Add to ORKGPropulsive performance and erosion behavior of accelerator nozzle operating as short pulse discharge or quasi-steady solid Teflon propellant plasma thruste
Pulsed inductive plasma thrusters [1-3] are spacecraft propulsion devices in which electrical energy...
Abstract: NASA Glenn Research Center (GRC) has evaluated the performance of a pulsed plasma thruster...
Since the Russian launch of the Zond-2 satellite in 1964 there have been over fifty years of research...
The technique of feeding a solid propellant into the discharge from the sides of the discharge was e...
Evaluation of magnetohydrodynamic arc thrusters operating in quasi-steady mode with electrode vapor ...
Results are reported from a continued study of MPD thrusters operating in the quasi-steady mode and ...
Applications of quasi-steady state plasma acceleration to development of pulsed plasma jet engine
Exhaust velocity and thrust measurements are performed on a pulsed electrothermal thruster using pol...
This research is focused on several areas of the μPPT performance. An important idea studied is the ...
The performance of quasi-steady magnetoplasmadynamic (MPD) thrusters at high power levels is discuss...
Pulsed plasma thrusters are currently planned on two small satellite missions and proposed for a thi...
Experiments conducted at the Surrey Space Centre on a breadboard pulsed plasma thruster (PPT) have l...
Electric solid propellants are an attractive option for space propulsion because they are ignited by...
A simple model for the production of ions that impinge on and sputter erode the accelerator grid of ...
Measurements of the pulsed plasma thruster (PPT) plume upstream mass flux were made in the Molecular...
Pulsed inductive plasma thrusters [1-3] are spacecraft propulsion devices in which electrical energy...
Abstract: NASA Glenn Research Center (GRC) has evaluated the performance of a pulsed plasma thruster...
Since the Russian launch of the Zond-2 satellite in 1964 there have been over fifty years of research...
The technique of feeding a solid propellant into the discharge from the sides of the discharge was e...
Evaluation of magnetohydrodynamic arc thrusters operating in quasi-steady mode with electrode vapor ...
Results are reported from a continued study of MPD thrusters operating in the quasi-steady mode and ...
Applications of quasi-steady state plasma acceleration to development of pulsed plasma jet engine
Exhaust velocity and thrust measurements are performed on a pulsed electrothermal thruster using pol...
This research is focused on several areas of the μPPT performance. An important idea studied is the ...
The performance of quasi-steady magnetoplasmadynamic (MPD) thrusters at high power levels is discuss...
Pulsed plasma thrusters are currently planned on two small satellite missions and proposed for a thi...
Experiments conducted at the Surrey Space Centre on a breadboard pulsed plasma thruster (PPT) have l...
Electric solid propellants are an attractive option for space propulsion because they are ignited by...
A simple model for the production of ions that impinge on and sputter erode the accelerator grid of ...
Measurements of the pulsed plasma thruster (PPT) plume upstream mass flux were made in the Molecular...
Pulsed inductive plasma thrusters [1-3] are spacecraft propulsion devices in which electrical energy...
Abstract: NASA Glenn Research Center (GRC) has evaluated the performance of a pulsed plasma thruster...
Since the Russian launch of the Zond-2 satellite in 1964 there have been over fifty years of research...