The tether and/or transmission line connecting the SP-100 to space station presents some unorthodox challenges in high voltage engineering, power transmission, and distribution. The line, which doubles as a structural element of this unusual spacecraft, will convey HVDC from SP-100 to the platform in low Earth orbit, and environment where the local plasma is sufficient to cause breakdown of exposed conductors at potentials of only a few hundred volts. Its anticipated several years operation, and continuously accumulating exposure to meteoroids and debris, raises an increasing likelihood that mechanical damage, including perforation, will be sustained in service. The present concept employs an array of gas insulated solid wall aluminum coaxi...
The initial design and evaluation of a 5 kW arcjet power electronics breadboard which as been integr...
The effect of nozzle configuration on the operating characteristics of a low power dc arcjet thruste...
Present practices in lightning protection of aircraft deal primarily with the direct effects of ligh...
The SP-100 program was established in 1983 by DOD, DOE, and NASA as a joint program to develop the t...
The ion thruster is one of several forms of space electric propulsion being considered for use on fu...
The goal of the triagency SP-100 Program is to develop long-lived, compact, lightweight, survivable ...
A 260 kW magnetoplasmadynamic (MPD) thruster test facility was assembled and used to characterize th...
The performance of the power system on the solar mesosphere explorer (SME) since launch is discussed...
Studies have shown that use of solar dynamic (SD) power for the growth eras of the Space Station Fre...
Solar Photo Voltaic (PV) and thermal dynamic power systems for application to selected Low Earth Orb...
Thermal energy storage (TES) enables a solar dynamic system to deliver constant electric power throu...
A nuclear space power system the SP-100 is being developed for future missions where large amounts o...
Since 1984, NASA Lewis Research Center was developing high power, high frequency space power compone...
The engineering model resistojet intended for altitude maintenance onboard the space station was tes...
Research and pilot line production efforts directed towards the fabrication of high efficiency ultra...
The initial design and evaluation of a 5 kW arcjet power electronics breadboard which as been integr...
The effect of nozzle configuration on the operating characteristics of a low power dc arcjet thruste...
Present practices in lightning protection of aircraft deal primarily with the direct effects of ligh...
The SP-100 program was established in 1983 by DOD, DOE, and NASA as a joint program to develop the t...
The ion thruster is one of several forms of space electric propulsion being considered for use on fu...
The goal of the triagency SP-100 Program is to develop long-lived, compact, lightweight, survivable ...
A 260 kW magnetoplasmadynamic (MPD) thruster test facility was assembled and used to characterize th...
The performance of the power system on the solar mesosphere explorer (SME) since launch is discussed...
Studies have shown that use of solar dynamic (SD) power for the growth eras of the Space Station Fre...
Solar Photo Voltaic (PV) and thermal dynamic power systems for application to selected Low Earth Orb...
Thermal energy storage (TES) enables a solar dynamic system to deliver constant electric power throu...
A nuclear space power system the SP-100 is being developed for future missions where large amounts o...
Since 1984, NASA Lewis Research Center was developing high power, high frequency space power compone...
The engineering model resistojet intended for altitude maintenance onboard the space station was tes...
Research and pilot line production efforts directed towards the fabrication of high efficiency ultra...
The initial design and evaluation of a 5 kW arcjet power electronics breadboard which as been integr...
The effect of nozzle configuration on the operating characteristics of a low power dc arcjet thruste...
Present practices in lightning protection of aircraft deal primarily with the direct effects of ligh...