
)D
esig
n fo
r Q
uiet
Inte
grat
ed Q
uiet
, Effi
cien
t A
ircra
ft D
esig
nE
nvi
ron
men
tally
Fri
end
ly, C
lean
Bu
rnin
g E
ng
ines
UE
ET
UE
ET
Dem
o (F
&S
D)
Inte
llige
nt P
ropu
lsio
n S
yste
ms
Inte
grat
ed F
light
/Pro
puls
ion
Inte
llige
nce
Dem
o (F
&S
D)
Aut
onom
ous
Pro
puls
ion
Sys
tem
sS
mar
t A
ircr
aft
and
Au
ton
om
ou
s C
on
tro
lIF
CS
-Gen
II ( F
&S
D)
IFC
S -
Ada
p tiv
e O
p tim
al F
CS
Dem
o ( F
&S
D)
UA
V in
the
NA
S S
tep
1 an
d 2
(FS
D)
Mul
ti-U
AV
Com
man
d, C
ontr
ol, C
omm
unic
atio
ns (
F&
SD
)A
uton
omou
s R
obus
t Avi
onic
sA
uRA
Flig
ht D
emo
(F&
SD
)S
entie
nt A
ir V
ehic
leA
uton
omou
s C
ertif
icat
ion
Met
hods
Aut
onom
ous
Tra
nsp o
rt T
echn
olog
y
NASA/CP—2004-212963/VOL1 65
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Fac
tors
Dri
vin
g C
han
ge
Fac
tors
Dri
vin
g C
han
ge
•A
dmin
istr
atio
n/O
MB
dri
vers
tha
t ar
e no
t go
ing
away
-Be
mor
e co
mpe
titi
ve (
outh
ouse
and
in h
ouse
) to
get
“be
st p
rodu
ct”
-Rig
ht s
ize
the
NA
SA in
stit
utio
n (p
eopl
e an
d fa
cilit
ies)
-Pro
per
role
of
gove
rnm
ent
prog
ram
s in
aer
ospa
ce R
&D
foo
d ch
ain
• In
crea
sing
str
ess
on F
eder
al b
udge
t-G
row
ing
Fed
eral
def
icit
s fo
r fo
rese
eabl
e fu
ture
-Adm
inis
trat
ion
prio
riti
es (
Hom
elan
d se
curi
ty a
nd a
nti t
erro
rism
)-A
eros
pace
pri
orit
ies
(Nat
iona
l and
Age
ncy)
NASA/CP—2004-212963/VOL1 66
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gyO
pp
ort
un
itie
sO
pp
ort
un
itie
s
Opp
ortu
nity
to:
-sig
nifi
cant
ly s
tren
gthe
n U
EE
T in
the
eye
s of
our
cus
tom
ers/
part
ners
/sta
keho
lder
s
--in
crea
se t
he s
uppo
rt o
f ke
y de
cisi
on m
aker
s fo
r U
EE
T
-mak
e m
ajor
tec
hnol
ogy
impa
cts
on n
ext
gene
rati
on g
as t
urbi
ne e
ngin
e pr
opul
sion
sys
tem
s
-ca
rry
our
rela
tion
ship
wit
h D
oD (
IHP
TE
T/V
AA
TE
) to
the
nex
t le
vel
-for
ge a
par
tner
ship
wit
h N
AI,
NG
LT
-be
a le
ader
in d
evel
opin
g an
new
NA
SA/o
t her
gov
ernm
ent
agen
cies
/indu
stry
/uni
vers
ity
part
ners
hip
mod
el f
or a
eros
pace
R&
T
NASA/CP—2004-212963/VOL1 67
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ho
w d
o w
e d
o it
?H
ow
do
we
do
it?
NASA/CP—2004-212963/VOL1 68
Veh
icle
Sys
tem
s(H
Q)
Qui
et
Airc
raft
Tec
hnol
ogy
-Q
AT
(L
aRC
/GR
C)
Inte
grat
ed
Tai
lore
d A
eros
truc
ture
s -
ITA
S (
L aR
C)
Low
E
mis
sion
s A
ltern
ativ
e P
ower
-LE
AP
(GR
C)
Flig
ht a
nd S
yste
m
Dem
onst
ratio
ns(D
FR
C)
Ultr
a E
ffici
ent
Eng
ine
Tec
hnol
ogy
-U
EE
T
(GR
C)
Aut
onom
ous
Rob
ust
Avi
onic
s -
AuR
A(L
aRC
/DF
RC
)
Effi
cien
t A
erod
ynam
icS
hape
s an
d In
tegr
atio
n -
EA
SI
(LaR
C)
Str
ateg
y T
eam
(One
rep
rese
ntat
ive
per
cent
er)
Ext
ern
al G
rou
ps
Red
Tea
mA
TA
C/V
SW
GN
RC
/AS
EB
Veh
icle
Sys
tem
s P
rogr
am S
truc
ture
UE
ET
new
wil
l:•B
e a
TR
L 1
-6 p
roje
ct.
