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Rocket engine operation method
rocket engine. In the staged combustion cycle, propellant flows through multiple combustion chambers, and is thus combusted in stages. The main advantage
Staged_combustion_cycle
air staged supply and fuel staged supply. Applications of staged combustion include boilers and rocket engines. Air staging, or two-stage combustion, is
Staged_combustion
SpaceX family of liquid-fuel rocket engines
subcooled liquid oxygen in a full-flow staged combustion cycle. This type of combustion is a twin-shaft staged combustion cycle that uses both oxidizer-rich
SpaceX_Raptor
Rocket engine power cycle
in October 2022. Expander cycle Pressure-fed engine Rocket engine Staged combustion cycle Gas-generator cycle Electric-pump-fed engine Sutton, George
Combustion_tap-off_cycle
Type of rocket engine which uses liquid fuel stored at very low temperatures
efficiency, staged-combustion engines can fill both roles at the cost of greater complexity, and expander engines are exclusively used on upper stages due to
Cryogenic_rocket_engine
Type of reciprocating heat engine
external combustion engine (EC engine) is a reciprocating heat engine where a working fluid, contained internally, is heated by combustion in an external
External_combustion_engine
Liquid fuel rocket engine
engine burning liquid oxygen and liquid methane in an oxidizer-rich staged combustion cycle. It is designed by aerospace company Rocket Lab for its Neutron
Archimedes_(rocket_engine)
Engine in which fuel combusts with an oxidizer
internal combustion engine (ICE or IC engine) is a heat engine in which the combustion of a fuel occurs with an oxidizer (usually air) in a combustion chamber
Internal_combustion_engine
Rocket engine that uses liquid fuels and oxidizers
Examples: RL10 for Atlas V and Delta IV second stages (closed cycle), H-II's LE-5 (bleed cycle). Staged combustion cycle A fuel- or oxidizer-rich mixture is
Liquid-propellant_rocket
Rocket engine operation method
the BE-3U engine used on the upper stage of its New Glenn launch vehicle. In a similar way that the staged combustion can be implemented separately on the
Expander_cycle
Rocket engine operation method
gas generator (analogous to, but distinct from, a preburner in a staged combustion cycle) and the resulting hot gas is used to power the propellant pumps
Gas-generator_cycle
Space launch vehicle in development
company redesigned Helix from a gas-generator cycle to an oxygen-rich staged combustion cycle. Some components used in early engine versions, such as the
RFA_One
Proposed Soviet rocket engine
USSR. The RD-701 would have been a tripropellant engine that used a staged combustion cycle with afterburning of oxidizer-rich hot turbine gas. The RD-701
RD-701
Major component of a liquid rocket engine
a mechanically simple but slightly less efficient powerhead. In a staged combustion cycle the preburner gas is routed into the main chamber instead, raising
Powerhead_(rocket_engine)
Pump driven by a gas turbine
reaction design (common in staged combustion and other closed cycles). They can consist of one or more stages, where each stage has both a stator, which
Turbopump
Rocket engine operation method
II upper stage[citation needed] Copenhagen Suborbitals' Spica Gas-generator cycle Combustion tap-off cycle Expander cycle Staged combustion cycle Electric-pump-fed
Pressure-fed_engine
Launch system that only uses one rocket stage
A single-stage-to-orbit (SSTO) vehicle reaches orbit from the surface of a body using only propellants and fluids and without expending tanks, engines
Single-stage-to-orbit
American aerospace company
firing stand. The first successful hot fire of Stoke Space's full flow staged combustion (FFSC) Engine, named Zenith, was reported in June 2024. In January
Stoke_Space
Burning of fuel with pure oxygen
temperature, so the mixture is diluted by mixing with recycled flue gas, or staged combustion. The recycled flue gas can also be used to carry fuel into the boiler
Oxy-fuel_combustion_process
Rocket engine
oxidizer-rich staged combustion cycle rocket engine burning LOX and kerosene developed by Space Pioneer. The TH-11 engine features a reusable design, staged combustion
TH-11
Large liquid methane fuelled staged-combustion rocket engine by Blue Origin
