AI & ChatGPT searches , social queries for PULSED INDUCTIVE-THRUSTER
Search references for PULSED INDUCTIVE-THRUSTER. Phrases containing PULSED INDUCTIVE-THRUSTER
See searches and references containing PULSED INDUCTIVE-THRUSTER!
Search references for PULSED INDUCTIVE-THRUSTER. Phrases containing PULSED INDUCTIVE-THRUSTER
See searches and references containing PULSED INDUCTIVE-THRUSTER!PULSED INDUCTIVE-THRUSTER
Type of spacecraft plasma propulsion system
A pulsed inductive thruster (PIT) is a form of ion thruster, used in spacecraft propulsion. It is a plasma propulsion engine using perpendicular electric
Pulsed_inductive_thruster
Type of propulsion for spacecraft
A pulsed plasma thruster (PPT) or as a plasma jet engine (PJE), is a form of electric spacecraft propulsion. PPTs are generally considered the simplest
Pulsed_plasma_thruster
Type of electric propulsion
is also crucial to the operation of most pulsed plasma thrusters.[citation needed] Pulsed inductive thrusters (PIT) also use the Lorentz force to generate
Plasma_propulsion_engine
Topics referred to by the same term
electrically Hall-effect thruster, a type of ion thruster Pulsed inductive thruster, a pulsed form of ion thruster Magnetoplasmadynamic thruster, electric propulsion
Thruster
Form of electric spacecraft propulsion
charged ion stream to prevent charging of the spacecraft. Pulsed inductive thrusters (PITs) use pulses instead of continuous thrust and have the ability to
Ion_thruster
Form of electrically powered spacecraft propulsion
Unit, which demonstrated the successful operation of a quasi-steady pulsed MPD thruster in space. Research at Moscow Aviation Institute, RKK Energiya, National
Magnetoplasmadynamic_thruster
Spacecraft propulsion device
Magnetoplasmadynamic thruster, electric propulsion using the Lorentz force Pulsed inductive thruster, a pulsed form of ion thruster Pulsed plasma thruster, using current
Thrusters_(spacecraft)
Space propulsion system
The gridded ion thruster is a common design for ion thrusters, a highly efficient low-thrust spacecraft propulsion method running on electrical power
Gridded_ion_thruster
Hypothetical spacecraft propulsion through continuous nuclear explosions for thrust
Nuclear pulse propulsion or external pulsed plasma propulsion is a hypothetical method of spacecraft propulsion that uses nuclear explosions for thrust
Nuclear_pulse_propulsion
Type of spacecraft propulsion using electrical energy to accelerate propellant
Hall-effect thrusters, and colloid thrusters; electromagnetic devices such as pulsed plasma thrusters, magnetoplasmadynamic thrusters, and pulsed inductive thrusters;
Spacecraft electric propulsion
Spacecraft_electric_propulsion
Space propulsion system, a gridded electrostatic ion thruster
The NASA Evolutionary Xenon Thruster (NEXT) project at Glenn Research Center is a gridded electrostatic ion thruster about three times as powerful as the
NEXT_(ion_thruster)
Propulsion system creating motion without propellant
thrusters such as the EmDrive and Cannae drive, the helical engine, Mach-effect or MEGA drives, quantum drive claims, and the quantum vacuum thruster
Reactionless_drive
Type of electric propulsion system
propulsion, a Hall-effect thruster (HET, sometimes referred to as a Hall thruster or Hall-current thruster) is a type of ion thruster in which the propellant
Hall-effect_thruster
Electrothermal thruster in development
concepts are the electrodeless plasma thruster, the microwave arcjet rocket, and the pulsed inductive thruster. The propellant, a neutral gas such as
Variable Specific Impulse Magnetoplasma Rocket
Variable_Specific_Impulse_Magnetoplasma_Rocket
Type of rocket engine
A cold gas thruster (or a cold gas propulsion system) is a type of rocket engine which uses the expansion of a (typically inert) pressurized gas to generate
Cold_gas_thruster
Spacecraft propulsion technology
for an atmosphere-breathing electric propulsion system using an inductive plasma thruster". Acta Astronautica. 147: 114–126. arXiv:2103.02328. Bibcode:2018AcAau
Atmosphere-breathing electric propulsion
Atmosphere-breathing_electric_propulsion
Type of spacecraft propulsion system