•The
onl
ypr
ojec
t in
the
Veh
icle
Sys
tem
s Pr
ogra
m fo
cuse
d en
tire
ly o
n tu
rbin
e en
gine
pro
puls
ion
syst
ems.
• In
vest
app
roxi
mat
ely
20%
of
reso
urce
s in
to d
evel
opin
g a
tech
nol o
gy f
ound
atio
n fo
r th
e fo
llow
on
proj
ect.
Veh
icle
Inte
grat
ion,
S
trat
egy,
and
Tec
hnic
al
Ana
lysi
s (V
IST
A)
NASA/CP—2004-212963/VOL1 69
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Pro
puls
ion
& P
ower
P
rogr
am/P
roje
ct(T
urbi
ne e
ngin
e po
rtio
n)
UE
ET
Pro
gram
/Pro
ject
(FY
04 p
lans
)
UE
ET
new
(FY
04-0
7)
The
FY
04 C
halle
nge
The
FY
04 C
halle
nge
NASA/CP—2004-212963/VOL1 70
* L
TO
*
LT
O --
Lan
din
g/T
ake-
off
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Vis
ion:
Dev
elop
and
han
d of
f re
volu
tiona
ry tu
rbin
e en
gine
prop
ulsi
on te
chno
logi
es th
at w
ill e
nabl
e fu
ture
gen
erat
ion
vehi
cles
ove
r a
wid
e ra
nge
of f
light
spe
eds.
Goa
ls:
Pro
puls
ion
tech
nolo
gies
to e
nabl
e in
crea
ses
in s
yste
m e
ffic
ienc
yan
d,
ther
efor
e, f
uel b
urn
redu
ctio
ns o
f up
to 1
5 %
(eq
uiva
lent
red
uctio
ns
in C
O2
)
Com
bust
or te
chno
logi
es (
conf
igur
atio
n an
d m
ater
ials
) w
hich
will
en
able
red
uctio
ns in
LT
O*
NO
xof
70%
rel
ativ
e to
199
6 IC
AO
st
anda
rds.
The
se w
ill r
emai
n th
e sa
me!
The
se w
ill r
emai
n th
e sa
me!
NASA/CP—2004-212963/VOL1 71
UE
ET
new
“C
hara
cter
isti
cs”
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
• U
EE
Tne
w w
ill f
ocus
on
tech
nolo
gies
for
subs
onic
and
sup
erso
nic
com
mer
cial
sys
tem
s.T
he s
ubso
nic
syst
ems
will
be
regi
onal
jet
s th
ough
larg
e w
ide
bodi
esT
he s
uper
soni
c sy
stem
s w
ill b
e SS
BJ
thro
ugh
com
mer
cial
tra
nspo
rts
(10
-100
PA
X)
• U
EE
Tne
w w
ill d
o se
lect
ed r
otor
craf
t tec
hnol
ogie
s th
at a
re d
ualu
se t
echn
olog
ies
whi
ch b
enef
itou
r pr
ime
cust
omer
bas
e.
• U
EE
Tne
w w
ill c
onti
nue
to e
mph
asiz
e pa
rtne
rshi
p ef
fort
s w
ith
DoD
tha
t em
phas
ize
colla
bora
tiv e
effo
rts
to d
evel
op d
ual u
se t
echn
olog
ies.
• U
EE
Tne
w w
ill u
se s
yste
ms
stud
ies
resu
lts
as a
pri
me
fact
or in
pri
orit
izin
g an
d se
lect
ing
tech
nolo
gy e
ffor
ts. E
xper
t op
inio
n w
ill b
e em
ploy
ed w
here
ver
appr
opri
ate
(e.g
. are
as w
here
syst
ems
stud
ies
cann
ot c
urre
ntly
mod
el t
echn
olog
y im
pact
s).
