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A liquid nitrogen engine is powered by liquid nitrogen, which is stored in a tank. Traditional nitrogen engine designs work by heating the liquid nitrogen
Liquid_nitrogen_engine
Liquid state of nitrogen
Liquid nitrogen (LN2) is nitrogen in a liquid state at low temperature. It has a boiling point of about −196 °C (−321 °F; 77 K). Liquid nitrogen is produced
Liquid_nitrogen
Chemical compound
Ammonia is an inorganic chemical compound of nitrogen and hydrogen with the formula NH3. A stable binary hydride and the simplest pnictogen hydride, ammonia
Ammonia
One of the physical forms of elemental oxygen
Commons has media related to Liquid oxygen. Oxygen storage Industrial gas Cryogenics Liquid hydrogen Liquid helium Liquid nitrogen List of stoffs Natterer
Liquid_oxygen
Vehicle with hydrogen internal combustion engine
occur in engine exhaust. However, hydrogen combustion occurs in an atmosphere containing nitrogen and oxygen, which can produce oxides of nitrogen (NOx)
Hydrogen internal combustion engine vehicle
Hydrogen_internal_combustion_engine_vehicle
Concept of hybrid atmospheric jet engine
atmosphere. A liquid air cycle engine uses liquid hydrogen (LH2) fuel to liquefy the air. In a liquid oxygen/liquid hydrogen rocket, the liquid oxygen (LOX)
Liquid_air_cycle_engine
Air that has been condensed into a liquid
percentage of the components and their respective liquid densities (see liquid nitrogen and liquid oxygen). Although air contains trace amounts of carbon
Liquid_air
A liquid apogee engine (LAE), or apogee engine, refers to a type of chemical rocket engine typically used as the main engine in a spacecraft. The name
Liquid_apogee_engine
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
Hygroelectricity Implosion Kaplan turbine Light crude oil Liquid fuel Liquid nitrogen engine Marine current power Magnetohydrodynamic, generator, MHD generator
List_of_energy_resources
Liquid form of rocket propellants
been flown. Many factors go into choosing a propellant for a liquid-propellant rocket engine. The primary factors include ease of operation, cost, hazards/environment
Liquid_rocket_propellant
Automotive supplement
oxygen and nitrogen gas is exothermic and thus contributes to a higher temperature in the combustion engine, the decomposition increases engine efficiency
Nitrous_oxide_engine
Liquid state of the element hydrogen
jet engine in both appearance and principle. Liquid hydrogen is typically used as a concentrated form of hydrogen storage. Storing it as liquid takes
Liquid_hydrogen
Non-airbreathing engine used to propel a missile or vehicle
test engine was built in Germany in 1963, by Ludwig Boelkow. Liquid hydrogen engines were first successfully developed in America: the RL10 engine first
Rocket_engine
Overview of and topical guide to automobiles
Ignition Liquid Nitrogen Engine configuration (IC engines only) Flat engine Flathead engine Four-stroke engine H engine Pushrod engine Reciprocating engine Single-cylinder
Outline_of_automobiles
Chemical compound
periodically introduced vaporized nitrogen tetroxide and a petroleum benzine to a spark plug for ignition, with the engine putting out 300 pulsating explosions
Dinitrogen_tetroxide
Indian rocket engine
The Vikas engine (a portmanteau from initials of VIKram Ambalal Sarabhai ) is a family of hypergolic liquid fuelled rocket engines conceptualized and designed
Vikas_(rocket_engine)
System that converts heat or thermal energy to mechanical work
gas or liquid. During this process, some heat is normally lost to the surroundings and is not converted to work. Also, in a mechanical engine, some energy
Heat_engine
Topics referred to by the same term
of a conventional liquid and those of a solid crystal Liquid layout, a web design that does not rely upon fixed widths Liquid nitrogen vehicle, a vehicle
Liquid_(disambiguation)
American rocket engine family used on Titan missile first stages
rocket engine capable (in its various models) of burning the three most-common liquid rocket propellant combinations: liquid oxygen/RP-1, nitrogen tetroxide
Aerojet_LR87
Compound containing nitrogen and oxygen
