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Rocket engine that uses liquid fuels and oxidizers
A liquid-propellant rocket or liquid rocket uses a rocket engine burning liquid propellants. (Alternate approaches use gaseous or solid propellants.)
Liquid-propellant_rocket
Liquid form of rocket propellants
The highest specific impulse chemical rockets use liquid propellants (liquid-propellant rockets). They can consist of a single chemical (a monopropellant)
Liquid_rocket_propellant
Type of rocket engine fuel
hypergolic in Wiktionary, the free dictionary. A hypergolic propellant is a rocket propellant whose components spontaneously ignite upon contact with one
Hypergolic_propellant
Chemical or mixture used in a rocket engine
Rocket propellant is used as a reaction mass ejected from a rocket engine to produce thrust. The energy required can either come from the propellants
Rocket_propellant
Rocket with a motor that uses solid propellants
A solid-propellant rocket or solid rocket is a rocket with a rocket engine that uses solid propellants (fuel/oxidizer). The earliest rockets were solid-fuel
Solid-propellant_rocket
Liquid-fueled rocket engine
Rutherford is a liquid-propellant rocket engine designed by aerospace company Rocket Lab and manufactured in Long Beach, California. The engine is used
Rutherford_(rocket_engine)
Rocket engine
Curie is a liquid-propellant rocket engine designed and manufactured by Rocket Lab. A bipropellant is used for the propulsion of the third stage/kick
Curie_(rocket_engine)
Rocket engine that uses both liquid / gaseous and solid fuel
hybrid-propellant rocket is a rocket with a rocket motor that uses rocket propellants in two different phases: one solid and the other either gas or liquid.
Hybrid-propellant_rocket
Non-airbreathing engine used to propel a missile or vehicle
rockets or motors) are chemical rockets which use a mix of fuel and oxidizer in a solid state. Liquid-propellant rockets use one or more propellants in
Rocket_engine
Vehicle propelled by ejection of gases
(hypergolic propellants), two liquids that must be ignited to react (like kerosene (RP1) and liquid oxygen, used in most liquid-propellant rockets), a solid
Rocket
Type of rocket engine which uses liquid fuel stored at very low temperatures
Since one or more of the propellants is in the liquid phase, all cryogenic rocket engines are by definition liquid-propellant rocket engines. Various cryogenic
Cryogenic_rocket_engine
Rocket that uses a single propellant with a catalyst
monopropellant rocket (or "monochemical rocket") is a rocket that uses a single chemical as its propellant.[contradictory] Monopropellant rockets are commonly
Monopropellant_rocket
Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially
tripropellant rocket is a rocket that uses three propellants, as opposed to the more common bipropellant rocket or monopropellant rocket designs, which
Tripropellant_rocket
Solid propellant motor used to augment the thrust of a rocket
weighed approximately 500,000 kilograms. Compared to liquid propellant rockets, the solid-propellant motors (SRMs) have been capable of providing large
Solid_rocket_booster
Nuclear spacecraft propulsion technology
rocket (NTR) is a type of thermal rocket where the heat from a nuclear reaction replaces the chemical energy of the propellants in a chemical rocket.