NASA/CP—2004-212963/VOL1 72
Cri
tica
l asp
ects
of
UE
ET
Re
inve
ntio
n
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Low
er T
RL
eff
orts
-Lay
fou
ndat
ion
for
follo
w o
n pr
ojec
t-In
telli
gent
Pro
puls
ion
Syst
ems
-All
effo
rts
open
ly c
ompe
ted
and
sele
cted
-Par
tner
ship
s en
cour
aged
Hig
her
TR
L e
ffor
ts-C
ontr
ibut
ion
to a
chie
vem
ent
of U
EE
T g
oals
-App
ropr
iate
for
NA
SA in
vest
men
t-P
ossi
ble
dual
use
tec
hnol
ogy
wit
h pa
rtne
ring
wit
h D
oD-U
p fr
ont
com
mit
men
ts b
y co
st s
hari
ngpa
rtne
rC
ost
shar
ing
amou
nt a
nd ty
peT
echn
olog
y tr
ansi
tion
/inse
rtio
n pl
anA
ppro
ach
to u
tiliz
ing
NA
SA p
erso
nnel
, fac
iliti
es
NASA/CP—2004-212963/VOL1 73
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
UE
ET
new
Su
b P
roje
ct S
tru
ctu
reU
EE
Tn
ew S
ub
Pro
ject
Str
uct
ure
I&D
I&D
370
%L
TO
NO
xH
LL
WC
T1
IPSF
T4
HII
2
UE
ET
Joe
Shaw
Cat
hy P
eddi
e
John
Roh
de le
adC
arol
Gin
ty le
adM
ile W
atts
lead
Mar
y Jo
Lon
g-D
avis
lead
Car
olyn
Mer
cer
lead
1 HL
LW
CT
-Hig
hly
Loa
ded,
Low
Wei
ght
Com
pres
sor
and
Tur
bine
2 Hig
hly
Inte
grat
ed I
nlet
3 Int
egra
tion
and
Dem
onst
rati
on4 I
ntel
ligen
t pr
opul
sion
Sys
tem
Fou
ndat
ion
Tec
hnol
ogie
s
NASA/CP—2004-212963/VOL1 74
App
roac
h to
Re
inve
ntin
g U
EE
T
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
70%
LT
O N
Ox
Com
bust
or
Hig
hly
Loa
ded
Low
Wei
ght
Com
pres
sor&
Tur
bine
(H
LL
WC
T)
Hig
hly
Inte
grat
ed I
nlet
(H
II)
Inte
llige
nt P
ropu
lsio
n Sy
stem
F
ound
atio
n T
echn
olog
ies
(IP
SFT
)
Inte
grat
ion&
Dem
onst
rati
on (
I&D
)
FY
04F
Y05
FY
06F
Y07
FY
04Y
ear
of T
rans
itio
n
Tec
hnol
ogy
eval
uati
ons/
sele
ctio
ns/t
erm
inat
ions
Sub
proj
ects
NASA/CP—2004-212963/VOL1 75
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
70%
LT
O N
Ox
Com
bust
or
Hig
hly
Loa
ded
Low
Wei
ght
Com
pres
sor&
Tur
bine
(H
LL
WC
T)
Hig
hly
Inte
grat
ed I
nlet
(H
II)
Inte
llige
nt P
ropu
lsio
n Sy
stem
F
ound
atio
n T
echn
olog
ies
(IP
SFT
)
Inte
grat
ion&
Dem
onst
rati
on (
I&D
)
FY
04F
Y05
FY
06F
Y07
Em
issi
ons
tech
nolo
gies
req
uire
d fo
r IP
S
IPS
wor
ksho
psN
RA
IPS
Tec
hF
ound
atio
n
FY
04Y
ear
of T
rans
itio
n
Sub
proj
ects
Tur
bom
achi
nery
/mat
eria
ls t
echn
olog
ies
requ
ired
for
IP
S
Inle
t/no
zzle
tec
hnol
ogie
s re
quir
ed f
or I
PS
“Int
ellig
ent”
pro
puls
ion
syst
em t
echn
olog
ies
App
roac
h to
Re
inve
ntin
g U
EE
T-L
ower
TR
L
NASA/CP—2004-212963/VOL1 76
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
70%
LT
O N
Ox
Com
bust
or
Hig
hly
Loa
ded
Low
Wei
ght
Com
pres
sor&
Tur
bine
(H
LL
WC
T)
Hig
hly
Inte
grat
ed I
nlet
(H
II)
Inte
llige
nt P
ropu
lsio
n Sy
stem
F
ound
atio
n T
echn
olog
ies
(IP
SFT
)
Inte
llige
nt P
ropu
lsio
n Sy
