Proceedings of the Second Workshop on Voltage Breakdown in Electronic Equipment at Low Air PressureThe Second Workshop on Voltage Breakdown in Electronic Equipment at Low Air Pressure was sponsored by the Jet Propulsion Laboratory, Pasadena, California.
It has been three and one-half years since the convening of the first workshop on voltage breakdown. In this interval, gains are evidenced in the progress and sophistication in solving voltage breakdown problems affecting electronic equipment operating at high altitudes or other low air pressure environments. Although space applications predominate the area of concern, other projects such as the SST are becoming increasingly involved with voltage breakdown.
High-voltage breakdown in spacecraft continues; however, the incidences of occurrence appear to have decreased in spite of an increase in the number of missions flown. This, it is felt, is due to many project managers now requiring all equipment with voltage in excess of 270-V peak to be designed to operate in the critical pressure region without damage, even though its normal functional environment is sea level pressure and the hard vacuum of space. In addition, designers are becoming more aware of the principle of good high-voltage design by selecting void-free components, proper spacing of conductors, isolating high-voltage circuitry from lower voltage areas, etc. The consensus seems to be that the slight increase in cost to achieve a provable corona-free design is more than offset by the increase in confidence that the equipment will survive accidental loss of vacuum during high-vacuum tests, inadvertent turn on while passing through the critical air-pressure region of earth after launch or outgassing in flight pressurizing the enclosure into the critical pressure region.
Document ID
19700022975
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
E. R. Bunker, Jr. (Jet Propulsion Lab La Cañada Flintridge, California, United States)
Date Acquired
September 2, 2013
Publication Date
March 5, 1969
Publication Information
Publication: Proceedings of the Second Workshop on Voltage Breakdown in Electronic Equipment at Low Air Pressure
IDRelationTitle19700022976WorkA study of voltage breakdown in spacecraft systems from test and flight experience19700022977WorkSome observations of corona breakdown on various antenna types in simulated planetary atmospheres19700022978WorkVHF breakdown on a Nike-Cajun rocket19700022979WorkDevelopment of packaging techniques for an amplitron and power supply19700022980WorkDevelopment of electronographic image converters for far-ultraviolet space astronomy applications19700022981WorkLow-voltage breakdown in electronic equipment when exposed to a partial-pressure nitrogen environment containing water vapor19700022982WorkThe Bendix OAO star tracker high-voltage system and its design considerations19700022983WorkA vented high-voltage system for satellite applications19700022984WorkOpen construction magnetic components for the SERT 2 power conditioner19700022985WorkDesign considerations for corona-free high- voltage transformers19700022986WorkHigh-voltage packaging investigations in the advanced technology group19700022987WorkCorona evaluation of spacecraft wires and connectors19700022988WorkLow-level corona detectors19700022989WorkThe dc voltage breakdown processes and external detection techniques19700022990WorkTesting of high-voltage spacecraft systems in a simulated ionospheric plasma19700022991WorkRocket-exhaust initiation of conduction in connectors at altitude19700022992WorkHigh-voltage breakdown in an OSO-4 pointed experiment19700022993WorkThe prevention of electrical breakdown in spacecraft19700022994WorkThe influence of gas velocity on the breakdown potential of argon, helium, and nitrogen19700022995WorkBreakdown studies for possible atmospheres on Mars and Venus19700022997WorkReduction of gas-discharge breakdown thresholds in the ionosphere due to multipacting19700022998WorkThe effects of outgassing materials on voltage breakdown19700022976WorkA study of voltage breakdown in spacecraft systems from test and flight experience19700022977WorkSome observations of corona breakdown on various antenna types in simulated planetary atmospheres19700022978WorkVHF breakdown on a Nike-Cajun rocket19700022979WorkDevelopment of packaging techniques for an amplitron and power supply19700022980WorkDevelopment of electronographic image converters for far-ultraviolet space astronomy applications19700022981WorkLow-voltage breakdown in electronic equipment when exposed to a partial-pressure nitrogen environment containing water vapor19700022982WorkThe Bendix OAO star tracker high-voltage system and its design considerations19700022983WorkA vented high-voltage system for satellite applications19700022984WorkOpen construction magnetic components for the SERT 2 power conditioner19700022985WorkDesign considerations for corona-free high- voltage transformers19700022986WorkHigh-voltage packaging investigations in the advanced technology group19700022987WorkCorona evaluation of spacecraft wires and connectors19700022988WorkLow-level corona detectors19700022989WorkThe dc voltage breakdown processes and external detection techniques19700022990WorkTesting of high-voltage spacecraft systems in a simulated ionospheric plasma19700022991WorkRocket-exhaust initiation of conduction in connectors at altitude19700022992WorkHigh-voltage breakdown in an OSO-4 pointed experiment19700022993WorkThe prevention of electrical breakdown in spacecraft19700022994WorkThe influence of gas velocity on the breakdown potential of argon, helium, and nitrogen19700022995WorkBreakdown studies for possible atmospheres on Mars and Venus19700022997WorkReduction of gas-discharge breakdown thresholds in the ionosphere due to multipacting19700022998WorkThe effects of outgassing materials on voltage breakdown