Auroral charging of spacecraft is an important class of space weather impacts on technological systems in low Earth orbit. In order for space weather models to accurately specify auroral charging environments, they must provide the appropriate plasma environment characteristics responsible for charging. Improvements in operational space weather prediction capabilities relevant to charging must be tested against charging observations.
Topics: Minow, Joseph I., NASA Langley Research Center
No abstract available
Topics: Air Force Research Lab., Bolling Air Force Base, Ferguson, Dale C., Minow, Joseph I., NASA Langley...
No abstract available
Topics: Altstatt, Richard L., Jacobs Engineering Group, Inc., Minow, Joseph I., NASA Marshall Space Flight...
(1) High energy (>100keV) electrons penetrate spacecraft walls and accumulate in dielectrics or isolated conductors; (2) Threat environment is energetic electrons with sufficient flux to charge circuit boards, cable insulation, and ungrounded metal faster than charge can dissipate; (3) Accumulating charge density generates electric fields in excess of material breakdown strenght resulting in electrostatic discharge; and (4) System impact is material damage, discharge currents inside of...
Topics: NASA Technical Reports Server (NTRS), INTERNAL ENERGY, TERRESTRIAL RADIATION, OUTER RADIATION BELT,...
No abstract available
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, DAMAGE, CONTAMINANTS, SOLAR ARRAYS,...
The awareness of potentially significant impacts of space weather on spaceand ground ]based technological systems has generated a strong desire in many sectors of government and industry to effectively transform knowledge and understanding of the variable space environment into useful tools and applications for use by those entities responsible for systems that may be vulnerable to space weather impacts. Essentially, effectively transitioning science knowledge to useful applications relevant to...
Topics: NASA Technical Reports Server (NTRS), SPACE WEATHER, AEROSPACE ENVIRONMENTS, AURORAS, INTERNATIONAL...
The emission of secondary electrons from surfaces exposed to the space plasma and radiation environment is a process of great importance to space system engineering design and operations. A spacecraft will collect charge until it reaches an equilibrium potential gov,erned by the balance of incoming electron and ion currents from the space environment with outgoing secondary, backscattered, and photoelectron currents. Laboratory measurements of secondary electron yields are an important...
Topics: NASA Technical Reports Server (NTRS), ELECTRON EMISSION, SPACE EXPLORATION, ION CURRENTS, SPACE...
Evaluating spacecraft charging behavior of a vehicle in the space environment requires knowledge of the material properties relevant to the charging process. Implementing surface and internal charging models requires a user to specify a number of material electrical properties including electrical resistivity parameters (dark and radiation induced), dielectric constant, secondary electron yields, photoemission yields, and breakdown strength in order to correctly evaluate the electric discharge...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, SENSITIVITY, ELECTRIC FIELDS, ELECTRICAL...
This slide presentation reviews information on space radiation environments important to magnetospheric missions including trapped radiation, solar particle events, cosmic rays, and solar winds. It also includes information about ion penetration of the magnetosphere, galactic cosmic rays, solar particle environments, CRRES internal discharge monitor, surface charging and radiation effects.
Topics: NASA Technical Reports Server (NTRS), COSMIC RAYS, SOLAR FLARES, SOLAR CORPUSCULAR RADIATION,...
It has been well established that polar orbiting satellites can see mild to severe charging levels during solar minimum conditions (Frooninckx and Sojka, 1992, Anderson and Koons, 1996, Anderson, 2012). However, spacecraft operations during solar maximum cannot be considered safe from auroral charging. Recently, we have seen examples of high level charging during the recent approach to solar maximum. We present here a survey of charging events seen by the Defense Meteorological Satellite...
Topics: NASA Technical Reports Server (NTRS), DMSP SATELLITES, SOLAR CYCLES, SOLAR MAXIMUM MISSION,...
No abstract available
Topics: NASA Technical Reports Server (NTRS), SURFACE ENERGY, ELECTRIC POTENTIAL, ELECTRICAL MEASUREMENT,...
It has been well established that polar orbiting satellites can experience mild to severe auroral charging levels (on the order of a few hundred volts to few kilovolts negative frame potentials) during solar minimum conditions (Frooninckx and Sojka, 1992; Anderson and Koons, 1996; Anderson, 2012). These same studies have shown a strong reduction in charging during the rising and declining phases of the past few solar cycles with a nearly complete suppression of auroral charging at solar...