Origin. It uses liquefied methane fuel and operates on an oxygen-rich staged combustion cycle. The BE-4 produces 2,800 kN (640,000 lbf) of thrust at sea level
BE-4
Aerospace manufacturer in Colorado, US
about 270 employees. The company announced that it would supply the upper stage engine for Astra Space’s in-development Rocket 4. As of 2024 its Draper
Ursa_Major_Technologies
Rocket engine operation method
of which power the first stage of Astra Space's Rocket 3. In comparison to turbo-pumped rocket cycles such as staged combustion and gas generator, an electric
Electric-pump-fed_engine
Reusable first-stage rocket developed by SpaceX
uses a full-flow staged combustion cycle with oxygen and methane-rich turbopumps. Before 2014, only two full-flow staged-combustion rocket engine designs
SpaceX_Super_Heavy
Russian rocket engine manufacturer
created in 1969-1974 for RS-18 rocket first stage. Further on, two engines were developed: staged combustion RD0235, and open cycle steering engine RD0236
Chemical Automatics Design Bureau
Chemical_Automatics_Design_Bureau
Reusable medium-lift launch vehicle
Services Program. The first stage design includes 7 full-flow staged combustion rocket engines, burning methalox. The second stage measures 13 ft (4.0 m) in
Stoke_Space_Nova
Russian rocket engineer (1908–1971)
because it avoided the need for separate fuel lines to each sprayer. Staged combustion (Замкнутая схема) was first proposed by Alexey Isaev in 1949. Although
Aleksei_Isaev
Reusable spacecraft under development by SpaceX
a full-flow staged combustion cycle, which has both oxygen and methane-rich turbopumps. Before 2014, only two full-flow staged-combustion rocket engine
SpaceX_Starship_(spacecraft)
Space Shuttle and SLS main engine
staged combustion, de Laval-type engine. The request was based on the then-current design of the Space Shuttle which featured two reusable stages, the
RS-25
Chinese liquid-fuel rocket engine
rocket engine burning liquid methane and liquid oxygen in a full-flow staged combustion cycle. The engine is currently under development and is designed to
YF-215
Large Soviet rocket engine that used hypergolic propellants
being about 26 MPa. This was achieved by applying the full-flow staged combustion cycle for all the incoming mass of fuel, which is turned into a gas
RD-270
Hypothetical spacecraft propulsion through continuous nuclear explosions for thrust
increased. One "pulse" consist of the injection of a fuel pellet into the combustion chamber, its consumption through a series of fission-fusion reactions
Nuclear_pulse_propulsion
Allegedly unexplained human incineration
Spontaneous human combustion (SHC) is the pseudoscientific concept of the spontaneous combustion of a living (or recently deceased) human body without
Spontaneous_human_combustion
Rocket engines developed by SpaceX
methane-based engines for their future rockets. These engines would use staged cycle combustion, for higher efficiency similar to the system used on the former
SpaceX_rocket_engines
Chinese liquid-fuel rocket engine
hydrogen and liquid oxygen in a staged combustion cycle. It is China's first hydrogen-oxygen engine to use the staged combustion cycle and is expected to be
YF-90
Russian rocket engine
for both the first and second stage. But to achieve the required performance, Kosberg had to develop a staged combustion engine, a then extremely aggressive
RD-0210
Rocket driven by nuclear fusion power
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Fusion_rocket
U.S. Air Force project in the 1990s and early 2000s
sometimes also termed a powerpack) that would utilize a full flow staged combustion cycle (FFSC). The prime contractors were Rocketdyne and Aerojet. The
Integrated Powerhead Demonstrator
Integrated_Powerhead_Demonstrator
Partially-reusable heavy-lift launch vehicle by Blue Origin
plans called for the first stage to be powered by seven of Blue Origin's BE-4 single-shaft oxygen-rich staged combustion liquid methane/liquid oxygen
New_Glenn
Proposed spacecraft propulsion method
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Bussard_ramjet
Proposed nuclear pulse propulsion through antimatter-catalyzed nuclear chain reactions
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Antimatter-catalyzed nuclear pulse propulsion
Antimatter-catalyzed_nuclear_pulse_propulsion
Non-airbreathing engine used to propel a missile or vehicle
