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Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially
A tripropellant rocket is a rocket that uses three propellants, as opposed to the more common bipropellant rocket or monopropellant rocket designs, which
Tripropellant_rocket
Chemical or mixture used in a rocket engine
drag and reducing the effective delta-v requirement. The proposed tripropellant rocket uses mainly dense fuel while at low altitude and switches across
Rocket_propellant
Non-airbreathing engine used to propel a missile or vehicle
A rocket engine, also known as a rocket motor, is a reaction engine, producing thrust in accordance with Newton's third law by ejecting reaction mass
Rocket_engine
Rocket engine that uses liquid fuels and oxidizers
rockets can be monopropellant rockets using a single type of propellant, or bipropellant rockets using two types of propellant. Tripropellant rockets
Liquid-propellant_rocket
Vehicle propelled by ejection of gases
that can restart Steam rocket – Thermal rocket that uses superheated water held in a pressure vessel Tripropellant rocket – Rocket that burns 3 propellants
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
Rocket with a motor that uses solid propellants
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 rockets powered
Solid-propellant_rocket
Electrothermal thruster in development
The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an electrothermal thruster under development for possible use in spacecraft propulsion.
Variable Specific Impulse Magnetoplasma Rocket
Variable_Specific_Impulse_Magnetoplasma_Rocket
Method used to accelerate spacecraft
have simple reliable chemical thrusters (often monopropellant rockets) or resistojet rockets for orbital station-keeping, while a few use momentum wheels
Spacecraft_propulsion
Rocket driven by nuclear fusion power
A fusion rocket is a theoretical design for a rocket driven by fusion propulsion, which could provide efficient and sustained acceleration in space without
Fusion_rocket
Rocket engine that uses both liquid / gaseous and solid fuel
A 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
Hybrid-propellant_rocket
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
Type of rocket engine exhaust
extension Multistage rocket Tripropellant rocket Huzel, Dieter K.; Huang, David H. (1971). NASA SP-125, Design of Liquid Propellant Rocket Engines (2nd ed
Altitude_compensating_nozzle
List of definitions of terms and concepts commonly used in aerospace engineering
Trans Lunar Injection – Transonic – Transverse wave – Tripropellant rocket – Tsiolkovsky rocket equation – Turbomachinery – Two-stage-to-orbit – UFO –
Glossary of aerospace engineering
Glossary_of_aerospace_engineering
Type of rocket engine which uses liquid fuel stored at very low temperatures
A cryogenic rocket engine is a rocket engine that uses a cryogenic fuel and oxidizer; that is, both its fuel and oxidizer are gases which have been liquefied
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
Proposed Soviet rocket engine
cancelled shortly before the end of USSR. The RD-701 would have been a tripropellant engine that used a staged combustion cycle with afterburning of oxidizer-rich
RD-701
Launch system that only uses one rocket stage
VTVL tripropellant rockets, and showed that it could improve payload size by around 30%. Operational experience with the DC-X experimental rocket has caused
Single-stage-to-orbit
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 nozzle
Glushko has used an expanding nozzle on one design, the RD-701 tripropellant rocket. Funding ran out with the fall of the Soviet state, but the designers
Expanding_nozzle
Change in velocity per amount of fuel
a chemical propellant ever test-fired in a rocket engine was 542 seconds (5.32 km/s) with a tripropellant of lithium, fluorine, and hydrogen. However
Specific_impulse
Rocket engine operation method
is one of the most commonly used engine cycles in bipropellant liquid rocket engines. Propellant is burned in a gas generator (analogous to, but distinct
Gas-generator_cycle
— Transverse wave — Tripropellant rocket — Tsiolkovsky rocket equation — Turbomachinery — Two-stage-to-orbit — UFO UAV V-2 rocket — Variable specific
Index of aerospace engineering articles
Index_of_aerospace_engineering_articles
Form of electric spacecraft propulsion
spacecraft must rely on other methods such as conventional chemical rockets or non-rocket launch technologies to reach their initial orbit. Konstantin Tsiolkovsky
Ion_thruster
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 another
Hypergolic_propellant
Rocket engine operation method
cycle, preburner cycle, or closed cycle) is a power cycle of a bipropellant rocket engine. In the staged combustion cycle, propellant flows through multiple
Staged_combustion_cycle