Topics: NASA Technical Reports Server (NTRS), SOLAR CYCLES, AURORAS, SOLAR ACTIVITY, ENERGETIC PARTICLES,...
It has been well established that POLAR orbiting satellites can see mild to severe charging levels during solar minimum conditions (Frooninckx and Sojka, 1992, Anderson and Koons, 1996, Anderson, 2012). However, spacecraft operations during solar maximum cannot be considered safe from auroral charging. Recently, we have seen examples of high level charging during the recent approach to solar maximum. We present here a survey of charging events seen by the Defense Meteorological Satellite...
Topics: NASA Technical Reports Server (NTRS), DMSP SATELLITES, SOLAR CYCLES, SOLAR MAXIMUM MISSION,...
Today's presentation is a short tutorial on auroral charging of spacecraft and the characteristics of the space plasma environment that are required to predict charging.
Topics: NASA Technical Reports Server (NTRS), AURORAS, FLUX DENSITY, IONS, ELECTRONS, PHOTOELECTRIC...
No abstract available
Topics: NASA Technical Reports Server (NTRS), INTERNATIONAL SPACE STATION, SPACECRAFT CHARGING, EXTERNAL...
Materials exposed to the space plasma environment charge to a net potential relative to the ambient plasma. The charging process is due to differential currents to the material surface that results in a net surface charge density. While this process is termed "spacecraft surface charging" when applied to aerospace hardware, it also applies to the surfaces of astronomical objects in direct contact with the space plasma environment including a number of planetary bodies, asteroids, and...
Topics: NASA Technical Reports Server (NTRS), AEROSPACE ENVIRONMENTS, SPACE PLASMAS, EXPOSURE, SURFACE...
During its first five months of operations, the Langmuir Probe on the Floating Potential Probe (FPP) obtained data on ionospheric electron densities and temperatures in the ISS orbit. In this paper, the algorithms for data reduction are presented, and comparisons are made of FPP data with ground-based ionosonde and Incoherent Scattering Radar (ISR) results. Implications for ISS operations are detailed, and the need for a permanent FPP on ISS is examined.
Topics: NASA Technical Reports Server (NTRS), ELECTROSTATIC PROBES, IONOSPHERIC TEMPERATURE, ELECTRON...
The International Space Station (ISS) space environments community utilizes near real time space weather data to support a variety of ISS engineering and science activities. The team has operated the Floating Potential Measurement Unit (FPMU) suite of plasma instruments (two Langmuir probes, a floating potential probe, and a plasma impedance probe) on ISS since 2006 to obtain in-situ measurements of plasma density and temperature along the ISS orbit and variations in ISS frame potential due to...
Topics: NASA Technical Reports Server (NTRS), INTERNATIONAL SPACE STATION, SPACE WEATHER, GEOMAGNETISM,...
This document includes a viewgraph presentation plus the full paper presented at the conference. The Living With a Star Ion Flux Model (IFM) is a radiation environment risk mitigation tool that provides magnetospheric ion flux values for varying geomagnetic disturbance levels in the geospace environment. IFM incorporates flux observations from the Polar and Geotail spacecraft in a single statistical flux model. IFM is an engineering environment model which predicts the proton flux not only in...
Topics: NASA Technical Reports Server (NTRS), FLUX (RATE), GEOMAGNETIC TAIL, PROTONS, SOLAR WIND, MODELS,...
The International Space Station (ISS) maintains an altitude typically between 300 km and 400 km in low Earth orbit (LEO) which itself is situated in the Earth's ionosphere. The ionosphere is a region of partially ionized gas (plasma) formed by the photoionization of neutral atoms and molecules in the upper atmosphere of Earth. It is important to understand what electron density the spacecraft is/will be operating in because the ionized gas along the ISS orbit interacts with the electrical power...
Topics: NASA Technical Reports Server (NTRS), EXTRAVEHICULAR ACTIVITY, INTERNATIONAL SPACE STATION,...
The International Space Station (ISS) space environments community utilizes near real time space weather data to support a variety of ISS engineering and science activities. The team has operated the Floating Potential Measurement Unit (FPMU) suite of plasma instruments (two Langmuir probes, a floating potential probe, and a plasma impedance probe) on ISS since 2006 to obtain in-situ measurements of plasma density and temperature along the ISS orbit and variations in ISS frame potential due to...
Topics: NASA Technical Reports Server (NTRS), INTERNATIONAL SPACE STATION, SPACE WEATHER, GEOMAGNETISM,...