Nuclear_thermal_rocket
Liquid fuel rocket engine
Archimedes is a liquid-fuel rocket engine burning liquid oxygen and liquid methane in an oxidizer-rich staged combustion cycle. It is designed by aerospace
Archimedes_(rocket_engine)
Highly refined form of kerosene used as rocket fuel
(Rocket Propellant-1 or Refined Petroleum-1) and similar fuels like RG-1 and T-1 are highly refined kerosene formulations used as rocket fuel. Liquid-fueled
RP-1
Unguided anti-aircraft rocket
mounted on an adapted 88 mm gun mounting. The rocket was driven by a liquid fueled engine. The liquid propellant used was a hypergolic mixture consisting of
Taifun_(rocket)
Chemical substance used for propulsion
storage, most propellants are stored as either a solid or a liquid. A rocket propellant is a mass that is expelled from a vehicle, such as a rocket, in such
Propellant
Proposed rocket propulsion mechanism
salt-water rocket (NSWR) is a theoretical type of nuclear thermal rocket designed by Robert Zubrin. In place of traditional chemical propellant, such as
Nuclear_salt-water_rocket
Rocket engine operation method
closed cycle) is a power cycle of a bipropellant rocket engine. In the staged combustion cycle, propellant flows through multiple combustion chambers, and
Staged_combustion_cycle
Type of nuclear propulsion method with an ultra high specific-inpulse
The fission-fragment rocket is a rocket engine design that directly harnesses hot nuclear fission products for thrust, as opposed to using a separate fluid
Fission-fragment_rocket
Russian rocket engine manufacturer
company designed a wide range of high technology products, including liquid propellant rocket engines, a nuclear reactor for space use, the first Soviet laser
Chemical Automatics Design Bureau
Chemical_Automatics_Design_Bureau
First South Korean orbital launch vehicle developed domestically
became the seventh country in the world to have a medium-sized liquid-propellant rocket engine over 75 tons. Nuri (KSLV-II) is a three-stage launch vehicle
Nuri_(rocket)
European rocket engine for upper stages
Vinci is a restartable, cryogenic, liquid-propellant rocket engine that powers the upper stage of Ariane 6. While development began in 1998 for the planned
Vinci_(rocket_engine)
Argentine proposed expendable launch system
is a series of Argentine rockets, including the Tronador I and Tronador II vehicles, to develop a liquid-propellant rocket expendable launch system called
Tronador_(rocket)
Solid propellant rocket used by the Space Shuttle
thrust, roughly double the most powerful single-combustion chamber liquid-propellant rocket engine ever flown, the Rocketdyne F-1. With a combined mass of
Space Shuttle Solid Rocket Booster
Space_Shuttle_Solid_Rocket_Booster
Family of rocket stages which can be used as a space tug
Centaur was the first rocket stage to use hydrolox propellant—liquid hydrogen (LH2) and liquid oxygen (LOX)—a high-energy combination well suited for
Centaur_(rocket_stage)
Peruvian engineer
rocket experts described him as a pioneer in aeronautics based on Paulet's retrospective statements detailing his construction of a liquid-propellant
Pedro_Paulet
Rocket designed to take measurements during its flight
interim step, they developed a liquid-propellant rocket to meet the Signal Corps' requirements for a sounding rocket, capable of carrying 11 kilograms
Sounding_rocket
First rockets
Raumschiffahrt (Society for Space Travel, or VfR), and in 1931 launched a liquid propellant rocket (using oxygen and gasoline). Similar work was done from 1932 onwards
History_of_rockets
Theoretical spacecraft propulsion system
propulsion do. The rocket would only have to carry the means of capturing solar energy, such as concentrators and mirrors. The heated propellant would be fed
Solar_thermal_rocket
Indian rocket engine
History of Liquid Propellant Rocket Engines. AIAA. p. 799. ISBN 9781563476495. Sutton, George Paul (2006). History of Liquid Propellant Rocket Engines.
Vikas_(rocket_engine)
Early Soviet rocket laboratory
Tikhonravov worked on developing oxygen/alcohol liquid-propellant rocket engines. Ultimately liquid propellant rocket engines were given a low priority during
Reactive Scientific Research Institute
Reactive_Scientific_Research_Institute
Type of spacecraft propulsion system
A nuclear electric rocket (more properly nuclear electric propulsion) is a type of spacecraft propulsion system where thermal energy from a nuclear reactor
Nuclear_electric_rocket
Type of rocket engine
of the propellant.[citation needed] Cold gas systems can use either a solid, liquid or gaseous propellant storage system; but the propellant must exit
Cold_gas_thruster
Rocket engine used on the Saturn V rocket
program. The F-1 remains the most powerful single combustion chamber liquid-propellant rocket engine ever developed. Rocketdyne developed the F-1 and the E-1