stem
s P
roje
ct
FY
05F
Y06
FY
07F
Y08
Em
issi
ons
tech
nolo
gies
req
uire
d fo
r IP
S
Tur
bom
achi
nery
/mat
eria
ls t
echn
olog
ies
requ
ired
for
IP
S
Inle
t/no
zzle
tec
hnol
ogie
s re
quir
ed f
or I
PS
“Int
ellig
ent”
pro
puls
ion
syst
em t
echn
olog
ies
App
roac
h to
Re
inve
ntin
g U
EE
T-L
ower
TR
L
NASA/CP—2004-212963/VOL1 77
Dev
elop
ing
Hig
her
TR
L T
echn
olog
y P
artn
ersh
ips/
Tra
nsit
ions
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
A k
ey p
art o
f th
e ne
w U
EE
T P
roje
ct w
ill b
e th
e se
lect
ion
and
tran
sitio
n of
UE
ET
te
chno
logi
es w
ith in
dust
ry/ D
oD p
artn
ers
to a
suf
fici
ently
hig
h le
vel s
o th
at o
ur
part
ners
can
use
them
in f
utur
e “p
rodu
ct d
esig
ns’
afte
r fu
rthe
r te
chno
logy
eff
orts
that
go
beyo
nd N
ASA
’s c
hart
er (
i.e. T
RL
6).
The
suc
cess
of
this
eff
ort w
ill b
e on
e m
easu
re a
s to
how
UE
ET
will
be
grad
edbo
th b
y th
e go
vern
men
t (e.
g. N
ASA
HQ
, OM
B, C
ongr
ess)
and
our
par
tner
s.
But
we
mus
t add
ress
“co
rpor
ate
wel
fare
” co
ncer
ns a
nd d
oing
DoD
’sjo
b.
NASA/CP—2004-212963/VOL1 78
App
roac
h to
Re
inve
ntin
g U
EE
T-H
ighe
r T
RL
’s
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
70%
LT
O N
Ox
Com
bust
or
Hig
hly
Loa
ded
Low
Wei
ght
Com
pres
sor&
Tur
bine
(H
LL
WC
T)
Hig
hly
Inte
grat
ed I
nlet
(H
II)
Inte
llige
nt P
ropu
lsio
n Sy
stem
F
ound
atio
n T
echn
olog
ies
(IP
SFT
)
Inte
grat
ion&
Dem
onst
rati
on (
I&D
)
FY
04F
Y05
FY
06F
Y07
“TR
L6”
par
tner
ship
dem
os
FY
04Y
ear
of T
rans
itio
n
Tec
h re
adin
ess/
tran
siti
on
Indu
stry
pro
posa
ls
Sub
proj
ects
NASA/CP—2004-212963/VOL1 79
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
70%
LT
O N
Ox
Com
bust
or
Hig
hly
Loa
ded
Low
Wei
ght
Com
pres
sor&
Tur
bine
(H
LL
WC
T)
Hig
hly
Inte
grat
ed I
nlet
(H
II)
Inte
llige
nt P
ropu
lsio
n Sy
stem
F
ound
atio
n T
echn
olog
ies
(IP
SFT
)
Inte
grat
ion&
Dem
onst
rati
on (
I&D
)
FY
04F
Y05
FY
06F
Y07
TR
L5
annu
lar
rig
dem
os
Indu
stri
al p
ropo
sals
/dec
isio
ns
TR
L6
engi
ne d
emos
(pa
rtne
rshi
ps)
TR
L5
mat
eria
ls d
emos
Tec
hnol
ogy
tran
siti
on/in
sert
ion
App
roac
h to
Re
inve
ntin
g U
EE
T-H
ighe
r T
RL
’s
QA
T/U
EE
T p
artn
ersh
ip
NASA/CP—2004-212963/VOL1 80
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
70%
LT
O N
Ox
Com
bust
or
Hig
hly
Loa
ded
Low
Wei
ght
Com
pres
sor&
Tur
bine
(H
LL
WC
T)
Hig
hly
Inte
grat
ed I
nlet
(H
II)
Inte
llige
nt P
ropu
lsio
n Sy
stem
F
ound
atio
n T
echn
olog
ies
(IP
SFT
)
Inte
grat
ion&
Dem
onst
rati
on (
I&D
)
FY
04F
Y05
FY
06F
Y07
Som
e te
chno
logi
es w
ill n
ot r
equi
re e
ngin
e te
sts
to s
ucce
ssfu
lly
Som
e te
chno
logi
es w
ill n
ot r
equi
re e
ngin
e te
sts
to s
ucce
ssfu
lly t
rans
ition
.tr
ansi
tion.