nuclear electrical generation systems, including VASIMR, DS4G, and pulsed inductive thruster (PIT). PIT and VASIMR are unique in their ability to trade between
Nuclear_electric_rocket
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
Proposed spacecraft propulsion method
the fusion runway pellets with a spacecraft moving at high speed. Laser pulses could be used to guide the pellets. If using impact fusion, the spacecraft
Bussard_ramjet
Device claimed to be a propellantless spacecraft thruster
physics. The concept has at times been referred to as a resonant cavity thruster. Physicists and engineers generally regard the EmDrive concept as pseudoscience
EmDrive
Ion thruster subtype
A colloid thruster (or electrospray thruster) is a type of low thrust electric propulsion rocket engine that uses electrostatic acceleration of charged
Colloid_thruster
The electrodeless plasma thruster is a spacecraft propulsion engine commercialized under the acronym "E-IMPAcT" for "Electrodeless-Ionization Magnetized
Electrodeless_plasma_thruster
Method of spacecraft propulsion
900 °C, specific impulse could be doubled in comparison to a cold gas thruster using the same propellant. In other words, a quadrupling of the temperature
Resistojet_rocket
Spacecraft propulsion system by NASA. 50kW Hall-effect thrusters, now for Lunar Gateway
electric power for its Hall-effect thrusters for maneuverability, which can be supported by chemical monopropellant thrusters for high-thrust attitude control
Advanced Electric Propulsion System
Advanced_Electric_Propulsion_System
Prototype spacecraft propulsion engine
The helicon double-layer thruster is a prototype electric spacecraft propulsion. It was created by Australian scientist Christine Charles, based on a technology
Helicon_double-layer_thruster
Conceptual rocket engine
expand through the magnetic nozzle and beyond, and thus, function as an ion thruster. The construction of the experimental research device and most of its early
Direct_Fusion_Drive
Proposed nuclear pulse propulsion through antimatter-catalyzed nuclear chain reactions
Antimatter-catalyzed nuclear pulse propulsion, antiproton-catalyzed nuclear pulse propulsion, ACMF: Antiproton-Catalyzed Microfission-Fusion and AIM: Antimatter
Antimatter-catalyzed nuclear pulse propulsion
Antimatter-catalyzed_nuclear_pulse_propulsion
Mechanism where confined high-speed particles confer energy to a vehicle
is either pulsed or continuous. A continuous beam lends itself to thermal rockets, photonic thrusters, and light sails. In contrast, a pulsed beam lends
Beam-powered_propulsion
Method used to accelerate spacecraft
engines Magnetoplasmadynamic thrusters Electrodeless plasma thrusters Pulsed inductive thrusters Pulsed plasma thrusters Variable specific impulse magnetoplasma
Spacecraft_propulsion
creates thrust for the vacuum arc thruster. Thus, whereas the insulator is used as propellant in a pulsed plasma thruster, in a VAT the solid metallic cathode
Vacuum_arc_thruster
Rocket that burns 3 propellants at once or 2 fuels with an oxidizer, sequentially
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Tripropellant_rocket
Type of space propulsion using microwaves
Microwave electrothermal thruster, also known as MET, is a propulsion device that converts microwave energy (a type of electromagnetic radiation) into
Microwave electrothermal thruster
Microwave_electrothermal_thruster
Type of electric spacecraft propulsion system
(FEEP) is an advanced electrostatic space propulsion concept, a form of ion thruster, that uses a liquid metal as a propellant – usually either caesium, indium
Field-emission electric propulsion
Field-emission_electric_propulsion
Type of plasma source
plasma Induction plasma technology Pulsed inductive thruster High density fluorocarbon etching of silicon in an inductively coupled plasma: Mechanism of etching
Inductively_coupled_plasma
Rocket driven by nuclear fusion power
fusion instead of direct thrust. Spacecraft propulsion methods such as ion thrusters require electric power to run but are highly efficient. In some cases
Fusion_rocket
Type of rocket engine fuel