Rocketdyne_F-1
Rocket used to trigger lightning
conductive path when the exhaust gases are discharged from the rocket. In a liquid propellant rocket a solution of calcium chloride is used to form the conductive
Lightning_rocket
Solid-rocket propellant
perchlorate composite propellant (APCP) is a solid rocket propellant. It differs from many traditional solid rocket propellants such as black powder or
Ammonium perchlorate composite propellant
Ammonium_perchlorate_composite_propellant
Philippine missile program
the weapon as the Philippines' first liquid-propellant rocket. The associated weaponry system of the Bongbong rocket is similar to the Soviet unguided artillery
Project_Santa_Barbara
Use of self-generated gaseous propellant
use of self-generated gaseous propellant to pressurize liquid propellant in rockets. Traditional liquid-propellant rockets have been most often pressurized
Autogenous_pressurization
German long-range ballistic missile
missile and suborbital launch vehicle. The missile, powered by a liquid-propellant rocket engine, was developed during the Second World War in Nazi Germany
V-2_rocket
1902 Peruvian rocket aircraft project
Pedro Paulet developed a liquid-propellant rocket engine in 1895. In 1902, he designed the Avión Torpedo, a liquid-propellant rocket-powered aircraft that
Avión_Torpedo
Rocket engine
The XLR11, company designation RMI 6000C4, was the first liquid-propellant rocket engine developed in the United States for use in aircraft. It was designed
Reaction_Motors_XLR11
Aircraft which uses a rocket engine for propulsion
using liquid-propellant was decades ahead of rocket engineers at the time who utilized black powder as a propellant. Reports of Paulet's rocket aircraft
Rocket-powered_aircraft
Class of rocket
(XLR52-AJ-2) liquid-fueled engine, a variant of the engine in the RTV-N-10 Aerobee. Finally, the third stage was a solid-propellant rocket motor. All three-stage
Vanguard_(rocket)
{\displaystyle x=0} respectively. Boltzmann equation Spray (liquid drop) Liquid-propellant rocket Smoluchowski coagulation equation Williams, F. A. (1958)
Williams_spray_equation
Rocket engine operation method
Pressure-fed engine Rocket engine Solid-propellant rocket Staged combustion cycle George Paul Sutton (2006). History of Liquid Propellant Rocket Engines. AIAA
Electric-pump-fed_engine
Rocket engine
Motors LR99 engine was the first large, throttleable, restartable liquid-propellant rocket engine. Development began in the 1950s by the Reaction Motors Division
Reaction_Motors_XLR99
Rocket driven by nuclear fusion power
ion rocket thrusters (343 km/s exhaust velocity) powered by ten D-He3 IEC fusion reactors. The concept would need 300 tonnes of argon propellant for a
Fusion_rocket
Passing cold propellant through tubes around a rocket engine to cool it
In rocket engine design, regenerative cooling is a configuration in which some or all of the propellant is passed through tubes, channels, or in a jacket
Regenerative cooling (rocketry)
Regenerative_cooling_(rocketry)
Throttleable Liquid Propulsion Demonstrator (TLPD) is a prototype liquid-propellant rocket engine under development by the Polish Lukasiewicz Research
Throttleable Liquid Propulsion Demonstrator
Throttleable_Liquid_Propulsion_Demonstrator
A rocket turbine engine is a combination of two types of propulsion engines: a liquid-propellant rocket and a turbine jet engine. Its power-to-weight
Rocket_turbine_engine
Proposed hybrid ramjet and rocket engine
nozzle Avatar (spacecraft) – India's air-breathing spaceplane Liquid-propellant rocket Precooled jet engine "Reaction Engines Limited Engine Names" (PDF)
SABRE_(rocket_engine)
American rocket engine family used on Titan missile first stages
The LR87 is an American liquid-propellant rocket engine that was used on the first stages of Titan intercontinental ballistic missiles and launch vehicles
Aerojet_LR87
Spacecraft propulsion device
a solid propellant RF resonant cavity thruster, an electromagnetic thruster using microwaves Liquid apogee engine – A liquid-propellant rocket used as
Thrusters_(spacecraft)
Nazi ballistic missile series
designed by Arthur Rudolph, used a pressure-fed rocket propellant system burning ethanol and liquid oxygen, and produced 2.9 kN (660 lbf) of thrust for
Aggregat
Type of vibration in a rocket engine
Pogo oscillation is a self-excited type of vibration in liquid-propellant rocket engines caused by combustion instability. The unstable combustion results
Pogo_oscillation
Method of spacecraft propulsion
magnitude lower than those of more conventional solid fuel and liquid-propellant rockets. As a result, they are unsuitable for orbital maneuvers that require
Resistojet_rocket
Serbian defense company
Development and Production) is a Serbian company which develops solid rockets, turbojet powered missiles, and the production of energetic materials.