A radioisotope rocket or radioisotope thermal rocket is a type of thermal rocket engine that uses the heat generated by the decay of radioactive elements
Radioisotope_rocket
Proposed spacecraft propulsion method
field. The Bussard ramjet can thus be seen as a ramjet variant of a fusion rocket.[citation needed] The Bussard ramjet was proposed in 1960 by the physicist
Bussard_ramjet
Proposed rocket propulsion mechanism
The nuclear salt-water rocket (NSWR) is a theoretical type of nuclear thermal rocket designed by Robert Zubrin. In place of traditional chemical propellant
Nuclear_salt-water_rocket
Type of spacecraft electric propulsion system
An arcjet rocket or arcjet thruster is a form of electrically powered spacecraft propulsion, in which an electrical discharge (arc) is created in a flow
Arcjet_rocket
Hypothetical type of spacecraft
nuclear propulsion. Specifically, it would be a type of gas core reactor rocket that uses a quartz wall to separate the nuclear fuel from the coolant and
Nuclear_lightbulb
Rocket engine that uses photons to propel a spacecraft
In a traditional nuclear photonic rocket, an onboard nuclear reactor would generate such high temperatures that the blackbody radiation from the reactor
Nuclear_photonic_rocket
Type of spacecraft propulsion using electrical energy to accelerate propellant
through electric or magnetic fields. Their principal advantage over chemical rockets is much higher specific impulse, meaning greater propellant efficiency
Spacecraft electric propulsion
Spacecraft_electric_propulsion
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
Spacecraft propulsion device
secondary rocket engine or other high thrust device is used to control the attitude of the rocket, while the primary thrust engine (generally also a rocket engine)
Thrusters_(spacecraft)
Hypothetical spacecraft propulsion through continuous nuclear explosions for thrust
Project Orion was the first serious attempt to design a nuclear pulse rocket. A design was formed at General Atomics during the late 1950s and early
Nuclear_pulse_propulsion
Method of spacecraft propulsion
craft has been inserted into orbit. Most satellites use monopropellant rocket motors or cold gas thrusters for such orbital adjustments. Both methods
Resistojet_rocket
Rocket engine operation method
The expander cycle is a power cycle of a Bipropellant liquid rocket engine. In this cycle, the fuel is used to cool the engine's combustion chamber, picking
Expander_cycle
Rocket engine operation method
The pressure-fed engine is a class of rocket engine designs. A separate gas supply, usually helium, pressurizes the propellant tanks to force fuel and
Pressure-fed_engine
Type of rocket engine
a type of rocket engine which uses the expansion of a (typically inert) pressurized gas to generate thrust. As opposed to traditional rocket engines, a
Cold_gas_thruster
Theoretical spacecraft propulsion system
A solar thermal rocket is a theoretical spacecraft propulsion system that would make use of solar power to directly heat reaction mass, and therefore would
Solar_thermal_rocket
Physical and science fiction concept
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
Anti-gravity
Space propulsion method using Sun radiation
of low-cost operations combined with high speeds (relative to chemical rockets) and long operating lifetimes. Since they have few moving parts and use
Solar_sail
Proposed spacelaunch method
A mass driver or electromagnetic catapult is a proposed method of non-rocket spacelaunch which would use a linear motor to accelerate and catapult payloads
Mass_driver
Space navigation technique
from gravity assist alone, a rocket burn near the periapsis (closest planetary approach) uses the least fuel. A given rocket burn always provides the same
Gravity_assist
Type of electric propulsion
were converted to thrust. Ad Astra Rocket Company is developing the Variable Specific Impulse Magnetoplasma Rocket (VASIMR). Canadian company Nautel is
Plasma_propulsion_engine
Rocket engine power cycle
is a power cycle of a bipropellant rocket engine. The cycle takes a small portion of hot exhaust gas from the rocket engine's combustion chamber and routes
Combustion_tap-off_cycle
Form of electrically powered spacecraft propulsion
current xenon-based ion thrusters, and about 25 times better than liquid rockets. MPD technology also has the potential for thrust levels of up to 200 newtons
Magnetoplasmadynamic_thruster
Class of liquid rocket propellants
class of liquid rocket propellants that were intended in the early 2010s to be able to replace hydrazine as the standard storable rocket propellent in some
Nitrous_oxide_fuel_blend
Rocket engine operation method
The electric-pump-fed engine is a bipropellant rocket engine in which the fuel pumps are electrically powered, and so all of the input propellant is directly
Electric-pump-fed_engine
Device claimed to be a propellantless spacecraft thruster
