The development of high power magnetoplasmadynamic (MPD) thrusters is rapidly approaching an impasse to further development: the lack of a facility with adequate vacuum pumping and energy removal capacity to support the resolution of key MPD life and performance issues by FY-93. Several studies have been performed that identify vacuum systems or facility concepts that would alleviate this problem. Although feasible, the proposed vacuum systems require significant research and development; and the proposed facility concepts all require the added development of a gas dynamic diffuser. 8 refs., 4 figs
The following activities and plans in the MPD thruster development are summarized: (1) experimental ...
The paper starts with a brief account of the origins of MPD concept followed by an explanation of Lo...
Abstract: The Magnetically enhanced Vacuum Arc Thruster (MVAT) is a solid propellant micro-thruster ...
Propulsion requirements for large platform orbit raising, cargo and piloted planetary missions, and ...
Currently available or realizable applied eld magnetoplasmadynamic (AF–MPD) thrusters operating in ...
High-power electromagnetic thrusters have been proposed as primary in-space propulsion options for s...
Magnetoplasmadynamic (MPD) thrusters are capable of accelerating quasi-neutral plasmas to high exhau...
IRS and Alta are currently involved in ESA and EU (HIPER) programs aiming for the development of hig...
Testing high power electric propulsion devices poses unique requirements on space simulation facilit...
Performance and lifetime requirements for multimegawatt magnetoplasmadynamic (MPD) thrusters were us...
A 260 kW magnetoplasmadynamic (MPD) thruster test facility was assembled and used to characterize th...
High-power electromagnetic thrusters have been proposed as primary in-space propulsion options for s...
Historically, the National Aeronautics and Space Administration (NASA) has used rocket-powered vehic...
Developmental considerations for the magneto-plasma-dynamic (MPD) thruster are defined. General char...
Over the last decade there has been a growing demand for electric propulsion (EP) systems providing ...
The following activities and plans in the MPD thruster development are summarized: (1) experimental ...
The paper starts with a brief account of the origins of MPD concept followed by an explanation of Lo...
Abstract: The Magnetically enhanced Vacuum Arc Thruster (MVAT) is a solid propellant micro-thruster ...
Propulsion requirements for large platform orbit raising, cargo and piloted planetary missions, and ...
Currently available or realizable applied eld magnetoplasmadynamic (AF–MPD) thrusters operating in ...
High-power electromagnetic thrusters have been proposed as primary in-space propulsion options for s...
Magnetoplasmadynamic (MPD) thrusters are capable of accelerating quasi-neutral plasmas to high exhau...
IRS and Alta are currently involved in ESA and EU (HIPER) programs aiming for the development of hig...
Testing high power electric propulsion devices poses unique requirements on space simulation facilit...
Performance and lifetime requirements for multimegawatt magnetoplasmadynamic (MPD) thrusters were us...
A 260 kW magnetoplasmadynamic (MPD) thruster test facility was assembled and used to characterize th...
High-power electromagnetic thrusters have been proposed as primary in-space propulsion options for s...
Historically, the National Aeronautics and Space Administration (NASA) has used rocket-powered vehic...
Developmental considerations for the magneto-plasma-dynamic (MPD) thruster are defined. General char...
Over the last decade there has been a growing demand for electric propulsion (EP) systems providing ...
The following activities and plans in the MPD thruster development are summarized: (1) experimental ...
The paper starts with a brief account of the origins of MPD concept followed by an explanation of Lo...
Abstract: The Magnetically enhanced Vacuum Arc Thruster (MVAT) is a solid propellant micro-thruster ...