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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
Change in velocity per amount of fuel
but a maximum thrust of only 68 mN (0.015 lbf). The variable specific impulse magnetoplasma rocket (VASIMR) engine currently in development will theoretically
Specific_impulse
American rocket propulsion company
in funding to Ad Astra Rocket Company of Texas for further development of its Variable Specific Impulse Magnetoplasma Rocket (VASIMR), an electromagnetic
Ad_Astra_Rocket_Company
Form of electric spacecraft propulsion
plasma in the exhaust is neutral overall. The proposed Variable Specific Impulse Magnetoplasma Rocket (VASIMR) functions by using radio waves to ionize a
Ion_thruster
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
Non-airbreathing engine used to propel a missile or vehicle
(they have the lowest specific impulse) but measures can be taken to increase the rockets efficiency and certain types of rocket engines can be extremely
Rocket_engine
Method used to accelerate spacecraft
Pulsed inductive thrusters Pulsed plasma thrusters Variable specific impulse magnetoplasma rockets (VASIMR) Vacuum arc thrusters Mass drivers designed
Spacecraft_propulsion
Type of propelling nozzle
proposed for some types of propulsion (for example, Variable Specific Impulse Magnetoplasma Rocket, VASIMR), in which the flow of plasma or ions are directed
Rocket_engine_nozzle
Chemical element with atomic number 18 (Ar)
Argon is used as a propellant in the development of the Variable Specific Impulse Magnetoplasma Rocket (VASIMR). Compressed argon gas is allowed to expand
Argon
Low-frequency EM wave created in plasmas by a magnetic field
plasma-based rockets are suitable for interplanetary travel. Helicon double-layer thruster Variable Specific Impulse Magnetoplasma Rocket Storey, L. R
Helicon_(physics)
already been tested to varying levels, such as Variable Specific Impulse Magnetoplasma Rocket, and nuclear rockets. In the former case, a trip time of forty
Colonization_of_Mars
High efficiency engine for space travel
Field-emission electric propulsion Variable Specific Impulse Magnetoplasma Rocket (VASIMR) Batteries in space Liquid-propellant rocket List of spacecraft with electric
Solar_electric_propulsion
ESA plan a human mission to Mars in the 2030s. The Variable Specific Impulse Magnetoplasma Rocket (VASIMR) is an electro-magnetic thruster for spacecraft
History_of_technology
Tripropellant rocket — Tsiolkovsky rocket equation — Turbomachinery — Two-stage-to-orbit — UFO UAV V-2 rocket — Variable specific impulse magnetoplasma rocket — Velocity
Index of aerospace engineering articles
Index_of_aerospace_engineering_articles
American astronaut and entrepreneur (born 1950)
Years of research and development have produced the Variable Specific Impulse Magnetoplasma Rocket (VASIMR), an electrical propulsion device for use in
Franklin_Chang-Díaz
Proposed spacelaunch method
with some thruster types, including mass drivers and variable specific impulse magnetoplasma rockets). Since a mass driver could use any type of mass for
Mass_driver
List of definitions of terms and concepts commonly used in aerospace engineering
with the vertical launch of MW 18014 on 20 June 1944. Variable specific impulse magnetoplasma rocket – (VASIMR), is an electrothermal thruster under development
Glossary of aerospace engineering
Glossary_of_aerospace_engineering
Chemical substance used for propulsion
arc Microwave – a type of Radiofrequency ion thruster Variable specific impulse magnetoplasma rocket (VASIMR) – using microwave-generated plasma as the propellant
Propellant
Hypothetical propulsion systems for interstellar travel
Magnetoplasmadynamic thruster Pulsed plasma thruster Variable Specific Impulse Magnetoplasma Rocket Electromagnetic propulsion Spacecraft electric propulsion
Theoretical spacecraft propulsion
Theoretical_spacecraft_propulsion
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
Use of circular rotational force to mimic gravity
Hall effect thrusters and Variable Specific Impulse Magnetoplasma Rockets (VASIMR). Both provide very high specific impulse but relatively low thrust
Artificial_gravity
Maxwell Prize (2018) Franklin Chang-Diaz created the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) concept, an electromagnetic thruster for spacecraft
List_of_plasma_physicists
contributed to the theoretical underpinning of the Variable Specific Impulse Magnetoplasma Rocket (VASIMR) project in collaboration with NASA. He has
Boris_Breizman
Proposed spacecraft propulsion method
the interstellar medium is relatively large, and both the magsail and magnetoplasma sail have significant thrust for travel away from Earth using the force
Magnetic_sail
Van Allen radiation belt Vapor–liquid–solid method Variable Specific Impulse Magnetoplasma Rocket Vector inversion generator Versatile Toroidal Facility
List of plasma physics articles
List_of_plasma_physics_articles
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