the combustion temperature sufficiently. Staged combustion (Замкнутая схема) was first proposed by Alexey Isaev in 1949. The first staged combustion engine
Rocket_engine
Proposed rocket propulsion mechanism
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Nuclear_salt-water_rocket
Type of rocket engine fuel
valves. The propellants, in turn, flow through control valves into the combustion chamber; there, their instant contact ignition prevents a mixture of unreacted
Hypergolic_propellant
Type of electric propulsion
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Plasma_propulsion_engine
Reusable superheavy-lift general-purpose launch vehicle
uses a full-flow staged combustion cycle with oxygen and methane-rich turbopumps. Before 2014, only two full-flow staged-combustion rocket engine designs
SpaceX_Starship
Large staged combustion rocket engine by Blue Origin
the Apollo Lunar Module's Descent Stage Lunar Module Ascent Engine – used on the Apollo Lunar Module's Ascent Stage RL10 – Ubiquitous LOX/LH2 expander
BE-7
Russian rocket engine
an RP-1/LOX mixture and uses an extremely efficient, high-pressure staged combustion cycle. The engine runs with an oxidizer-to-fuel ratio of 2.72 and
RD-180
Space propulsion system, electrostatic gridded ion thruster
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
NASA Solar Technology Application Readiness
NASA_Solar_Technology_Application_Readiness
Conceptual rocket engine
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Direct_Fusion_Drive
Space propulsion system, a gridded electrostatic ion thruster
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
NEXT_(ion_thruster)
Rocket engine
is a 22-kilonewton (5,000 lbf) thrust Kerosene/LOX oxidizer-rich staged combustion cycle rocket engine. Hadley is the first engine developed by Ursa
Hadley_engine
Partially-reusable medium-lift launch vehicle
this way. The first stage is powered by 9 oxygen-rich staged-combustion CH4/LOx ("methalox") Archimedes rocket engines. The second stage of Neutron is completely
Rocket_Lab_Neutron
Russian liquid-fuei rocket engine
RD-193 is fueled by a kerosene / LOX mixture and uses an oxygen-rich staged combustion cycle. RD-193 was proposed as a replacement for the NK-33, which is
RD-193
Russian rocket engine
oxygen-rich staged combustion cycle, developed by the Chemical Automatics Design Bureau in Voronezh. RD-0124 engines are used on the Block I stage used on
RD-0124
Type of rocket nozzle
service. It was a liquid oxygen/liquid hydrogen design that used staged combustion and generated about 250,000 lbf (1,100 kN) thrust. An enlarged version
Expanding_nozzle
Topics referred to by the same term
A combustion engine is an engine which generates mechanical power by combustion of a fuel. Combustion engines are of two general types: Internal combustion
Combustion_engine
Japanese hydrolox staged combustion rocket engine
The LE-7 and its succeeding upgrade model the LE-7A were staged combustion cycle LH2/LOX liquid rocket engines produced in Japan for the H-II series of
LE-7
Rocket engine using oxidizer-rich staged combustion, 2.2 MN thrust
200-kilonewton-class (500,000 lbf) thrust RP-1/LOX oxidizer-rich staged combustion cycle rocket engine project. The engine was conceived in 2014, and
Aerojet_Rocketdyne_AR1
Soviet rocket engine
combustion chamber pressure with reduced complexity and cost (but it was single-use), as compared to the RS-25. It uses a fuel-rich staged combustion
RD-0120
Chinese super-heavy rocket in development
the same type. The third stage is optional and uses a single 120-tonne-thrust liquid hydrogen/liquid oxygen staged combustion engine named the YF-91. Long-term
Long_March_9
Type of electric propulsion system
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Hall-effect_thruster
Russian rocket engine
RD-191 is fueled by a kerosene / LOX mixture and uses an oxygen-rich staged combustion cycle. In the future the engine is expected to become a workhorse
RD-191
Spacecraft propulsion system by NASA. 50kW Hall-effect thrusters, now for Lunar Gateway
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Advanced Electric Propulsion System
Advanced_Electric_Propulsion_System
Soviet rocket engine
oxygen-rich staged combustion cycle, they are not directly related to the NK-33. The N1 launcher originally utilized NK-15 engines for its first stage and a
NK-33
American metallurgist (born c. 1965)