and reaction control thrusters: Apollo command and service module RCS, Space Shuttle OMS and RCS; Ariane 5 EPS; Draco thrusters used by the SpaceX Dragon
Hypergolic_propellant
Vehicle propulsion using electromagnetic fields
magnetoplasmadynamic thruster sometimes referred to as the Lorentz force accelerator (LFA), and the electrodeless pulsed inductive thruster (PIT). Even today
Magnetohydrodynamic_drive
Rocket engine operation method
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Expander_cycle
Nuclear spacecraft propulsion technology
a dramatic increase in performance. To do this, pulsed reactors operate in a series of brief pulses rather than the continual chain reaction of a conventional
Nuclear_thermal_rocket
Space propulsion method using Sun radiation
solar sail has also been proposed to be addressed with a solar photon thruster. This also uses a reflective membrane, but unlike a conventional solar
Solar_sail
Type of rocket engine which uses liquid fuel stored at very low temperatures
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Cryogenic_rocket_engine
Proposed rocket propulsion mechanism
propulsion systems, except that NSWRs would generate continuous rather than pulsed thrust and may be workable on much smaller scales than the smallest feasible
Nuclear_salt-water_rocket
Rocket engine operation method
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Gas-generator_cycle
Proposed spacelaunch method
(which still often have a niche in extreme pulse power applications). However, energy can be stored inductively in superconducting coils. A 1 km long mass
Mass_driver
Propulsion concepts and technologies
first laboratory electric thruster was electrothermal and the first electric thruster to ever fly in space was of the pulsed (mostly electromagnetic) plasma
Field_propulsion
Topics referred to by the same term
and statistics Programmable interval timer, a computing device Pulsed inductive thruster, a device used in spacecraft propulsion Pyrena or pit, the hard
Pit
Load bearing cable connecting objects in space
are currently tracked on radar and have predictable orbits. Although thrusters could be used to change the orbit of the system, a tether could also be
Space_tether
Charged-particle flow due to high electrostatic potential
ioniser Ion thruster Ionocraft Plasma actuator Hall-effect thruster Magnetohydrodynamic drive Magnetoplasmadynamic thruster Pulsed inductive thruster Field-emission
Ion_wind
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
perhaps 1.3 to 1.5 N (0.29 to 0.34 lbf), making them useful only for thrusters. In order to increase the power for medium-duration missions, engines
Radioisotope_rocket
Type of nuclear propulsion method with an ultra high specific-inpulse
from the individual fuel particles. Fission sail Nuclear salt-water rocket Pulsed nuclear thermal rocket Fission fragment reactor Chapline, G.; Dickson, P
Fission-fragment_rocket
Proposed spacecraft propulsion method
Magnetoplasmadynamic thruster (aka MPD Arc jet in Japan) in 2015, multiple antenna coils in 2019, and a multi-pole MPD thruster in 2020. Slough published
Magnetic_sail
Chemical substance used for propulsion
hydrogen, hydrazine, or lithium; expelled using the Lorentz force Pulsed inductive thruster – because this reactive engine uses a radial magnetic field, it
Propellant
Space propulsion system, electrostatic gridded ion thruster
Application Readiness (NSTAR) is a type of spacecraft ion thruster called electrostatic ion thruster. It is a highly efficient low-thrust spacecraft propulsion
NASA Solar Technology Application Readiness
NASA_Solar_Technology_Application_Readiness
Type of solar sail
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Diffractive_solar_sail
Rocket that uses a single propellant with a catalyst
storable propellant after passing it over a catalyst bed. The power for the thruster comes from the high pressure gas created during the decomposition reaction
Monopropellant_rocket
Rocket engine that uses both liquid / gaseous and solid fuel
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Hybrid-propellant_rocket
Class of liquid rocket propellants
