scramjet : Related Words Words similar in meaning to scramjet

ramjet«
mach«
jet engine«
scramjets«
turbojet«
scramjet engine«
engine«
turbo-ramjet«
supersonic«
fuel«
rocket«
pulsejet«
combustion«
specific impulse«
pulse detonation engine«
speed«
combustion chamber«
jet«
vehicle«
hypersonic«
thrust«
rocket engine«
scramjet operation«
aircraft«
scramjet vehicle«
air«
flow«
gas«
orbital speed«
oxidizer«
combustor«
inlet«
hifire«
subsonic speed«
velocity«
atmosphere«
weight«
liquid oxygen«
orbit«
payload«
subsonic velocity«
temperature«
active cooling«
drag«
weight ratio«
incoming air«
nozzle«
supersonic flow«
flight«
waverider«
ciam«
operating range«
twin scramjet engine«
similar verification«
scramjet stage«
onboard oxidiser«
mode scramjets«
hypersonic airbreathing vehicle«
single stage vehicle«
fuel mass fraction«
compressor fan«
compressed flow«
efficiency«
payload mass fraction«
scramjet design«
scramjet technology«
subsonic combustion«
advantage«
supersonic combustion ramjet«
coolant«
supersonic combustion«
thrust nozzle«
reusable vehicle«
hypersonic velocity«
hyper«
stage«
lower thrust«
kinetic energy«
complexity«
tankage«
turbomachinery«
ramjet engine«
hypersonic speed«
engine efficiency«
aerodynamic lift«
acceleration«
launch system«
technology organisation«
hydrogen«
reaction«
solid rocket booster«
vehicle speed«
test vehicle«
supersonic flight«
atmospheric oxygen«
range«
heat«
temperature rise«
oxygen content«
turbofan engine«
mass«
turbojet engine«
liquid hydrogen«
direct relation«
disadvantage«
nasa«
pressure«
lower speed«
supersonic speed«
deceleration«
fuel injection«
launch vehicle«
atv«
altitude«
x-51a waverider test«
x-51a craft«
x-30 research«
world record hypersonic airspeed«
whitney rocketdyne scramjet engine«
vehicle total mass«
usable dynamic pressure«
usable control technique«
upper operating«
unmanned x-51a waverider«
uk defense company qinetiq«
typical turbojet engine«
typical space capsule«
typical ramjet«
transatmospheric lifter«
tether vehicle«
tankage ratio«
takeoff fuel weight«
takeoff dry weight«
t3 ground test facility«
supersonic speed result«
supersonic inflow«
successful scramjet flight«
suborbital atmospheric propulsion«
speed scramjet«
speed jet-«
specialized rocket research vehicle«
single stage transfer«
simulated mach«
separate fuel supply«
scramjet ﬂight«
scramjet test«
scramjet launch vehicle«
scramjet hardware«
scramjet ground test«
scramjet flow«
scramjet experimentation«
scram engine«
rocket propulsion system facility«
resistant underside«
regenerative cooling technique«
reduced reaction scheme«
reaction space launch development«
pyrophoric fuel additive«
pure scramjet engine«
pure scramjet«
professor ray stalker«
primary jp-7 fuel«
powerful solid rocket booster«
potential combustion heat release«
orbiter gross weight«
orbital vehicles«
optimal climb/descent profile«
nasa langley arc«
minimum mach«
mediocre thrust«
lower performance rocket«
lower intake dynamic pressure«
limited combustion«
level atmospheric flight«
langley ahstf«
intricate turbomachinery«
installation drag«
inlet diffuser«
initial propulsion requirements«
initial propulsion requirement«
initial mass ratio«
hyshot project«
hyshot flight test«
hypersonics technology«
hypersonic flying laboratory«
hypersonic flight regime«
hypersonic airbreathing«
hifire.«
hifire flight«
heg shock tunnel«
heavy faa regulation«
heated scramjet test facility«
gas aerothermodynamics«
fuel heat«
fuel constant«
final design method«
faulty control fin«
extra rocket engine«
experimental scramjet engine«
experiment ﬂight«
expensive hypersonic test chamber«
equal takeoff weight«
engine installation drag«
empty mass fraction«
droppable solid rocket booster«