At Rocketdyne, Reza began working on the problem of oxygen-rich staged combustion cycle engines. American engine manufacturers had historically avoided
Monica_Reza
Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially
limitations across phases; and the difficulty of achieving and sustaining combustion of the metal. In the 1960s, Rocketdyne test-fired an engine using a mixture
Tripropellant_rocket
Type of solar sail
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Diffractive_solar_sail
Rocket with a motor that uses solid propellants
cannot be shut off, as it contains all the ingredients necessary for combustion within the chamber in which they are burned. More advanced solid rocket
Solid-propellant_rocket
Type of spacecraft propulsion system
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Nuclear_electric_rocket
Type of nuclear propulsion method with an ultra high specific-inpulse
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Fission-fragment_rocket
Liquid form of rocket propellants
than alcohol, but standard gasoline and kerosene left too much soot and combustion by-products that could clog engine plumbing. In addition, they lacked
Liquid_rocket_propellant
Proposed US kerolox rocket engine
The TR-107 was a developmental rocket engine designed in 2002 by Northrop Grumman for the NASA and DoD-funded Space Launch Initiative (SLI). Operating
TR-107
Rocket engine
engine, which was the first staged combustion engine in the world. The engine was initially created to power the Blok D stage of the Soviet Union's abortive
RD-58
Type of spacecraft electric propulsion system
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Arcjet_rocket
Soviet (now Russian) liquid rocket engine
11D123) is a liquid upper stage rocket engine burning RG-1 (refined kerosene) and LOX in an oxidizer rich staged combustion cycle with an O/F ratio of
RD-120
Physical and science fiction concept
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Anti-gravity
Type of spacecraft propulsion using electrical energy to accelerate propellant
Conventional rockets achieve motion by expelling mass, most commonly the combustion output from chemical propellants to generate thrust via Newton's third
Spacecraft electric propulsion
Spacecraft_electric_propulsion
Type of spacecraft plasma propulsion system
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Pulsed_inductive_thruster
Proposed spacelaunch method
weapons in a similar manner as classic firearms or cannon using chemical combustion. Hybrids between coilguns and railguns such as helical railguns are also
Mass_driver
Form of electrically powered spacecraft propulsion
through the exhaust chamber. Unlike chemical propulsion, there is no combustion of fuel.[citation needed] As with other electric propulsion variations
Magnetoplasmadynamic_thruster
Electrothermal thruster in development
ISBN 978-1-62410-037-6. Retrieved April 2, 2023. "VASIMR VX-200 first stage achieves full power rating" (PDF) (Press release). Ad Astra Rocket Company
Variable Specific Impulse Magnetoplasma Rocket
Variable_Specific_Impulse_Magnetoplasma_Rocket
Chinese rocket engine
LOX and kerosene in an oxidizer-rich staged combustion cycle. The engine is designed for use on the first stage of the Chinese government's new generation
YF-100
Soviet (now Russian) rocket engine, the most powerful in the world
four combustion chambers, all supplied by one single-shaft, single-turbine turbopump rated at 170 MW (230,000 hp) in an oxidizer-rich stage combustion cycle
RD-170
Rocket engine
to use a closed-cycle design with staged combustion of generator gas in the combustion chamber. For the second stage of this missile, the NK-9V engine
NK-9
Soviet rocket engine
RG-1 (a rocket grade kerosene) in an oxidizer rich staged combustion cycle. It has four combustion chambers that provide thrust vector control by gimbaling
RD-8
UDMH/N2O4 burning engine in the staged combustion cycle. Development years: 1962-1968 . For use as main engine of the first stage of R-27. First engine submerged
A.M. Isayev Chemical Engineering Design Bureau
A.M._Isayev_Chemical_Engineering_Design_Bureau
Indian semi-cryogenic rocket engine
kerosene in an oxidizer-rich staged combustion cycle, the engine will boost payload capacity of LVM3 replacing current L110 stage powered by 2 Vikas engines
SE-2000
Prototype spacecraft propulsion engine
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Helicon_double-layer_thruster
Nuclear spacecraft propulsion technology