pollutants. Nitrogen dioxide is a reddish-brown gas with a pungent, acrid odor above 21.2 °C (70.2 °F; 294.3 K) and becomes a yellowish-brown liquid below 21
Nitrogen_dioxide
Term for nitric oxide and nitrogen dioxide
between nitrogen and oxygen during combustion of fuels, such as hydrocarbons, in air; especially at high temperatures, such as in car engines. In areas
NOx
Use of low temperature liquids to store energy
storage (CES) is the use of low temperature (cryogenic) liquids such as liquid air or liquid nitrogen to store energy. The technology is primarily used for
Cryogenic_energy_storage
State of matter
can be liquefied by cooling, producing liquids such as liquid oxygen, liquid nitrogen, liquid hydrogen and liquid helium. However, not all gases can be
Liquid
Highly refined form of kerosene used as rocket fuel
rocket fuel. Liquid-fueled rockets that use RP-1 as fuel are known as kerolox rockets. In their engines, RP-1 is atomized, mixed with liquid oxygen (LOX)
RP-1
Respiration of oxygen-rich liquid by a normally air-breathing organism
Liquid breathing would not result in the saturation of body tissues with high pressure nitrogen or helium that occurs with the use of non-liquids, thus
Liquid_breathing
Type of rocket engine fuel
oxidizer, nitrogen tetroxide, are all liquid at ordinary temperatures and pressures. They are therefore sometimes called "storable liquid propellants"
Hypergolic_propellant
Inline engine with four banks driving two crankshafts
An H engine is a piston engine comprising two separate flat engines (complete with separate crankshafts), most often geared to a common output shaft. The
H_engine
Substance used to reduce or regulate the temperature of a system
solid and liquid. Liquid gases may fall here, or into refrigerants, as their temperature is often maintained by evaporation. Liquid nitrogen is the best
Coolant
US ethanol-oxygen rocket engine
The RS-88 (Rocket System-88) is a liquid-fueled rocket engine designed and built in the United States by Rocketdyne (later Pratt & Whitney Rocketdyne
RS-88
Engine in which fuel combusts with an oxidizer
Street patented an internal combustion engine, which was also the first to use liquid fuel, and built an engine around that time. In 1798, John Stevens
Internal_combustion_engine
Type of rocket engine
cold gas thruster allows its usage in situations where regular liquid rocket engines would be too hot. This eliminates the need to engineer heat management
Cold_gas_thruster
Rocket engine
Aestus is a hypergolic liquid rocket engine used on an upper stage of Ariane 5 family rockets for the orbital insertion. It features unique design of 132
Aestus
Chemical which reduces air pollution from diesel engines
and sometimes marketed as AdBlue) is a liquid used to reduce the amount of air pollution created by a diesel engine. Specifically, DEF is an aqueous urea
Diesel_exhaust_fluid
1940s German aircraft rocket engine
The Walter HWK 109-509 was a German liquid-fuel bipropellant rocket engine that powered the Messerschmitt Me 163 Komet and Bachem Ba 349 aircraft. It was
Walter_HWK_109-509
Linear Aerospike SR-71 Experiment 1997/8 NASA for X-33
cycle gaseous helium and liquid nitrogen through the experiment to check its plumbing system for leaks and to check engine operation characteristics
Linear Aerospike SR-71 Experiment
Linear_Aerospike_SR-71_Experiment
Series of gas turbine engines developed by Chrysler
fifth-generation turbine engine. However, Chrysler went on to develop a sixth generation gas-turbine engine which finally met US nitrogen oxide regulations,
Chrysler_turbine_engine
Rocket engine that uses both liquid / gaseous and solid fuel
matter), hybrid rockets tend to fail more benignly than liquids or solids. Like liquid rocket engines, hybrid rocket motors can be shut down easily and the
Hybrid-propellant_rocket
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
Gas law regarding proportionality of dissolved gas
Timothy R.; Tominaga, Toshihiro (1984). "The Solubility of Nitrogen and Air in Liquids". Journal of Physical and Chemical Reference Data. 13 (2): 563–600
Henry's_law
Type of hardening with nitrogen and carbon using a salt bath
the nomenclature jungle of nitrogen diffusion". Pye 2003, pp. 196–197. Pye 2003, pp. 201–202. Easterday, James R. "Liquid Ferritic Nitrocarburizing" (PDF)