dr. frederick s. billig«
downstream influence propagates«
discrete engine«
current scramjet technology«
coolant circulating«
constant vehicle takeoff weight«
constant dynamic pressure path«
connect test«
combustive standpoint«
cold model«
ciam test«
c-16 v/k facility«
boundary layer modeling«
boeing x-51 scramjet demonstrator«
axisymmetric hydrogen«
autonomous hypersonic flight control«
american defense scientist«
altitude specific«
aircraft top speed«
aerospace hardware cost«
aerodynamic maneuvering surface«
advanced scramjet«
additional oxidizer«
active cooling scheme«
propulsion«
x-51a waverider«
v scramjet flight experiment«
typical jet engine«
supersonic combusting ramjet«
style compression«
shcramjet«
scramjet power«
scramjet development«
scramjet combustor«
scramjet combustion«
reasonable computation«
ramjet type«
performance turbopumps«
mode scramjet«
maximum flight velocity«
instrumentation cost«
immense drag«
extreme technical challenge«
experimental scramjet«
dr. gordon l. dugger«
divergent thrust nozzle«
constant air pressure«
boeing x-51a«
atmospheric velocity«
airflow control system«
air upstream«
ablative shielding«
intake«
compression«
design«
x-51a«
x-43a.«
vehicle skin«
typical rocket engine«
traditional rocket«
thermal choking«
theoretical projection«
pure rocket power«
hypersonic international flight research experimentation«
freestream air«
equipment subject«
detachable rocket«
air impurity«
test«
total pressure loss«
takeoff mass«
short test time«
sa-5 surface«
orbital tether«
hypersonic rocket«
hypergolics«
flight test series«
expensive launch vehicle«
efficient thrust«
arc facility«
ahstf«
additional propulsion«
achievable speed«
sufficient compression«
special cooling«
reentry system«
lower mach«
loss coefficient«
length trip«
inlet fan«
indian space agency isro«
upper speed limit«
turbo pump«
total configuration«
reentry«
mechanical compressor«
fuelled rocket«
conventional turbofan«
complex fuel«
comparable density«
vehicle drag«
shock tunnel«
fuel stream«
failure prone«
depressed trajectory«
thrust/weight ratio«
poor thrust«
hypersonic technology«
expensive testing«
severe demand«
perfect simulation«
moter«
low supersonic speed«
low lift«
kholod«
hypersonic flight experiment«
heavy craft«
cryogenic facility«
cheaper access«
x-43a«
gravity loss«
aviation motor«
australian defence science«
u defense advanced research project agency«
total enthalpy«
test craft«
propellant«
other fuel«
conventional jet engine«
supersonic flight speed«
freestream«
supersonic airflow«
orbit vehicle«
flame holder«
significant thrust«
flight test data«
final acceleration«
x team«
simple liquid«
ram accelerator«
hypersonic flow«
simple formulation«
liquid air cycle engine«
hypersonic aircraft«
united state land«
speed flow«
missile flight«
divergent nozzle«
combustion rate«
central motivation«
busemann«
analytical paper«
advanced technology vehicle«
calculation«
successful flight test«
oxygen«
amount«
stagnation temperature«
dense fluid«
payload fraction«
normal shock«
magnitude«
modern rocket«
base configuration«
cost«
unit«
propulsion method«
subsonic flow«
energy fuel«
speed characteristic«
heat insulation«
x project«
joint research program«
many proposal«
structure«
throttling«
tolerable level«
combined cycle«
density«
lack«
higher speed«
eventual cost«
turbulent mixing«
space shuttle external tank«
turbine stage«
orbit due«
engine jet«
billig«
flight altitude«
outback south australia«
throttle setting«
woomera test range«
flameout«
hypersonic flight«
final application«
atmospheric test«
reaction scheme«
loss«
70.85kg/m³)and«
1:1 simulation«
90-minute flight«

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