The development of lithium magnetoplasmadynamic (MPD) thrusters at JPL is discussed. The following topics are presented in vugraph form: mercury vapor mass flow control; porous tungsten vaporizer and housing; the lithium vaporizer experiment; a dry box for handling solid lithium; MPD thruster electrode modeling; engine lifetime definitions; cathode failure modeling; cathode erosion modeling; cathode thermal modeling; near cathode plasma model regions; cathode work function modeling; anode work function modeling; and radiation-cooled anodes
Magnetoplasmadynamic (MPD) thrusters have demonstrated performance and power handling capabilities w...
Information on space propulsion and technology and the cryogenic fluid depot is given in viewgraph f...
A stability equation relating thruster discharge current, argon propellant mass flow rate, and elect...
The topics covered are presented in viewgraph form and include the following: engine lifetime assess...
Inhouse magnetoplasmadynamic (MPD) thruster technology is discussed. The study focussed on steady st...
The topics are presented in viewgraph form and include the following: overall strategy for magnetopl...
Performance and lifetime requirements for multimegawatt magnetoplasmadynamic (MPD) thrusters were us...
The topics are presented in viewgraph form and include the following: facility construction; quadrup...
A lithium vaporizer for a high-power magnetoplasmadynamic (MPD) thruster is modeled using a parallel...
A two-dimensional, two-temperature, single fluid MHD code was used to predict the performance of cyl...
A 260 kW magnetoplasmadynamic (MPD) thruster test facility was assembled and used to characterize th...
Systems technology for nuclear electric propulsion (NEP) vehicles is discussed. The following topics...
Analysis and design of thrust chamber with gas generator, and thermodynamic-combustion characteristi...
Recent interest in solar electric orbit transfer vehicles (SEOTV's) has prompted a reevaluation of p...
Presentation concerns the building a test facility for high power and thermonuclear fusion propulsio...
Magnetoplasmadynamic (MPD) thrusters have demonstrated performance and power handling capabilities w...
Information on space propulsion and technology and the cryogenic fluid depot is given in viewgraph f...
A stability equation relating thruster discharge current, argon propellant mass flow rate, and elect...
The topics covered are presented in viewgraph form and include the following: engine lifetime assess...
Inhouse magnetoplasmadynamic (MPD) thruster technology is discussed. The study focussed on steady st...
The topics are presented in viewgraph form and include the following: overall strategy for magnetopl...
Performance and lifetime requirements for multimegawatt magnetoplasmadynamic (MPD) thrusters were us...
The topics are presented in viewgraph form and include the following: facility construction; quadrup...
A lithium vaporizer for a high-power magnetoplasmadynamic (MPD) thruster is modeled using a parallel...
A two-dimensional, two-temperature, single fluid MHD code was used to predict the performance of cyl...
A 260 kW magnetoplasmadynamic (MPD) thruster test facility was assembled and used to characterize th...
Systems technology for nuclear electric propulsion (NEP) vehicles is discussed. The following topics...
Analysis and design of thrust chamber with gas generator, and thermodynamic-combustion characteristi...
Recent interest in solar electric orbit transfer vehicles (SEOTV's) has prompted a reevaluation of p...
Presentation concerns the building a test facility for high power and thermonuclear fusion propulsio...
Magnetoplasmadynamic (MPD) thrusters have demonstrated performance and power handling capabilities w...
Information on space propulsion and technology and the cryogenic fluid depot is given in viewgraph f...
A stability equation relating thruster discharge current, argon propellant mass flow rate, and elect...