Most liquid-fueled chemical rockets use either hydrogen or hydrocarbon combustion, and the propellant is therefore mainly water (molecular mass 18) and
Nuclear_thermal_rocket
Ukrainian rocket engine
rocket engine burning LOX and Kerosene (RG-1) in a staged combustion cycle. It has a single combustion chamber that provides thrust vector control by gimbaling
RD-810
Thermodynamic cycle
The Atkinson-cycle engine is a type of internal combustion engine invented by James Atkinson in 1882. The Atkinson cycle is designed to provide efficiency
Atkinson_cycle
Form of electric spacecraft propulsion
run briefly on the ground EADS Radio-frequency Ion Thruster (RIT) Dual-Stage 4-Grid (DS4G) Hall-effect thrusters accelerate ions by means of an electric
Ion_thruster
Spacecraft propulsion device
Hypergolic Monopropellant Bipropellant Tripropellant Power cycles Staged combustion cycle Expander cycle Gas-generator cycle Tap-off cycle Intake mechanisms
Thrusters_(spacecraft)
Term for nitric oxide and nitrogen dioxide
oxidation (FLOX) and staged combustion significantly reduce thermal NOx in industrial processes. Bowin low NOx technology is a hybrid of staged-premixed-radiant
NOx
American space company
Mojave Air and Space Port facilities. Deneb is a 15,000 lbf (67 kN) staged combustion cycle engine that uses liquid oxygen (LOX) and methane as propellants
Impulse_Space
American aerospace propulsion manufacturer
200 kN) thrust RP-1/LOX oxidizer-rich staged combustion cycle engine. Rocketdyne H-1 (RP-1/LOX) – A first stage engine flown on the Saturn I and Saturn
Aerojet_Rocketdyne
Rocket engine that uses both liquid / gaseous and solid fuel
encouraged stable combustion. The oxidizer could be throttled with one valve, and a high oxidizer to fuel ratio helped simplify combustion. The negative observations
Hybrid-propellant_rocket
Soviet super heavy-lift launch vehicle (1965–1972)
used in Glushko's existing engines on various ICBMs. The full flow staged combustion cycle RD-270 was in testing before program cancellation, achieving
N1_(rocket)
Rocket that uses a single propellant with a catalyst
small altitude and trajectory control rockets in satellites, rocket upper stages, crewed spacecraft, and spaceplanes. The simplest monopropellant rockets
Monopropellant_rocket
STAGED COMBUSTION
STAGED COMBUSTION
Surname or Lastname
English
English : byname from Middle English staley ‘resolute’, ‘reliable’, a reduced form of Stallard.Belgian French : from Old French estalee ‘fish trap’, hence possibly a metonymic occupational name for a fisherman, or topographic name for someone who lived near where fish traps were set.
Female
English
Feminine variant spelling of English unisex Stacey, STACEE means "resurrection."
Surname or Lastname
English
English : occupational name for someone who made and drove in stakes, or a topographic name for someone who lived near a boundary post for example, from a derivative of Middle English stake ‘post’, ‘stake’.
Girl/Female
Muslim
Sageda is
Boy/Male
Muslim
Hunter
Surname or Lastname
English (mainly Newcastle and Durham)
English (mainly Newcastle and Durham) : of uncertain origin, probably a derivative of northern Middle English stang ‘pole’ (of Old Norse origin). Possible meanings include a topographic name for someone who lived by a pole or stake (compare Stakes) or an occupational name for someone armed with one. Alternatively, it may be a nickname for someone who had ‘ridden the stang’, i.e. been carried on a pole through the streets as an object of derision, in punishment for some misdemeanor. However, this custom is of uncertain antiquity.Orcadian : probably a habitational name from a minor place called Stanagar in the parish of Stromness.German : occupational name for a maker of shafts for spears and the like, from an agent derivative of Middle High German stange ‘pole’, ‘shaft’.
Girl/Female
Muslim
Honey, Witness, Patriot
Surname or Lastname
English and North German
English and North German : nickname for someone who stammered, from Middle English, Middle Low German stamer ‘stammerer’.
Surname or Lastname
English
English : topographic name for someone who lived by a prominent post or stake, for example a boundary marker, from Middle English stake ‘post’, ‘stake’, or from the same word used as a nickname for a tall, thin person.
Surname or Lastname
English and Irish
English and Irish : variant of Stacey.