major classes of rocket fuels are: A common fuel in small maneuvering thrusters is hydrazine. It is liquid at room temperature and, having a positive
Nitrous_oxide_fuel_blend
Theoretical spacecraft propulsion system
inbound to receive fuel from the depot. Solar-thermal monoprop hydrogen thrusters are also integral to the design of the next-generation cryogenic upper
Solar_thermal_rocket
Proposed spacecraft propulsion device
panels and reels to hold the wires; the main body, including chemical thrusters for adjusting trajectory en route and at destination and communications
Electric_sail
Rocket-propelled by exhausted coolant of a gas-cooled nuclear reactor
Nuclear lightbulb Nuclear material Atomic physics Project Orion Nuclear pulse propulsion Discovery One Thode, L. E.; Cline, M. C.; Howe, S. D. (July 1998)
Gas_core_reactor_rocket
Liquid form of rocket propellants
Anflo, K.; Moore, S.; King, P. Expanding the ADN-based Monopropellant Thruster Family. 23rd Annual AIAA/USU Conference on Small Satellites. SSC09-II-4
Liquid_rocket_propellant
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Plasma_magnet
Hypothetical method of spacecraft propulsion
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Fission_sail
Rocket with a motor that uses solid propellants
control of the nozzle geometry or through the use of vent ports. Further, pulsed rocket motors that burn in segments, and that can be ignited upon command
Solid-propellant_rocket
Hypothetical type of spacecraft
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Nuclear_lightbulb
Rocket engine operation method
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Electric-pump-fed_engine
Rocket engine that uses photons to propel a spacecraft
to overcome the inherent inefficiency in producing thrust of the photon thruster by amplifying the momentum transfer of photons by recycling photons between
Nuclear_photonic_rocket
Space navigation technique
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Gravity_assist
High Power Electric Propulsion (HiPEP) is a variation of ion thruster for use in nuclear electric propulsion applications. It was ground-tested in 2003
High Power Electric Propulsion
High_Power_Electric_Propulsion
Rocket engine operation method
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Staged_combustion_cycle
Rocket engine operation method
temperature fuel. Spacecraft attitude control and orbital maneuvering thrusters are almost universally pressure-fed designs. Examples include the Reaction
Pressure-fed_engine
Physical and science fiction concept
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Anti-gravity
Rocket engine that uses liquid fuels and oxidizers
orbital maneuvering system (OMS) engines and Reaction control system (RCS) thrusters. SpaceX's Draco and SuperDraco engines for the Dragon spacecraft. For
Liquid-propellant_rocket
Rocket engine power cycle
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Combustion_tap-off_cycle
List of definitions of terms and concepts commonly used in aerospace engineering
Pressure-fed engine – Propeller – Proper orbital elements – Pulsed inductive thruster – Pulsed plasma thruster – Propulsion – Radar – system using the reflection
Glossary of aerospace engineering
Glossary_of_aerospace_engineering
Spacecraft propulsion using steam as propellant
artificial regolith and took off within the vacuum chamber using steam thrusters. The system components are expected to reach technology readiness level
World Is Not Enough (spacecraft propulsion)
World_Is_Not_Enough_(spacecraft_propulsion)
Pressure-fed engine — Propeller — Proper orbital elements — Pulsed inductive thruster — Pulsed plasma thruster — Propulsion — Philippine Space Agency — Radar — Railgun
Index of aerospace engineering articles
Index_of_aerospace_engineering_articles
with electric space propulsion. This includes both cruise engines and/or thrusters for altitude and orbit control. It is not specified whether the given
List of spacecraft with electric propulsion
List_of_spacecraft_with_electric_propulsion
Launch system that only uses one rocket stage
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Single-stage-to-orbit
Monopropellant