measurements refute all EmDrive claims by at least 3 orders of magnitude." Rocket engines operate by expelling propellant, which acts as a reaction mass and
EmDrive
Load bearing cable connecting objects in space
is theorized to be significantly less expensive than spaceflight using rocket engines. Tether satellites might be used for various purposes, including
Space_tether
Russian rocket engine manufacturer
companies on the Volga rocket engine project. The company continues to research and explore new engine concepts, such as the tripropellant, bi-modal engines
NPO_Energomash
Type of nuclear thermal rocket
A pulsed nuclear thermal rocket is a type of nuclear thermal rocket (NTR) concept developed at the Polytechnic University of Catalonia, Spain, and presented
Pulsed_nuclear_thermal_rocket
Propulsion system creating motion without propellant
science fiction trope as much as a technical claim, tying their appeal to the rocket equation and to the desire for a space engine that avoids the mass penalties
Reactionless_drive
Space propulsion system, electrostatic gridded ion thruster
Patterson, M. J.: "Ion Propulsion Development Projects in U. S.: Space Electric Rocket Test 1 to Deep Space 1." Journal of Propulsion and Power, Vol. 17, No. 3
NASA Solar Technology Application Readiness
NASA_Solar_Technology_Application_Readiness
Spacecraft propulsion system by NASA. 50kW Hall-effect thrusters, now for Lunar Gateway
is based on the 12.5 kW development model thruster called 'Hall Effect Rocket with Magnetic Shielding' (HERMeS). The AEPS solar electric engine makes
Advanced Electric Propulsion System
Advanced_Electric_Propulsion_System
Type of electric propulsion system
2514/1.38092. hdl:2027.42/77214. "U.N. Kills Any Plans to Use Mercury as a Rocket Propellant". spectrum.ieee.org. Retrieved 26 June 2026. Kerslake, William
Hall-effect_thruster
Rocket-propelled by exhausted coolant of a gas-cooled nuclear reactor
Gas core reactor rockets are a conceptual type of rocket that is propelled by the exhausted coolant of a gaseous fission reactor. The nuclear fission
Gas_core_reactor_rocket
Proposed nuclear pulse propulsion through antimatter-catalyzed nuclear chain reactions
antihydrogen. Tuning of the performance of a space vehicle is also possible. Rocket efficiency is strongly related to the mass of the working mass used, which
Antimatter-catalyzed nuclear pulse propulsion
Antimatter-catalyzed_nuclear_pulse_propulsion
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
Mechanism where confined high-speed particles confer energy to a vehicle
have also been proposed. Rockets are momentum machines; they use mass ejected from the rocket to provide momentum to the rocket. Momentum is the product
Beam-powered_propulsion
Type of propulsion for spacecraft
Plasma Thrusters (PPT's) are not to be confused with the Pulsed Plasma Rocket (PPR) developed by Howe Industries, as the PPT is an electric propulsion
Pulsed_plasma_thruster
Spacecraft propulsion technology
Ion-propelled aircraft Propulsive fluid accumulator – Self-filling orbital rocket fuel depot Romano, Francesco (January 2022). RF Helicon Plasma Thruster
Atmosphere-breathing electric propulsion
Atmosphere-breathing_electric_propulsion
Space propulsion system
systems were first demonstrated in space by the NASA Lewis Space Electric Rocket Test (SERT) I and II. These thrusters used mercury as the reaction mass
Gridded_ion_thruster
Type of electric spacecraft propulsion system
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
Field-emission electric propulsion
Field-emission_electric_propulsion
Hypothetical method of spacecraft propulsion
solar sail-like craft. It is similar in concept to the fission-fragment rocket in that the fission by-products are directly harnessed as working mass,
Fission_sail
Type of solar sail
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
Diffractive_solar_sail
Type of spacecraft plasma propulsion system
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
Pulsed_inductive_thruster
Propulsion concepts and technologies
propellants to generate thrust via Newton's third law, which is the familiar rocket launch with explosive flame and smoke beneath it. In this article, field
Field_propulsion
Space propulsion system, a gridded electrostatic ion thruster
NASA. 50kW Hall-effect thrusters, now for Lunar Gateway Nuclear electric rocket George R Schmidt; Michael J Patterson; Scott W Benson. "The NASA Evolutionary
NEXT_(ion_thruster)
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
Electrodeless_plasma_thruster
Proposed spacecraft propulsion device
atmospheric entry missions. Braking would require a conventional chemical rocket. The proposed craft has three parts: the E-sail module with solar panels
Electric_sail
Prototype spacecraft propulsion engine
nine months with conventional chemical rockets.[failed verification] Variable Specific Impulse Magnetoplasma Rocket (VASIMR) J Ling; M D West; T Lafleur;