Today’s presentation describes preliminary results from a study of extreme auroral charging in low Earth orbit. Goal of study is to document characteristics of auroral charging events of importance to spacecraft design, operations, and anomaly investigations.
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, SPACECRAFT DESIGN, LOW EARTH ORBITS,...
Solar wind composition is dominated by hydrogen (approx.96%) and helium (approx.3 to 4%) with a minor fraction (less than or equal to 1%) of heavy ions. Hydrogen (helium) ions impact spacecraft surfaces with energies from 0.5 to 5 keV (1.8 to 21 keV) due to variations in solar wind velocity from 300 km/s to 1000 km/sec with extremes of a few 10 s keV during periods of extremely high solar wind velocity exceeding 1000 km/sec. Mean impact energies are typically on the order of approximately 1 keV...
Topics: NASA Technical Reports Server (NTRS), SOLAR WIND, HELIUM, HYDROGEN, HYDROGEN IONS, HELIUM IONS, ION...
The Genesis spacecraft launched on 8 August 2001 sampled solar wind environments at L1 from 2001 to 2004. After the Science Capsule door was opened, numerous foils and samples were exposed to the various solar wind environments during periods including slow solar wind from the streamer belts, fast solar wind flows from coronal holes, and coronal mass ejections. The Survey and Examination of Eroded Returned Surfaces (SEERS) program led by NASA's Space Environments and Effects program had...
Topics: NASA Technical Reports Server (NTRS), AEROSPACE ENVIRONMENTS, GENESIS MISSION, CORONAL MASS...
The Natural Environments Branch at Marshall Space Flight Center is integral in developing, maintaining, and investigating NASA missions such as Space Launch Systems (SLS), currently under development, as well as many NASA and other agency satellite missions. We present the space environment capabilities of the Natural Environments Branch at MSFC. These in-house capabilities include model development, analysis of space and terrestrial related data, spacecraft charging anomaly investigations,...
Topics: NASA Technical Reports Server (NTRS), AEROSPACE ENVIRONMENTS, SPACECRAFT LAUNCHING, SYSTEMS...
Robotic and manned spacecraft from the Apollo era demonstrated that the lunar surface in daylight will charge to positive potentials of a few tens of volts because the photoelectron current dominates the charging process. In contrast, potentials of the lunar surface in darkness which were predicted to be on the order of a hundred volts negative in the Apollo era have been shown more recently to reach values of a few hundred volts negative with extremes on the order of a few kilovolts. The...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, LUNAR ORBITS, AEROSPACE ENVIRONMENTS,...
Spacecraft charging occurs when charged particles from the surrounding space plasma environment contact a spacecraft and unequal charging currents result in a net charge density accumulation on or in spacecraft materials. Charging becomes a threat when differential potentials between two points on the spacecraft or between the spacecraft and the ambient space environment build to the level that electric fields associated with the potentials exceed the electric breakdown strength of the...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, AEROSPACE ENVIRONMENTS, CHARGED...
The highest level spacecraft charging observed in low Earth orbit (LEO) occurs when spacecraft are exposed to energetic auroral electrons. Since auroral charging has been identified as a mechanism responsible for on-orbit anomalies and even possible satellite failures it is important to consider extreme auroral charging events as design and test environments for spacecraft to be used in high inclination LEO orbits. This paper will report on studies of extreme auroral charging events using data...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, ELECTRIC POTENTIAL, AURORAS, GEOMAGNETIC...
Spacecraft in low altitude, high inclination (including sun-synchronous) orbits are widely used for remote sensing of the Earth's land surface and oceans, monitoring weather and climate, communications, scientific studies of the upper atmosphere and ionosphere, and a variety of other scientific, commercial, and military applications. These systems episodically charge to frame potentials in the kilovolt range when exposed to space weather environments characterized by a high flux of energetic...
Topics: NASA Technical Reports Server (NTRS), AEROSPACE ENVIRONMENTS, EARTH SURFACE, LOW EARTH ORBITS,...
Internal charging is a risk to spacecraft in energetic electron environments. DICTAT, NU MIT computational codes are the most widely used engineering tools for evaluating internal charging of insulator materials exposed to these environments. Engineering tools are designed for rapid evaluation of ESD threats, but there is a need for more physics based models for investigating the science of materials interactions with energetic electron environments. Current tools are limited by the physics...
Topics: NASA Technical Reports Server (NTRS), ELECTRIC FIELDS, EXTRATERRESTRIAL RADIATION, ELECTROSTATIC...
