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Proceedings of the Spacecraft Charging Technology ConferenceOver 50 papers from the spacecraft charging conference are included on subjects such as: (1) geosynchronous plasma environment, (2) spacecraft modeling, (3) spacecraft materials characterization, (4) spacecraft materials development, and (5) satellite design and test.
Document ID
19780002186
Acquisition Source
Legacy CDMS
Document Type
Conference Proceedings
Authors
Pike, C. P. (NASA Lewis Research Center Cleveland, OH, United States)
Lovell, R. R. (NASA Lewis Research Center Cleveland, OH, United States)
Date Acquired
September 3, 2013
Publication Date
February 24, 1977
Subject Category
Astronautics (General)
Report/Patent Number
AFSG-364
AFGL-TR-77-0051
NASA-TM-X-73537
Report Number: AFSG-364
Report Number: AFGL-TR-77-0051
Report Number: NASA-TM-X-73537
Accession Number
78N10129
Funding Number(s)
PROJECT: AF PROJ. 7661
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

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IDRelationTitle19780002187WorkProceedings of the Spacecraft Charging Technology Conference: Executive Summary19780002188WorkSpacecraft Charging Technology Conference, P 78-2, overview19780002189WorkThe plasma environment at geosynchronous orbit19780002190WorkComposition of the hot plasma near geosynchronous altitude19780002191WorkInjun 5 observations of vehicle potential fluctuations at 2500 km19780002192WorkPreliminary report on the CTS transient event counter performance through the 1976 spring eclipse season19780002193WorkActive control of spacecraft charging on ATS-5 and ATS-619780002194WorkActive control of potential of the geosynchronous satellites ATS-5 and ATS-619780002195WorkPlasma distribution and spacecraft charging modeling near Jupiter19780002196WorkActive spacecraft potential control system selection for the Jupiter orbiter with probe mission19780002197WorkNuclear burst plasma injection into the magnetosphere and resulting spacecraft charging19780002198WorkElectrification of the proof mass of a drag-free or accelerometric satellite19780002199WorkAnalysis of penumbral eclipse data19780002200WorkThe multiple applications of electrons in space19780002201WorkModeling of spacecraft charging19780002202WorkA charging model for three-axis stabilized spacecraft19780002203WorkInduced charging of shuttle orbiter by high electron-beam currents19780002204WorkAn altitude-dependent spacecraft charging model19780002205WorkPioneer Venus spacecraft charging model19780002206WorkNumerical simulation of spacecraft charging phenomena19780002207WorkDynamic modeling of spacecraft in a collisionless plasma19780002208WorkCalculation of sheath and wake structure about a pillbox-shaped spacecraft in a flowing plasma19780002209WorkPrediction of large negative shaded-side spacecraft potentials19780002210WorkA simulation model of time-dependent plasma-spacecraft interactions19780002211WorkPhotoelectric charging of partially sunlit dielectric surfaces in space19780002212WorkThe Lewis Research Center geomagnetic substorm simulation facility19780002213WorkTesting of typical spacecraft materials in a simulated substorm environment19780002206WorkNumerical simulation of spacecraft charging phenomena19780002214WorkCharging characteristics of materials: Comparison of experimental results with simple analytical models19780002215WorkInvestigation of a CTS solar cell test patch under simulated geomagnetic substorm charging conditions19780002216WorkCharge distributions near metal-dielectric interfaces before and after dielectric surface flashover19780002217WorkSurface micro-discharges on spacecraft dielectrics19780002218WorkSurge current and electron swarm tunnel tests of thermal blanket and ground strap materials19780002219WorkA rugged electron/ion source for spacecraft charging experiments19780002220WorkConductive spacecraft materials development program19780002221WorkResults of literature search on dielectric properties and electron interaction phenomena related to spacecraft charging19780002222WorkElectrically Conductive Paints for Satellites19780002223WorkFormulation of electrically conductive, thermal-control coatings19780002224WorkMaterials and techniques for spacecraft static charge control19780002225WorkSecondary emission conductivity of high purity silica fabric19780002226WorkInvestigation of conductive thermal control coatings by a contactless method in vacuo19780002227WorkThe effects of the geosynchronous energetic particle radiation environment on spacecraft charging phenomena19780002228WorkSystem aspects of spacecraft charging19780002229WorkTransient response measurements on a satellite system19780002230WorkProvisional specification for satellite time in a geomagnetic environment19780002231WorkDevelopment of environmental charging effect monitors for operational satellites19780002232WorkViking and STP P78-2 electrostatic charging designs and