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![Contamination Study of a Micro Pulsed Plasma Thruster]( "Contamination Study of a Micro Pulsed Plasma Thruster")
Contamination Study of a Micro Pulsed Plasma Thruster59,99 €![Using a Gatling-Gun Configured Micro Pulsed Plasma Thruster as a Means to Control Micro Satellites with Extreme Precision]( "Using a Gatling-Gun Configured Micro Pulsed Plasma Thruster as a Means to Control Micro Satellites with Extreme Precision")
Using a Gatling-Gun Configured Micro Pulsed Plasma Thruster as a Means to Control Micro Satellites with Extreme Precision59,99 €![Thrust and Performance Study of Micro Pulsed Plasma Thrusters]( "Thrust and Performance Study of Micro Pulsed Plasma Thrusters")
Thrust and Performance Study of Micro Pulsed Plasma Thrusters59,99 €![Characterizing the Exhaust Plume of the Three-Electrode Micro Pulsed Plasma Thrusters]( "Characterizing the Exhaust Plume of the Three-Electrode Micro Pulsed Plasma Thrusters")
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Performance Characterization of a Novel Plasma Thruster to Provide a Revolutionary Operationally Responsive Space Capability with Micro- and Nano-Sate59,99 €![Patterning and Characterization of Carbon Nanotubes Grown in a Microwave Plasma Enhanced Chemical Vapor Deposition Chamber]( "Patterning and Characterization of Carbon Nanotubes Grown in a Microwave Plasma Enhanced Chemical Vapor Deposition Chamber")
Patterning and Characterization of Carbon Nanotubes Grown in a Microwave Plasma Enhanced Chemical Vapor Deposition Chamber59,99 €![An Experimental Study of a Pulsed DC Plasma Flow Control Actuator]( "An Experimental Study of a Pulsed DC Plasma Flow Control Actuator")
An Experimental Study of a Pulsed DC Plasma Flow Control Actuator59,99 €
The micro pulsed plasma thruster (micro-PPT) is a simple and versatile electric thruster capable of performing multiple missions, from precise attitude control on standard satellites to primary propulsion for nanosatellites. In order to fill this role as both industry and government move toward utilizing smaller satellites, micro-PPTs first need to be thoroughly tested on the ground. This study examines the deposition profile and rate of particle emission from the thruster so that satellite designers understand any potential contamination issues with sensitive instruments and solar panels.