Ferritic_nitrocarburizing
Chemical or mixture used in a rocket engine
the liquid propellant mass is converted into a huge volume of gas at high temperature and pressure. This exhaust stream is ejected from the engine nozzle
Rocket_propellant
Turbomachinery concept
turbojet (PCTJ) and hypersonic turbojet studies. A liquid nitrogen precooled hydrogen burning test engine was flown at Mach 2 at Taiki Aerospace Research
Precooled_jet_engine
Captured energy for later usage
Brick storage heater Cryogenic energy storage, liquid-air energy storage (LAES) Liquid nitrogen engine Eutectic system Ice storage air conditioning Molten
Energy_storage
Machine that converts one or more forms of energy into mechanical energy (of motion)
combination with air (all airbreathing engines), a side reaction between atmospheric oxygen and atmospheric nitrogen produces small amounts of NOx. If a
Engine
Chemical process
liquefies to form a liquid that is enriched in oxygen. The remaining gas is richer in nitrogen and is distilled to almost pure nitrogen (typically < 1ppm)
Air_separation
Aircraft engine family
The Rolls-Royce Merlin is a British liquid-cooled V12 piston aero engine of 27-litre (1,650 cu in) capacity. Developed as a private venture by Rolls-Royce
Rolls-Royce_Merlin
Rocket-powered aircraft and spaceplane operated by the US Air Force and NASA
fueled a turbopump for the main engines and auxiliary power units (APUs). Additional tanks for helium and liquid nitrogen performed other functions; the
North_American_X-15
Device that burns fuel to produce large volumes of relatively cool gas
mixtures of nitrogen, hydrogen and ammonia. The reaction is strongly exothermic and produces high volume of hot gas from small volume of liquid. 3 N 2 H
Gas_generator
Dual fuel engine
regulations. The natural gas is stored in liquid state (LNG) and the boil-off gas is routed to and burned in dual fuel engines. Shipping companies have been cautious
Marine_LNG_Engine
Proposed spaceflight launch system
second stage would use liquid oxygen (LOX) and liquid hydrogen (LH2) and be powered by the Raptor engine. Multiple variants were planned with payloads
Falcon_X
Hypergolic rocket engine manufactured by Aerojet
critical usage of this engine during the Apollo program. This version used Aerozine 50 (a 1:1 mix of UDMH and hydrazine) as fuel and nitrogen tetroxide (N2O4)
AJ10
Fluid used as an intermediary in a cooling or heating process
decompose. Gases such as water vapor, nitrogen, argon, helium and hydrogen have been used as heat transfer fluids where liquids are not suitable. For gases the
Heat-transfer_fluid
United States historic place
Research Center, in Ohio. The purpose of the Rocket Engine Test Facility was to test full-scale liquid hydrogen rockets at thrust chamber pressures of up
Rocket_Engine_Test_Facility
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
LR91
Colorless flammable liquid with an ammonia-like odor
formula N2H4. It is a simple pnictogen hydride, and is a colourless flammable liquid with an ammonia-like odour. Hydrazine is highly hazardous unless handled
Hydrazine
Peruvian engineer
Paulet's retrospective statements detailing his construction of a liquid-propellant rocket engine and a modern rocket propulsion system in the 1890s, though
Pedro_Paulet
Type of internal combustion engine
higher engine temperature; this impacts on power and emissions, notably increasing nitrogen oxides or NOx. In simple terms a stratified charge engine creates
Stratified_charge_engine
Ratio of kinematic viscosity to thermal diffusivity
dependence): Pr = 2/3 nitrogen and oxygen at temperatures below 1000 K: Pr varies between 0.71 and 0.76 air, which is primarily nitrogen and oxygen (250 to
Prandtl_number
Use of self-generated gaseous propellant
the liquid propellant tank it was sourced from. This helps keep the liquid propellant at the required pressure necessary to feed a rocket's engines. This
Autogenous_pressurization
Physical phenomenon
applies when the surface is at room temperature but the liquid is cryogenic, allowing liquid nitrogen droplets to harmlessly roll off exposed skin. Conversely
Leidenfrost_effect
Colourless non-flammable greenhouse gas