EDePro
Rocket engine
TM65 is a rocket engine developed by Copenhagen Suborbitals. TM65 uses Ethanol and liquid oxygen as propellants in a pressure-fed power cycle. Construction
TM65
Aerospace Science and Technology Corporation. The institute develops liquid-propellant rocket engines and guidance systems for China's space launchers. It employs
Academy of Aerospace Liquid Propulsion Technology
Academy_of_Aerospace_Liquid_Propulsion_Technology
Rocket engines developed by SpaceX
led by engineer Tom Mueller, the company developed a variety of liquid-propellant rocket engines, with at least one more of that type under development
SpaceX_rocket_engines
One of the physical forms of elemental oxygen
the oxidizer in the first liquid-fueled rocket invented in 1926 by Robert H. Goddard, an application which is ongoing. Liquid oxygen has a clear, pale
Liquid_oxygen
Form of electric spacecraft propulsion
amount of reaction mass or propellant required, but increases the amount of specific power required compared to chemical rockets. Ion thrusters are therefore
Ion_thruster
American physicist and inventor (1882–1945)
and engineer credited with creating and building the world's first liquid-fueled rocket, which was successfully launched on March 16, 1926. By 1915 his pioneering
Robert_H._Goddard
Russian and Soviet rocket family
commercial purposes. All Soyuz variants use RP-1 (kerosene) and liquid oxygen (LOX) as propellants, with the exception of the Soyuz-U2, which used Syntin (a
Soyuz_(rocket_family)
Engines used in EU rocket Ariane
designer of Viking and A4 engine George Paul Sutton, "History of Liquid Propellant Rocket Engines", p. 798 News Archive 2009 Viking engine (Archived) Souchier
Viking_(rocket_engine)
Family of American missiles and space launch vehicles
through its Convair division. Atlas was a liquid propellant rocket burning RP-1 kerosene fuel with liquid oxygen in three engines configured in an unusual
Atlas_(rocket_family)
Electrothermal thruster in development
electrodeless plasma thruster, the microwave arcjet rocket, and the pulsed inductive thruster. The propellant, a neutral gas such as argon or xenon, is injected
Variable Specific Impulse Magnetoplasma Rocket
Variable_Specific_Impulse_Magnetoplasma_Rocket
Soviet rocket laboratory 1921 to 1933
missiles in the Katyusha rocket launcher, as well as liquid propellant rockets, which became the prototypes of Soviet rockets and spacecraft. At the end
Gas_Dynamics_Laboratory
Type of propelling nozzle
(rocket) – a type of rocket engine Venturi effect Huzel, D. K. & Huang, D. H. (1971). NASA SP-125, Design of Liquid Propellant Rocket Engines (PDF) (2nd ed
Rocket_engine_nozzle
Type of liquid-propellant rocket engine
The SEPR 84 is a family of liquid-propellant rocket engines used as boosters for the Dassault Mirage III mixed-power high-altitude interceptor aircraft
SEPR_84
Rocket fuel combination
Devil's venom was a nickname coined by Soviet rocket scientists for a hypergolic liquid rocket fuel composed of a dangerous combination of red fuming nitric
Devil's_venom
Municipality in Mecklenburg-Vorpommern, Germany
Research Center, where the world's first functional large-scale liquid-propellant rocket, the V-2, was developed. The village with its seaport is located
Peenemünde
SpaceX family of liquid-fuel rocket engines
is powered by cryogenic liquid methane and liquid oxygen, a combination known as methalox. SpaceX's super-heavy-lift rocket Starship uses Raptor engines
SpaceX_Raptor
Single-stage ballistic missile
alternately Al-Samed, which means steadfastness in Arabic) was a liquid-propellant rocket tactical ballistic missile developed by Iraq in the years between
Al-Samoud_2
American gas-generator rocket engine used on Titan upper stages
The LR91 was an American liquid-propellant rocket engine, which was used on the second stages of Titan intercontinental ballistic missiles and launch vehicles
LR91
Chinese rocket engine
The YF-75 is a liquid cryogenic rocket engine burning liquid hydrogen and liquid oxygen in a gas generator cycle. It is China's second generation of cryogenic
YF-75
Class of liquid rocket propellants
Nitrous oxide fuel blend propellants are a class of liquid rocket propellants that were intended in the early 2010s to be able to replace hydrazine as
