A description is given of the electrical and mechanical design and operation of high voltage power supplies for space flight use. The supply was used to generate the spiraltron high voltage for low energy electron experiment on AE-C and D. Two versions of the supply were designed and built; one design is referred to as the low power version (AE-C) and the other as the high power version (AE-D). Performance is discussed under all operating conditions
The power processor operates in several modes, delivering up to 100 amperes of regulated electrical ...
Recent studies in electro-Aerodynamic (EAD) propulsion have stimulated the need for lightweight powe...
A power processing unit for a 15 kW Hall thruster is under development at NASA Glenn Research Center...
The design techniques, circuit components, fabrication techniques, and past experience used in succe...
This book is written for newcomers to the topic of high voltage (HV) in space and is intended to rep...
Experimental design of high voltage low current power source for unmanned, long term space missio
The results of testing a high voltage electrical power system (EPS) breadboard using high voltage po...
The low energy electron experiment (LEE) will provide differential measurements of the energy influx...
An improved high-voltage stepping supply, for space instrumentation is described where low power con...
Aerobee-borne electron accelerators for ejecting electron beams into upper atmospher
The power supply unit was developed to serve as the power source for a loran-C receiver. The power s...
High frequency power distribution and management is a technology ready state of development. As such...
High energy anode and cathode for dry tape battery - incapsulation of electrolyte - manufacturing an...
Direct current converters used in space electric power system for nuclear-electric power suppl
Performance of mercury electron bombardment thrustor at large acceleration potentia
The power processor operates in several modes, delivering up to 100 amperes of regulated electrical ...
Recent studies in electro-Aerodynamic (EAD) propulsion have stimulated the need for lightweight powe...
A power processing unit for a 15 kW Hall thruster is under development at NASA Glenn Research Center...
The design techniques, circuit components, fabrication techniques, and past experience used in succe...
This book is written for newcomers to the topic of high voltage (HV) in space and is intended to rep...
Experimental design of high voltage low current power source for unmanned, long term space missio
The results of testing a high voltage electrical power system (EPS) breadboard using high voltage po...
The low energy electron experiment (LEE) will provide differential measurements of the energy influx...
An improved high-voltage stepping supply, for space instrumentation is described where low power con...
Aerobee-borne electron accelerators for ejecting electron beams into upper atmospher
The power supply unit was developed to serve as the power source for a loran-C receiver. The power s...
High frequency power distribution and management is a technology ready state of development. As such...
High energy anode and cathode for dry tape battery - incapsulation of electrolyte - manufacturing an...
Direct current converters used in space electric power system for nuclear-electric power suppl
Performance of mercury electron bombardment thrustor at large acceleration potentia
The power processor operates in several modes, delivering up to 100 amperes of regulated electrical ...
Recent studies in electro-Aerodynamic (EAD) propulsion have stimulated the need for lightweight powe...
A power processing unit for a 15 kW Hall thruster is under development at NASA Glenn Research Center...