laughing gas or nitrous, among others, is a chemical compound, an oxide of nitrogen with the formula N2O. At room temperature, it is a colourless non-flammable
Nitrous_oxide
Line of hypergolic liquid rocket engines by SpaceX
SpaceX Draco is a hypergolic liquid rocket engine designed and built by SpaceX for use in their space capsules. Two engine types have been built to date:
SpaceX_Draco
Type of internal combustion engine that uses compression to create combustion
compression; thus, the diesel engine is also called a compression-ignition engine (or CI engine). This contrasts with engines using spark plug-ignition of
Diesel_engine
Rocket engines developed by SpaceX
Starships. Draco are hypergolic liquid-propellant rocket engines that utilize a mixture of monomethyl hydrazine fuel and nitrogen tetroxide oxidizer. Each Draco
SpaceX_rocket_engines
Combustion engine using an eccentric rotary design
nitrogen oxide (NOx) emissions, because combustion is slow and temperatures are lower than in other engines, and also because of the Wankel engine's good
Wankel_engine
Turkish liquid-fueled intercontinental ballistic missile
solid propellants, the Yıldırımhan utilizes a liquid-fuel propulsion system. The missile uses nitrogen tetroxide (N₂O₄) as an oxidizer, which implies
Yıldırımhan
Type of airplane
require new aircraft designs. Liquid hydrogen is one of the best coolants used in engineering, and precooled jet engines have been proposed to use this
Hydrogen-powered_aircraft
American rocket engine
Ascent Engine (LMAE), modified to burn liquid oxygen (LOX) and liquid methane (CH4) for NASA's Exploration Systems Architecture Study (ESAS) engine testing
RS-18
Form of fastening
shrink-fitting include compression shrink fitting, which uses a cryogen such as liquid nitrogen to cool the insert, and shape memory coupling, which is achieved by
Shrink-fitting
Expendable launch system used by the US Air Force
two LR87 liquid propellant engines. Stage 2 uses one LR91 liquid propellant engine. Stage 3 uses two Aerojet AJ-10-138 liquid propellant engines. Length:
Titan_IIIC
Chemical reaction between a fuel and oxygen
components. This problem was solved by re-designing the fuel injector. In liquid jet engines, the droplet size and distribution can be used to attenuate the instabilities
Combustion
Process of removing waste heat from a computer
harm the user, causing frostbite. Liquid helium, colder than liquid nitrogen, has also been used for cooling. Liquid helium boils at −269 °C (−452.20 °F)
Computer_cooling
Type of rocket pack
MPa). The pilot turns the engine thrust control handle, opening the regulator valve (3). Compressed nitrogen (1) displaces liquid hydrogen peroxide (2),
Bell_Rocket_Belt
Pump driven by a gas turbine
dramatically raise the pressure of liquid propellants and feed them to the combustion chamber of a rocket engine. While they have considerably higher
Turbopump
Mass ratio of air to a fuel
cause higher temperatures, which can lead to the formation of nitrogen oxides. Some engines are designed with features to allow lean-burn. For precise air–fuel
Air–fuel_ratio
Atmospheric effects used in the entertainment industry
accordingly. Nitrogen itself is relatively non-toxic, but in high concentrations it can displace oxygen, creating a suffocation hazard. Liquid nitrogen (−195
Theatrical_smoke_and_fog
1930s British piston aircraft engine
is a British 37-litre (2,240 cu in) capacity, 60-degree V12, liquid-cooled aero engine designed and built by Rolls-Royce Limited. In keeping with company
Rolls-Royce_Griffon
Type of injection fertilization
surface of fields in either a liquid or powder form by spraying it. Although CULTAN fertilization is only done for nitrogen application, injection irrigation
CULTAN_Fertilization
Soviet experimental aircraft
Kuznetsov NK-8 engines (they are now called NK-88) was actually powered by hydrogen. The fuel tank was located in the air-blown (or nitrogen) rear compartment
Tupolev_Tu-155
Automobile layout
A front-engine, rear-wheel-drive layout (FR), also called Système Panhard is a powertrain layout with an engine in front and rear-wheel-drive, connected
Front-engine, rear-wheel-drive layout
Front-engine,_rear-wheel-drive_layout