Nitrous_oxide_fuel_blend
Chinese rocket engine
"Asian space-rocket liquid-propellant engines". B14643.DE. Archived from the original on 2015-07-17. Retrieved 2015-07-15. "Long March". Rocket and Space
YF-23_(rocket_engine)
State of matter
include water or liquid metals, such as sodium or bismuth. Liquid propellant films are used to cool the thrust chambers of rockets. In machining, water
Liquid
American kerolox rocket engine
The Rocketdyne H-1 was a 205,000 lbf (910 kN) thrust liquid-propellant rocket engine burning LOX and RP-1. The H-1 was developed for use in the S-I and
Rocketdyne_H-1
Most common type of rocket, used to launch satellites
multistage rocket or step rocket is a launch vehicle that uses two or more rocket stages, each of which contains its own engines and propellant. A tandem
Multistage_rocket
Hypersonic research plane
intended to be an autonomous pilotless craft powered by a "Fastrac" liquid-propellant rocket engine, capable of reaching Mach 8 and performing 25 test flights
Orbital_Sciences_X-34
vapor pressure of the pumped liquid. Inducers are virtually always included in the turbopumps for liquid propellant rocket engines, although they are also
Inducer_(pump_component)
Type of nuclear thermal rocket
typical residence time is on seconds, however, in rockets chambers with subsonic velocities of the propellant around hundreds of meters per second, residence
Pulsed_nuclear_thermal_rocket
Space station made from a spent rocket stage
space station made from a spent liquid-propellant rocket stage. Such a rocket stage contains two large, airtight propellant tanks; it was realized that the
Wet_workshop
Conceptual rocket engine
Direct Fusion Drive (DFD) is a conceptual, low radioactivity, nuclear-fusion rocket engine, designed to produce both thrust and electric power, suitable for
Direct_Fusion_Drive
Type of spacecraft maneuver
Oberth maneuver is much more useful for high-thrust rocket engines such as liquid-propellant rockets, and less useful for low-thrust reaction engines such
Oberth_effect
Model of Titan III launch vehicle
LR-87 liquid propellant rocket, while the second stage consisted of an LR91 liquid propellant rocket. The third stage was an Agena D XLR81-BA-9 liquid propellant
Titan_IIIB
American expendable launch system
1 on April 8, 1964. The Titan II was a two-stage liquid-fuel rocket, using a hypergolic propellant combination of Aerozine 50 fuel and nitrogen tetroxide
Titan_II_GLV
Early Soviet rocket research bureau
study various aspects of rocketry. GIRD launched the first Soviet liquid propellant rocket in August 1933. In November 1933 it was incorporated into the Reactive
Group for the Study of Reactive Motion
Group_for_the_Study_of_Reactive_Motion
Rocket engine operation method
pressure-fed engine is a class of rocket engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and oxidizer
Pressure-fed_engine
Launch system that only uses one rocket stage
(SSTO) vehicle reaches orbit from the surface of a body using only propellants and fluids and without expending tanks, engines, or other major hardware
Single-stage-to-orbit
American rocket family
from orbit. Ablestar was a liquid-propellant rocket stage burning hypergolic propellants fed from gas-pressurized propellant tanks. It was used as the
Thor_(rocket_family)
was redirected to work on liquid propellant rocket engines. This resulted in the creation of ORM (from "Experimental Rocket Motor" in Russian) engines
Soviet_rocketry
Type of spacecraft electric propulsion system
monopropellant rockets. Aerojet MR-510 series arcjet engines are currently used on Lockheed Martin A2100 satellites using hydrazine as a propellant, providing
Arcjet_rocket
American short-range ballistic missile
Retrieved 9 October 2010. Sutton, George P. (2006). History of Liquid Propellant Rocket Engines. Reston, Virginia: American Institute of Aeronautics and
PGM-11_Redstone
Rocket-propelled by exhausted coolant of a gas-cooled nuclear reactor
temperatures to the propellant. Solid core nuclear thermal rockets can develop higher specific impulse than conventional chemical rockets due to the low molecular
Gas_core_reactor_rocket
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