Tec
hnol
ogy
tran
siti
on/in
sert
ion
Indu
stri
al p
ropo
sals
/dec
isio
ns
TR
L5
rig
dem
os (
part
ners
hips
)
App
roac
h to
Re
inve
ntin
g U
EE
T-H
ighe
r T
RL
’s
NASA/CP—2004-212963/VOL1 81
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
FY
06F
Y07
FY
08F
Y09
UE
ET
and
F&
SD p
roje
cts
will
TO
GE
TH
ER
pro
activ
ely
wor
k w
ith th
e c
UE
ET
and
F&
SD p
roje
cts
will
TO
GE
TH
ER
pro
activ
ely
wor
k w
ith th
e c u
stom
ers
to d
efin
e us
tom
ers
to d
efin
e an
d co
nduc
t the
req
uire
d fl
ight
dem
onst
rati
ons!
and
cond
uct t
he r
equi
red
flig
ht d
emon
stra
tion
s!
App
roac
h to
Re
inve
ntin
g U
EE
T-H
ighe
r T
RL
’s
UE
ET
Int
egra
tion
&D
emon
stra
tion
(I&
D)
UE
ET
Dem
os (
F&
SD)
NASA/CP—2004-212963/VOL1 82
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
So
me
thin
gs
wo
n’t
ch
ang
e!S
om
e th
ing
s w
on
’t c
han
ge!
NASA/CP—2004-212963/VOL1 83
Unm
anne
d A
eria
l V
ehic
le (
UA
V)
Non-Commercial Vehicles
Acc
ess-
to-
Spa
ce/H
igh
Mac
h P
latf
orm
Gen
eral
A
viat
ion
Air
craf
t (G
A)
4 P
AX
Commercial Vehicles
Su
bso
nic
Su
per
son
icH
yper
son
ic
Reg
iona
l Jet
T
rans
port
Lar
ge S
ubso
nic
Tra
nspo
rt
300
PA
X
50 P
AX
Hig
h Sp
eed
Civ
il T
rans
port
(H
SCT
)
300
PA
X
Supe
rson
ic
Bus
ines
s Je
t (SB
J)
10 P
AX
Ble
nded
Win
g B
ody
(BW
B)
500-
600
PA
X Mil
itar
y T
rans
port
(C
-17)
Adv
ance
d Fi
ghte
r
Bas
elin
e V
ehic
les
for
UE
ET
Tec
hnol
ogy
App
licat
ion
Stud
ies
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Thes
e ve
hicles
drive
the
tech
nology
inve
stmen
t st
rate
gy
Thes
e ve
hicles
dete
rmine
the
tech
nology
syne
rgies
NASA/CP—2004-212963/VOL1 84
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
will
ena
ble
futu
re g
ener
atio
n ve
hicl
es o
ver
a w
ide
rang
e of
flig
will
ena
ble
futu
re g
ener
atio
n ve
hicl
es o
ver
a w
ide
rang
e of
flig
ht s
peed
s.ht
spe
eds.
Vis
ion
Vis
ion
We
sup
po
rt t
he
visi
on
an
d a
re c
om
mit
ted
to
th
e su
cces
s o
f N
AS
A’s
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
(UE
ET
) P
roje
ct.