Aircraft engine that produces thrust by emitting a jet of gas
the engine, and this greatly heats the air. The upper limit is usually thought to be about Mach 5–8, as above about Mach 5.5, the atmospheric nitrogen tends
Jet_engine
Internal combustion engine with two banks of cylinders at an angle resembling a 'V'
A V engine, sometimes called a Vee engine, is a common configuration for internal combustion engines. It consists of two cylinder banks—usually with the
V_engine
Fuel for heating, cooking and vehicles
Liquefied petroleum gas, also referred to as liquid petroleum gas (LPG or LP gas), is a fuel gas which contains a flammable mixture of hydrocarbon gases
Liquefied_petroleum_gas
Fuels which require storage at very low temperatures to remain liquid
liquid air vehicle. Some common inert fuels include: Liquid nitrogen Liquid air Liquid helium Liquid neon These fuels utilize the beneficial liquid cryogenic
Cryogenic_fuel
Indian expendable medium-lift launch vehicle, developed by ISRO
unsymmetrical dimethylhydrazine (UDMH) and nitrogen tetroxide (N2O4). It is powered by two Vikas 2 engines, each generating 766 kilonewtons (172,000 lbf)
LVM3
Rocket engine test facility
gallons on stand Gas capability: hydrogen, nitrogen, helium, air RP-1 storage: 150,000 gallons (shared with F-1 engine test stand) Water deflector capacity:
Test_Stand_4670
First stage of the Saturn V rocket
liquid oxygen tank as well as a portion of the five liquid oxygen feed lines for the engines. The liquid oxygen (LOX) tank held 334,500 US gallons (1,266 m3;
S-IC
Cylinder layout for a piston engine
Straight / Inline engine A straight engine, or inline engine, is a configuration of multi-cylinder piston engine where all of the cylinders are arranged
Straight_engine
Mixture formation system
direct injection (PDI), is a fuel injection system for internal combustion engines that run on gasoline. It injects fuel directly into the combustion chamber
Gasoline_direct_injection
Satellite bus
was later increased to 2.55 m. The liquid apogee engine uses hydrazine fuel from the central tank along with nitrogen tetroxide oxidizer from two flanking
Lockheed_Martin_A2100
Rocket-powered land speed racing vehicle
and driven by Chuck Suba. Blue Flame's engine is a regeneratively cooled variable-thrust liquid-propellant engine, using a combination of high-test peroxide
Blue_Flame
NASA rocket engine testing facility in Mississippi
provide Liquid Hydrogen (LH2) and liquid oxygen (LOX) in addition to support fluids, gaseous helium (GHe), gaseous hydrogen (GH2) and gaseous nitrogen (GN2)
Stennis_Space_Center
Organic compound
important role in the cellular metabolism of nitrogen-containing compounds by animals and is the main nitrogen-containing substance in the urine of mammals
Urea
Car that uses pneumatic motors
compressed air is low compared to liquid nitrogen or hydrogen, and the energy efficiency of compressed air engine compared to a micro gas turbine with
Compressed-air_vehicle
Liquefied petroleum gas when it is used as a fuel in internal combustion engines
straight-six engine of a 2001 Ford Falcon (AU) 3.6-litre Alloytec bi-fuel (petrol and LPG) V6 engine of a 2006–2008 Holden Commodore (VE) The World Liquid Gas
Autogas
Type of thermometer
introduction of an inert gas such as nitrogen. This introduction of an inert gas increases the pressure on the liquid mercury and therefore its boiling point
Mercury-in-glass_thermometer
Reusable first-stage rocket developed by SpaceX
tanks with liquid nitrogen, which is nonflammable, though liquid oxygen may be loaded as well. After returning to the production site, the engines are installed
SpaceX_Super_Heavy
Hypergolic orbital maneuvering engines used on NASA's Space Shuttle
Orbital Maneuvering System (OMS) is a system of hypergolic liquid-propellant rocket engines used on the Space Shuttle and the Orion spacecraft. Designed
Orbital_Maneuvering_System
Location where rocket engines may be tested on the ground, under controlled conditions
may be designed to restrain the rocket engine in either a horizontal or vertical position. Liquid rocket engines are usually fired in a vertical position
Rocket_engine_test_facility
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