testing19780002233WorkDesign, construction and testing of the Communications Technology Satellite protection against spacecraft charging19780002234WorkCommon approach to solving SGEMP, DEMP, and ESD survivability19780002235WorkPlasma charging testing of communication satellites19780002236WorkQualification model spacecraft tests for DEMP, SGEMP, and ESD effects19780002237WorkSpacecraft charging anomalies on the DSCS II, launch 2 satellites19780002238WorkSpace environmental effects on the SKYNET 2B spacecraft19780002239WorkRCA Satcom 3-Axis spacecraft experience at geosynchronous altitude19780002231WorkDevelopment of environmental charging effect monitors for operational satellites19780002239WorkRCA Satcom 3-Axis spacecraft experience at geosynchronous altitude19780002222WorkElectrically Conductive Paints for Satellites19780002190WorkComposition of the hot plasma near geosynchronous altitude19780002195WorkPlasma distribution and spacecraft charging modeling near Jupiter19780002218WorkSurge current and electron swarm tunnel tests of thermal blanket and ground strap materials19780002203WorkInduced charging of shuttle orbiter by high electron-beam currents19780002236WorkQualification model spacecraft tests for DEMP, SGEMP, and ESD effects19780002189WorkThe plasma environment at geosynchronous orbit19780002216WorkCharge distributions near metal-dielectric interfaces before and after dielectric surface flashover19780002232WorkViking and STP P78-2 electrostatic charging designs and testing19780002194WorkActive control of potential of the geosynchronous satellites ATS-5 and ATS-619780002188WorkSpacecraft Charging Technology Conference, P 78-2, overview19780002214WorkCharging characteristics of materials: Comparison of experimental results with simple analytical models19780002228WorkSystem aspects of spacecraft charging19780002217WorkSurface micro-discharges on spacecraft dielectrics19780002204WorkAn altitude-dependent spacecraft charging model19780002197WorkNuclear burst plasma injection into the magnetosphere and resulting spacecraft charging19780002215WorkInvestigation of a CTS solar cell test patch under simulated geomagnetic substorm charging conditions19780002223WorkFormulation of electrically conductive, thermal-control coatings19780002192WorkPreliminary report on the CTS transient event counter performance through the 1976 spring eclipse season19780002187WorkProceedings of the Spacecraft Charging Technology Conference: Executive Summary19780002237WorkSpacecraft charging anomalies on the DSCS II, launch 2 satellites19780002208WorkCalculation of sheath and wake structure about a pillbox-shaped spacecraft in a flowing plasma19780002198WorkElectrification of the proof mass of a drag-free or accelerometric satellite19780002225WorkSecondary emission conductivity of high purity silica fabric19780002230WorkProvisional specification for satellite time in a geomagnetic environment19780002209WorkPrediction of large negative shaded-side spacecraft potentials19780002207WorkDynamic modeling of spacecraft in a collisionless plasma19780002238WorkSpace environmental effects on the SKYNET 2B spacecraft19780002199WorkAnalysis of penumbral eclipse data19780002205WorkPioneer Venus spacecraft charging model19780002227WorkThe effects of the geosynchronous energetic particle radiation environment on spacecraft charging phenomena19780002202WorkA charging model for three-axis stabilized spacecraft19780002229WorkTransient response measurements on a satellite system19780002226WorkInvestigation of conductive thermal control coatings by a contactless method in vacuo19780002220WorkConductive spacecraft materials development program19780002191WorkInjun 5 observations of vehicle potential fluctuations at 2500 km19780002219WorkA rugged electron/ion source for spacecraft charging experiments19780002193WorkActive control of spacecraft charging on ATS-5 and ATS-619780002212WorkThe Lewis Research Center geomagnetic substorm simulation facility19780002200WorkThe multiple applications of electrons in space19780002211WorkPhotoelectric charging of partially sunlit dielectric surfaces in space19780002196WorkActive spacecraft potential control system selection for the Jupiter orbiter with probe mission19780002201WorkModeling of spacecraft charging19780002210WorkA simulation model of time-dependent plasma-spacecraft interactions19780002235WorkPlasma charging testing of communication satellites19780002221WorkResults of literature search on dielectric properties and electron interaction phenomena related to spacecraft charging19780002224WorkMaterials and techniques for spacecraft static charge control19780002234WorkCommon approach to solving SGEMP, DEMP, and ESD survivability19780002213WorkTesting of typical spacecraft materials in a simulated substorm environment19780002233WorkDesign, construction and testing of the Communications Technology Satellite protection against spacecraft charging
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