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8/9/2019 NASA X-15 Rocket Poster
1/1
Burnout
AAARR
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NOOOONNNNNAAAAA
UTA
H
NEVAADDAA
AD
ORE G O N
F ee t 3 50TYPICALHIGH-ALTITUDE (Thousands)
SSSTTRRRATOOOSPPHEERE
IIONNNOOSSPP
jy f svy, h X-15 m h fss hhs-y p w pf s m. is svs s naSa s f h xp f sp.
To The edge ofBallistic theouter
sskinotheX-15 was
pmadeoanickel-chr
aomiumalloy
ce...
SenSational, iconic, groundbreaking. th X-15 hyps sh psy x h fs f h. i ws pm f s hvms,
jw-pp pfm hss, xy hm v. d 15-y
354,200 thighesT alTiTudeaTTainedfor a wingedaircrafT (ThaTs67
mileshigh!)andanachievemenT noTsurpassed unTil 2004
NW-2008-09-195-HQ
1,325 fThepeaKsurfaceTemperaTureofa TesT panel on
The X-15 duringa mach 5 mission
4,520 Topspeedof mach 6.70 anachievemenTunBroKen for 41 years
8-The g-forceeXperiencedByX-15piloTson
someflighTsduringreenTryinToearThsaTmosphere
a wing and a prayertsc j
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,
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.
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noselowdirection
sensorprovidedaccurate
measurementoangle
oattackandangleo
sideslipatsupersonicand
hypersonicvelocities.
pitothead
three-panels-thick
windshield(heated
withnitrogen
gastoprevent
rosting/ogging)
no.2eQuipment
compartment
skylight
hatch
use
panel
lauXiliary
power
units
iQuidnitrogentank
(airconditioning
andpressuriZation
system)
l
liQuid
oXygen
tankvent
liQuidoXygen
tank(engine
oXidiZer)
heliumtank
(orengine
propellant
pressuriZation)
controlsystem
thrusters
calledinconelX ,employedin ahotstructurethatwascapaBle
owithstandingtemperaturesineXcesso1200.theBeams and
sparsothewings andthering structureotheuselagewere
constructedromstrong titanium-manganesealloy.
w inglap
wingattachmentstructure
ammoniatank (engineuel)
hydrogenperoXidetank
(engineturBopumppropellant)
movaBle
uppervertical
staBiliZer
upper
speed
Brake
Xlr99-rm-1rocket engine
heliumtank(orenginepurge)
all-moving
horiZontal
staBiliZer
owerverticalstaBili Zer
(JettisonedJustBeor e
landing)
retractaBle
landinggear
skids
Ballistic
controlsystem
thrusters
no.3eQuipment
compartment
heliumtank(or
pressuriZation)liQuidoXygen
tankiller
hydraulicsystem
reservoirs
hydrogen
peroXidetank
(auXiliarypower
unitandBallistic
controlsystem
propellant)
heliumtank
(auXiliary
powerunit
propellant
pressuriZation)
telemetry
recorders
areaor
eXperiments
no.1eQuipment
compartmentBallistic
controlsystem
thrusters
half a million horsepowertbX15Xlr99.tx
b mtjX15
q.
dbbrmdtc,Xlr99
57,000, q .
tqx,bb
13,000.
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X15a2150.
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BX1 Xlr99
.
I
1 tankpressuriZationselecto
2 enginethrottle
3 altimeter
4 airspeed/machindicator
5 accelerometer
6 conventionalcenter stick
(movedtheaerodynamic
controlsuraces)
7 verticalvelocity indicator
8 systemwarninglights
9 canopyemergency
Jettisonhandle
754
3
8
9
1
6
2
flying aT The edget
,z
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iXb
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The carrier aircrafT
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.cb2 m5m6
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,b
2
HHEERREE
TYPICALHIGH-SPEEDMISSION PROFILE 3003.Controlin
near vacuum
250
4. Reentry 2. Leave 99.9%
heating200
atmosphere
Burnout
MISSION PROFILE
150
1.Launchfrom B-52
1005.Pull-out
65,000 ft
50
WENDOVER AFB
0
ELYHIGH RANGETRACKING
BEATTY STATIONHIGH RANGETRACKING
STATION
EDWARDS AFB
6.Glide tolanding
flighT s of discovery X-15 achievemenTsTheX-15slegacyis quanTifiaBlenoTJusTinTerms of speed or alTiTude achievemenTs,BuTals o in Terms of whaT iTTaughTnasaand The american puBlic aBouTThe fuTurepossiBiliTies of hypersonic flighT.These achievemenTs include:
r
dt t t t - t t tt
ft t t t k t t t
dt t-b t t- t
dt -tt b t t -t ttk t
dt t t t tb t t
dtt t bt t t kt-bt tt xt
heroes of The hypersonicatt 12tttnasa, tu.s.af,t u.s. n nt a at t X-15.
a. stt cnaac
X15.h
J8,1959,
sb17.h
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,x
m2.971,960.iJ1962,
j c
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nasam 25,1960.
h25
354,200
a22,1963.h
4,104bX15
.iJ1962,
jct,
bp
J.k.
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X15ba13,
1960,db14,1962.w
m4,56,
b200,000
300,000.hf
X15
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17,1962,aq
i
.
nasa
ft s. ptpn
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b
J10,
1962,ml.iJ 1962,
j c
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,m5.65
a26,1964,
295,600
sb28,1965.mk
jnb9,
1962,
ml,b
22X15 .t
b
X15a2.
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,34
,2
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m6.064,018
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X15.a
nasa,
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jnasaac.h
224
ssd
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mt o. TtbX15
ob29,1963,
14x2
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nasa X20
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.
X-15programmilesTones
1952T nt actt at,naca,tt tm10t
tt 12 t 50 .
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b t X-15.
1954naca,tu.s.a u.s.n mut t t "Jtpjt n h-s
r a."
1955ntaat ttX-15
.
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1957cttbt X-15.
1958wktX-15-1t.
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1959ftttX-15-1.
1960ftttXlr99.
1961fttbm 5.
1961fttb200,000 t.
1961fttbm 6.
1961fttb300,000 t.
1963fttb50 .
1963u tt354,200tt at 22.
1967u m6.70(4,520)t
otb3.
1968Tt,tbBd,tk
otb24.www.nasa.gov
Bd, 199X15.i1960
1970,d jbdrc.
theX-15megagraphicsteam:
asnasahq,pmdrc,dr.J,tldrc,
kl.rnasahq
ThePipeworksDesignCollective:
pdb,,sp,j,cc,hp3d
Formoreinformation:://...