Girl/Female
Hindu, Indian, Marathi
Stage
Girl/Female
Muslim/Islamic
Sageda is ..
Male
English
English unisex pet form of Latin Anastasia and Anastasius, both STACEY means "resurrection."
Surname or Lastname
English
English : nickname from Old English stagga ‘male deer’, ‘stag’. In northern dialects of Middle English the term was also used of a young horse, perhaps under Scandinavian influence, and in some cases this meaning may lie behind the original application of the name.
Surname or Lastname
English and Irish
English and Irish : from a pet form of the medieval male personal name Stace, a reduced vernacular form of Eustace.
Surname or Lastname
English
English : patronymic from Stagg.
Surname or Lastname
English
English : variant of Seager.Dutch (de Sager), and North German : occupational name from Dutch, Low German sager ‘sawyer’.French : from the Germanic personal name Sagher, composed of the elements sag- (an element related to Gothic and Old High German words meaning ‘quarrel’, ‘law-suit’) + hari, heri ‘army’.Jewish (Ashkenazic) : nickname from an agent derivative of German sagen ‘to say’.
Girl/Female
Indian
Sageda is
Surname or Lastname
English
English : variant of Stavers, an occupational name for a stave maker (see Staves), found predominantly in the northeast of England.
Surname or Lastname
English (East Midlands and South Yorkshire)
English (East Midlands and South Yorkshire) : possibly a metonymic occupational name for a stave maker, from the plural of Middle English staf ‘rod’, ‘staff’.
STAGED COMBUSTION
STAGED COMBUSTION
Boy/Male
Hindu, Indian, Kannada, Marathi, Sanskrit
Brave
Girl/Female
Tamil
Agreement
Female
English
Variant spelling of English Stephanie, STEFANIE means "crown."
Girl/Female
Hindu
Goddess Lakshmi
Female
Japanese
(è–è’²) Japanese name AYAME means "iris flower."
Boy/Male
American, Australian, British, Christian, English, German, Greek, Jamaican, Norse, Scandinavian, Scottish
Son of Andrew; Masculine
Girl/Female
American, Christian, Finnish, German, Hebrew, Indian, Swedish
Snow and Ice; God's Promise; God is My Oath; Noble; Nobility; Variant of Elizabeth; Pledged to God; God is Perfection; My God is a Vow
Girl/Female
Indian
Evil spirit.
Girl/Female
Hindu, Indian, Tamil
Daughter; Cute
Girl/Female
French
Form of Greek masculine Andrew, meaning manly or brave. Feminine form of Andre, masculine.
STAGED COMBUSTION
STAGED COMBUSTION
STAGED COMBUSTION
STAGED COMBUSTION
STAGED COMBUSTION
a.
Shaped like a wheel.
n.
A horse used in drawing a stage.
a.
Fascinated by the stage; seized by a passionate desire to become an actor.
a.
Pertaining to a stage; becoming the theater; theatrical.
a.
Shaped like an awl.
a.
Shaped like a saddle.
a.
Without scales, or with the scales removed; as, scaled herring.
n.
A degree of advancement in a journey; one of several portions into which a road or course is marked off; the distance between two places of rest on a road; as, a stage of ten miles.
a.
Recurring at regular time; not occasional; as, stated preaching; stated business hours.
a.
Having feathers which in form, color, or arrangement somewhat resemble scales; as, the scaled dove.
v. t.
To exhibit upon a stage, or as upon a stage; to display publicly.
a.
Shaped like a worm; /hick and almost cylindrical, but variously curved or bent; as, a worm-shaped root.
a.
Shaped like a strap; ligulate; as, a strap-shaped corolla.
n.
One of several marked phases or periods in the development and growth of many animals and plants; as, the larval stage; pupa stage; zoea stage.
a.
Shaped like a diamond or rhombus.
a.
Shaped like a globe.
n.
Exhibition on the stage.
a.
Shaped like the lash of a whip; long, slender, round, and tapering; as, a whip-shaped root or stem.
n.
A place of rest on a regularly traveled road; a stage house; a station; a place appointed for a relay of horses.
n.
One who has long acted on the stage of life; a practitioner; a person of experience, or of skill derived from long experience.