hydrazine monopropellant for use in spacecraft's attitude control and thruster systems. It was derived from an earlier, similar formulation which came
Cavea-B
US spacecraft
expected thrust force due to solar pressure is equivalent to 400 kW ion thruster systems used for comparable deep space missions. Spaceflight portal IKAROS
CubeSail_(UltraSail)
PSK31 – Pulse amplitude – Pulse duration – Pulse – Pulse-address multiple access – Pulse-code modulation – Pulsed inductive thruster – Pulse-width modulation
Index_of_electronics_articles
of the NIAC. MagBeam is different from a traditional electrostatic ion thruster in several ways, the primary one being that instead of the fuel and propulsion
MagBeam
Plasma Physics Experiment
Electrostatic Colloid thruster Ion thruster Gridded Hall-effect thruster Field-emission electric propulsion Electromagnetic Pulsed inductive thruster Magnetoplasmadynamic
Star_Thrust_Experiment
Aerospace Engineer
sources, magnetoplasmadynamic thrusters, and pulsed inductive thrusters. US Patent No. 10,823,158, “Deployable Gridded Ion Thruster,” Authors: Walker, M. L
Mitchell_L.R._Walker
Devices that measure magnetic field strength using the Hall effect
sensors respond both to static magnetic fields and to changing ones. (Inductive sensors, in contrast, only respond to changes in fields.) The Hall voltage
Hall_effect_sensor
Low-frequency EM wave created in plasmas by a magnetic field
Potentially, helicon double-layer thruster plasma-based rockets are suitable for interplanetary travel. Helicon double-layer thruster Variable Specific Impulse
Helicon_(physics)
plasma thruster Proton beam Pseudospark switch Pulsed Energy Projectile Pulsed laser deposition, Dynamic of the plasma Pulsed plasma thruster, also Plasma
List of plasma physics articles
List_of_plasma_physics_articles
Free-flying robotic system
gaseous state before being ejected through the thrusters for propulsion. Desired thrust is achieved through pulse modulation of thrust solenoids. The maximum
SPHERES
American plasma physicist (born 1950)
laser fields to accelerate particles, such as the ones used in plasma thrusters. He is also known to have worked on the hydrodynamics of charged liquids
Nathaniel_J._Fisch
heating Inductive charging Inductive coupling Inductively coupled plasma Inductively coupled plasma atomic emission spectroscopy Inductively coupled plasma
Index_of_physics_articles_(I)
State of matter
kinetics of reactions and formation of complex nanomaterials. Hall-effect thruster Solar plasma Plasma spraying Plasma in a tokamak Laboratory plasma Chemistry
Plasma_(physics)
Synchronous electric motor powered by an electronic controller
Turntable Drive Techniques". 2 November 2019. Retrieved 2021-12-02. "What is a Thruster?". Blue Robotics. Retrieved 2024-01-12. "Custom axial flux permanent magnet
Brushless_DC_electric_motor
New technologies actively in development
original on 22 September 2010. Retrieved 7 December 2011. Norris, G., "Pulse Power: Pulse Detonation Engine-powered Flight Demonstration Marks Milestone in
List_of_emerging_technologies
Device that creates charged atoms and molecules (ions)
source or electric discharge to create ions. Ions can be created in an inductively coupled plasma, which is a plasma source in which the energy is supplied
Ion_source
NASA program
laser thrusters, extreme sample return, and innovative spherical robots designed for planetary exploration. Phase I selections were: Adams, Rob: Pulsed Fission-Fusion
NASA Institute for Advanced Concepts
NASA_Institute_for_Advanced_Concepts
Concept of collecting solar power in outer space and distributing it to Earth
stabilization: NASA explored a spin-stabilized thin film concept. Photonic laser thruster (PLT) stabilized structure: Young Bae has proposed that photon pressure
Space-based_solar_power
hanger crown plug Thr/Th# – thruster ('#'- means identification letter/number of the equipment, e.g. thr3 or thr#3 means "thruster no. 3"[citation needed])
List of abbreviations in oil and gas exploration and production
List_of_abbreviations_in_oil_and_gas_exploration_and_production
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER
PULSED INDUCTIVE-THRUSTER