Will
iam
s In
tern
atio
nal
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Rob
ert D
. Sou
thw
ick,
Pra
tt &
Whi
tney
Fred
Kra
use,
Gen
eral
Ele
ctri
c A
ircr
aft E
ngin
es
Dim
itri M
avri
s, G
eorg
ia T
ech
Mah
moo
d N
aim
i, B
oein
g C
omm
erci
al A
irpl
ane
Com
pany
Tom
Har
tman
n, L
ockh
eed-
Mar
tin
Scot
t Cru
zen,
Wil
liam
s In
tern
atio
nal
Ger
ald
Bri
nes,
Alli
son-
Rol
ls R
oyce
Rob
ert J
. Sha
w, N
ASA
Gle
nn R
esea
rch
Cen
ter
Will
iam
Koo
p, A
ir F
orce
Res
earc
h L
abor
ator
yV
inod
Nan
gia,
Hon
eyw
ell
Tim
Con
ners
, Gul
fstr
eam
Las
t U
pdat
e-A
pril
2003
NASA/CP—2004-212963/VOL1 85
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
We
are
com
mit
ted
to
wo
rkin
g t
og
eth
er in
par
tner
ship
to
act
ivel
y
seek
ou
t o
pp
ort
un
itie
s
for
the
tran
sfer
of
app
rop
riat
e
tech
no
log
ies
bo
th in
to
and
ou
t o
f U
EE
T.
NASA/CP—2004-212963/VOL1 86
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Add
ress
ing
the
key
natio
nal a
gend
a ar
eas
that
will
con
trib
ute
toA
ddre
ssin
g th
e ke
y na
tiona
l age
nda
area
s th
at w
ill c
ontr
ibut
e to
21st
Cen
tury
21
st C
entu
ry
U. S
. aer
ospa
ce le
ader
ship
U. S
. aer
ospa
ce le
ader
shipTE
AM
NA
SA
DoD
FA
A
EP
A
Indu
stry
Uni
vers
itie
s
NASA/CP—2004-212963/VOL1 87
Bac
k-up
NASA/CP—2004-212963/VOL1 88
Pro
gra
m S
tatu
sP
rog
ram
Sta
tus
Oct
ob
er 2
003
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
Ult
ra E
ffic
ien
t E
ng
ine
Tec
hn
olo
gy
15%
fu
el b
urn
red
uct
ion
fo
r la
rge
sub
son
ic21
% p
roje
cted
fo
r 30
0 P
AX
25%
pro
ject
ed f
or
BW
B
8% f
uel
bu
rn r
edu
ctio
n f
or
smal
l su
bso
nic
, sm
all /
larg
e su
per
son
ic
21%
fo
r 50
PA
X18
% f
or
10 P
AX
SS
BJ
70%
N0x
red
uct
ion
(b
elow
ICA
O 9
6) f
or
sub
son
ic
(lar
ge
reg
ion
al)
com
bu
sto
rs
ove
r th
e L
TO
cyc
le
NA
SA
/ind
ust
ry p
artn
ersh
ip t
ests
of
sect
or
con
fig
ura
tio
ns
(TR
L4)
giv
e co
nfi
den
ce t
hat
tar
get
ob
ject
ive
will
be
reac
hed
.79
% r
edu
ctio
n p
roje
cted
fo
r 30
0PA
X83
% r
edu
ctio
n p
roje
cted
fo
r 50
PA
X
Sys
tem
s st
ud
ies
pro
ject
ion
s o
f co
mb
ined
imp
acts
of
UE
ET
te
chn
olo
gie
s u
sin
g a
vaila
ble
(lim
ited
) te
st d
ata
in T
RL
2-3+
ran
ge.
Init
ial p
rob
abili
stic
ass
essm
ent
resu
lts
ind
icat
e 94
% p
rob
abili
ty o
f m
eeti
ng
U
EE
T g
oal
fo
r 30
0 P
AX
Ben
efit
pro
ject
ion
s le
ss t
han
p
revi
ou
s ye
ars’
pro
ject
ion
sd
ue
to t
ech
no
log
y p
ort
folio
chan
ges
an
d r
efin
ed t
ech
no
log
yp
roje
ctio
ns.
Go
alS
tatu
sR
emar
ks
Sec
tor
test
s co
mp
lete
din
4Q
of
FY
03
NASA/CP—2004-212963/VOL1 89
Eva
l. of
Act
ive
Flo
w
Con
trol
Con
cept
sB
WB
Hig
h R
e N
o.