Helicon_double-layer_thruster
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
Vacuum_arc_thruster
US spacecraft
received from CubeSail". Based upon the state vector initially provided by Rocket Lab after deployment, our best assessment is that CubeSail was Space-Track
CubeSail_(UltraSail)
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
High Power Electric Propulsion
High_Power_Electric_Propulsion
Ion thruster subtype
(or electrospray thruster) is a type of low thrust electric propulsion rocket engine that uses electrostatic acceleration of charged liquid droplets for
Colloid_thruster
Type of space propulsion using microwaves
having inelastic collisions. Thrust is the force that is applied on the rocket caused by when the propellant is released. The formula for thrust is given
Microwave electrothermal thruster
Microwave_electrothermal_thruster
classic drag device is a sailing vessel. By contrast, an airplane or a rocket use a fuel source to supply their own energy. Gyroradius Magnetic sail,
Plasma_magnet
rocket Solid-propellant rocket Hybrid-propellant rocket Propellants Liquid propellant Cryogenic Hypergolic Monopropellant Bipropellant Tripropellant Power
MagBeam
Plasma Physics Experiment
fusion rockets, especially those formed by RMF. This concept is similar to the Direct Fusion Drive, a current research project to create a fusion rocket from
Star_Thrust_Experiment
Spacecraft propulsion using steam as propellant
steam engine. Asteroidal water Lunar water Spacecraft propulsion Steam rocket Water on Mars Water on terrestrial planets of the Solar System "The World
World Is Not Enough (spacecraft propulsion)
World_Is_Not_Enough_(spacecraft_propulsion)
Monopropellant
acid. It was researched during the 1960s by teams working at the Naval Air Rocket Test Station as an alternative to the more commonly used hydrazine monopropellant
Cavea-B
Proposed spacecraft propulsion method
after being initially accelerated by other means, for example. a fusion rocket, to a significant fraction of light speed, with a more detailed design published
Magnetic_sail
двигатель". ТАСС. Retrieved 2019-07-23. HUANG, WENSHENG (Dec 2017). "Electric rockets power bigger share". "MediaRoom - News Releases/Statements". MediaRoom
List of spacecraft with electric propulsion
List_of_spacecraft_with_electric_propulsion
TRIPROPELLANT ROCKET
TRIPROPELLANT ROCKET
TRIPROPELLANT ROCKET
Girl/Female
Hindu, Indian
Good Music
Boy/Male
Tamil
Honest
Girl/Female
Arabic, German, Gujarati, Hebrew, Hindu, Indian, Kannada, Malayalam, Marathi, Muslim, Sanskrit, Tamil, Telugu
The Brave Princess; A Parrot; Princess; Koel; Cuckoo; A Thing of Beauty; Nature; A Bird
Boy/Male
Hindu, Indian, Marathi
The Sun
Boy/Male
Indian, Tamil
King of One Kind of
Girl/Female
Muslim/Islamic
Acclaim
Girl/Female
Hindu, Indian, Marathi
Goddess of Grace
Boy/Male
Christian, Hindu, Indian, Tamil
Sky
Girl/Female
Tamil
Jershika | ஜேரà¯à®·à¯€à®•à®¾
Girl/Female
Hindu, Indian, Modern
Protection
TRIPROPELLANT ROCKET
TRIPROPELLANT ROCKET
TRIPROPELLANT ROCKET
TRIPROPELLANT ROCKET
TRIPROPELLANT ROCKET
n.
A composition of combustible matter used in the heading of rockets, in mines, etc., which, exploding in the air, presents a starlike appearance.
n.
A cruciferous plant (Eruca sativa) sometimes eaten in Europe as a salad.
n.
Rocket larkspur. See below.
v. t.
Any long and comparatively slender piece of wood, whether in natural form or shaped with tools; a rod; a wand; a staff; as, the stick of a rocket; a walking stick.
imp. & p. p.
of Rocket
n.
A blunt lance head used in the joust.
n.
Damewort.
n.
A fiery meteor; an ignis fatuus; a rocket.
n.
A bird, especially a pheasant, which, being flushed, rises straight in the air like a rocket.
n.
An attack upon a fortress or fortified town, with shells, hot shot, rockets, etc.; the act of throwing bombs and shot into a town or fortified place.
p. pr. & vb. n.
of Rocket
v. i.
To rise straight up; said of birds; usually in the present participle or as an adjective.
n.
An artificial firework consisting of a cylindrical case of paper or metal filled with a composition of combustible ingredients, as niter, charcoal, and sulphur, and fastened to a guiding stick. The rocket is projected through the air by the force arising from the expansion of the gases liberated by combustion of the composition. Rockets are used as projectiles for various purposes, for signals, and also for pyrotechnic display.
n.
An herb (Reseda luteola) related to mignonette, growing in Europe, and to some extent in America; dyer's broom; dyer's rocket; dyer's weed; wild woad. It is used by dyers to give a yellow color.
n.
A rocket that ascends high and burns as it flies; a species of fireworks.
v. t.
To cause to explode; as, to fire a torpedo; to disharge; as, to fire a musket or cannon; to fire cannon balls, rockets, etc.