The design techniques, circuit components, fabrication techniques, and past experience used in successful high-voltage power supplies for spacecraft flight systems are described. A discussion of the basic physics of electrical discharges in gases is included and a design rationale for the prevention of electrical discharges is provided. Also included are typical examples of proven spacecraft high-voltage power supplies with typical specifications for design, fabrication, and testing
Developing suitable solid state power controllers for space vehicles electrical power system
A power processing unit for a 15 kW Hall thruster is under development at NASA Glenn Research Center...
NASA Lewis Research Center is presently developing a 60 GHz traveling wave tube for satellite cross-...
This book is written for newcomers to the topic of high voltage (HV) in space and is intended to rep...
The scope, size, and capability of the nation's space-based activities are limited by the level of e...
The results of testing a high voltage electrical power system (EPS) breadboard using high voltage po...
The specific electrical discharge problems that can directly affect the shuttle vehicle and its payl...
The development of spacecraft with electrical loads that require high voltage power is discussed. Th...
A description is given of the electrical and mechanical design and operation of high voltage power s...
Two programmable, high voltage DC power supplies were developed as part of the flight electronics fo...
Three types of solid state power controllers (SSPC's) for high voltage, high power DC system applica...
This presentation describes recent activities in materials research for high voltage power transmiss...
The Lewis/OAST program for the development of Component Technology for Space Power Systems is descri...
Space power components including a family of bipolar power switching transistors, fast switching pow...
This presentation describes the NASA GRC Multifunctional Materials Team activities in high voltage m...
Developing suitable solid state power controllers for space vehicles electrical power system
A power processing unit for a 15 kW Hall thruster is under development at NASA Glenn Research Center...
NASA Lewis Research Center is presently developing a 60 GHz traveling wave tube for satellite cross-...
This book is written for newcomers to the topic of high voltage (HV) in space and is intended to rep...
The scope, size, and capability of the nation's space-based activities are limited by the level of e...
The results of testing a high voltage electrical power system (EPS) breadboard using high voltage po...
The specific electrical discharge problems that can directly affect the shuttle vehicle and its payl...
The development of spacecraft with electrical loads that require high voltage power is discussed. Th...
A description is given of the electrical and mechanical design and operation of high voltage power s...
Two programmable, high voltage DC power supplies were developed as part of the flight electronics fo...
Three types of solid state power controllers (SSPC's) for high voltage, high power DC system applica...
This presentation describes recent activities in materials research for high voltage power transmiss...
The Lewis/OAST program for the development of Component Technology for Space Power Systems is descri...
Space power components including a family of bipolar power switching transistors, fast switching pow...
This presentation describes the NASA GRC Multifunctional Materials Team activities in high voltage m...
Developing suitable solid state power controllers for space vehicles electrical power system
A power processing unit for a 15 kW Hall thruster is under development at NASA Glenn Research Center...
NASA Lewis Research Center is presently developing a 60 GHz traveling wave tube for satellite cross-...