Val
idat
ion
UE
ET
Lev
el I
Mile
sto
ne
Sch
edu
le20
0020
0120
0220
0320
04F
Y
1.0
Pro
pu
lsio
n S
yste
ms
Inte
gra
tio
n a
nd
A
sses
smen
t
2.0
Em
issi
on
s R
edu
ctio
n
3.0
Hig
hly
Lo
aded
Tu
rbo
mac
hin
ery
4.0
Mat
eria
ls &
Str
uct
ure
s fo
r H
igh
Per
form
ance
5.0
Pro
pu
lsio
n A
irfr
ame
Inte
gra
tio
n
Pro
puls
ion
Sys
tem
(s)
Con
cept
ual D
efin
ition
Pre
limin
ary
Tec
hnol
ogy
Ben
efits
Ass
essm
ent
Fla
met
ube
Eva
l’s.
of 7
0% L
TO
NO
x C
once
pts
Met
hods
D
owns
elec
t
Flo
w C
ontr
ol C
once
pt(s
) S
elec
ted
for
FanF
low
Con
trol
Con
cept
(s)
Sel
ecte
d fo
r T
urbi
ne
Not
es:
1) P
CA
mile
ston
es a
re d
enot
ed b
y
2) W
BS
6.0
res
erve
d fo
r P
rogr
am M
gmt.
func
tions
2005
Inte
rim T
echn
olog
y A
sses
smen
tsIn
itial
Hig
h F
idel
ity
Sys
tem
Sim
ulat
ion
Ann
ular
Rig
Dem
os
(Lg.
Eng
.) -
70%
LT
O N
0x C
onfig
s.
Phy
sics
Bas
ed P
redi
ctio
n C
odes
Val
idat
ed (
Com
b.)
Hig
hly
Load
ed M
ultis
tage
V
alid
atio
n -
Com
pres
sor
Phy
sics
Bas
ed P
redi
ctio
n C
odes
Val
idat
ed (
T/M
)
Con
figur
atio
n X
V
alid
atio
n
Eva
l. of
Act
ive
Flo
w
Con
trol
App
roac
hes
Hig
hly
Load
ed H
P/L
P
Val
idat
ion
-T
urbi
ne
Fin
al T
echn
olog
yA
sses
smen
t
Flo
w C
ontr
ol C
once
pt(s
) S
elec
ted
for
Com
pres
sor
7.0
Inte
llig
ent
Pro
pu
lsio
n
Co
ntr
ols
Eng
ine
Arc
hite
ctur
e/P
ayof
f Stu
dies
Act
ive
Com
bust
ion
Con
trol
Stu
dies
8.0
Inte
gra
ted
Co
mp
on
ent
Tech
no
log
y D
emo
nst
rati
on
sIC
TD
Pla
n fo
r S
mal
lT
hrus
t Cla
ss E
ngin
es
2200
ºF C
MC
Lin
er D
emo
Asp
iratin
g S
eal D
emo
May
200
2 R
ebas
elin
e
Cer
amic
The
rmal
Bar
rier
Coa
ting
(TB
C)
Con
cept
(s)
Sel
ectio
n
Mat
’l S
ys. f
or C
MC
T
urbi
ne V
ane
Hig
h T
emp.
Mat
’ls.
Cap
abili
ties
Dem
os.
EP
M A
lloy
Upp
er
Tem
p. L
imit
Low
Con
duct
ive
Cer
amic
TB
C
Sys
tem
Sel
ecte
dC
once
pts
Sel
ecte
d fo
r 30
00ºF
C
MC
Mat
’l S
yste
mF
easi
bilit
y of
300
0ºF
C
MC
Mat
’l S
yste
m
Est
ab’d
.
Com
p. T
ools
Ava
il. fo
r D
esig
n of
Sin
gle
Cry
stal
N
icke
l-bas
e A
lloys
70%
LT
O N
0x R
ed.
Dem
o’d
-S
ecto
r R
ig
Init.
Low
N0x
Sec
tor
Rig
Dem
o.
Dow
nsel
ect R
egio
nal
Eng
. Con
trac
tor
Dow
nsel
ect L
arge
E
ng. C
ontr
acto
r
Sim
ulat
e B
ench
mar
k C
omb.
E
xper
imen
t w/ L
iqui
d S
pray
Inj
ecto
r
Con
trol
s A
rchi
tect
ure/
Pay
off S
tudi
es
Inte
grat
ed C
ompo
nent
Tec
hnol
ogy
Dem
onst
ratio
ns P
lan
-->
f/Lg
. Thr
ust C
lass
Eng
.
ICT
C P
lan
for
Acc
ess
to S
pace
E
ngin
es
2006
Flo
w C
ontr
ol
Pro
of-o
f-C
once
pts:
-F
an
-C
ompr
esso
r
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.
Fea
sibi
lity
of U
HT
C a
s >
300
0ºF
-S
truc
tura
l or
Fun
ctio
nal C
oatin
g M
at’l.
NASA/CP—2004-212963/VOL1 90