Spacecraft in low altitude, high inclination (including sun -synchronous) orbits are widely used for remote sensing of the Earth fs land surface and oceans, monitoring weather and climate, communications, scientific studies of the upper atmosphere and ionosphere, and a variety of other scientific, commercial, and military applications. These systems episodically charge to frame potentials in the kilovolt range when exposed to space weather environments characterized by a high flux of energetic...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, AEROSPACE ENVIRONMENTS, GEOSYNCHRONOUS...
Orbiting approximately 400 km above the Earth, the International Space Station (ISS) is a unique research laboratory used to conduct ground-breaking science experiments in space. The ISS has eight Solar Array Wings (SAW), and each wing is 11.7 meters wide and 35.1 meters long. The SAWs are controlled individually to maximize power output, minimize stress to the ISS structure, and minimize interference with other ISS operations such as vehicle dockings and Extra-Vehicular Activities (EVA). The...
Topics: NASA Technical Reports Server (NTRS), ELECTRIC POTENTIAL, EXTRAVEHICULAR ACTIVITY, SPACE PLASMAS,...
The sunlit lunar surface charges to positive potentials with mean values of a few tens of volts where photoelectron currents dominate the charging process. In contrast, surfaces in darkness may charge to negative potentials on the order of a few hundred volts when the charging process is dominated by hot electron populations in the absence of solar photons. Recently, observations of electron beams measured by instruments on spacecraft in low lunar orbit have been interpreted as evidence for...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, SPACE WEATHER, LUNAR ENVIRONMENT,...
A Solar Sail Radiation Environment (SSRE) model has been developed for defining charged particle environments over an energy range from 0.01 keV to 1 MeV for hydrogen ions, helium ions, and electrons. The SSRE model provides the free field charged particle environment required for characterizing energy deposition per unit mass, charge deposition, and dose rate dependent conductivity processes required to evaluate radiation dose and internal (bulk) charging processes in the solar sail membrane...
Topics: NASA Technical Reports Server (NTRS), ENVIRONMENT MODELS, SOLAR SAILS, CHARGING, INTERPLANETARY...
This slide presentation reviews a method to analyze the plasma data that is reported on board the International Space station (ISS). The Floating Potential Measurement Unit (FPMU), the role of which is to obtain floating potential and ionosphere plasma measurements for validation of the ISS charging model, assess photo voltaic array variability and interpreting IRI predictions, is composed of four probes: Floating Potential Probe (FPP), Wide-sweep Langmuir Probe (WLP), Narrow-sweep Langmuir...
Topics: NASA Technical Reports Server (NTRS), ELECTROSTATIC PROBES, IMPEDANCE PROBES, PLASMA PROBES, DATA...
The International Space Station (ISS) continues to be a world-class space research laboratory after over 15 years of operations, and it has proven to be a fantastic resource for observing spacecraft floating potential variations related to high voltage solar array operations in Low Earth Orbit (LEO). Measurements of the ionospheric electron density and temperature along the ISS orbit and variations in the ISS floating potential are obtained from the Floating Potential Measurement Unit (FPMU)....
Topics: Alabama Univ., Krause, Linda Habash, Minow, Joseph I., NASA Marshall Space Flight Center,...
No abstract available
Topics: Alabama Univ., Krause, Linda Habash, Minow, Joseph I., NASA Marshall Space Flight Center,...
The design estimate for the materials for the International Space Station (ISS) specified in SSP 30512 was a conservative estimate. The environment dose was over estimated. The materials originally qualified for approximately 10-15 years are anticipated to be acceptable for periods of up to 20-30 years based on SSP-30512 or 40-60 years based on 2x SSP-30512. This viewgraph presentation shows charts and graphs that review the altitude, the solar minimum and maximum, and the radiation exposure of...
Topics: NASA Technical Reports Server (NTRS), RADIATION DOSAGE, SOLAR ACTIVITY EFFECTS, RADIATION EFFECTS,...
The 700 km x 5.8 Re orbit of the two Van Allen Probes spacecraft provide a unique opportunity to investigate spacecraft charging in geostationary transfer orbits. We use records from the Helium Oxygen Proton Electron (HOPE) plasma spectrometer to identify candidate surface charging events based on the "ion line" charging signature in the ion records. We summarize the energetic particle environment and the conditions necessary for charging to occur in this environment. We discuss the...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, EARTH ORBITAL ENVIRONMENTS, TRANSFER...
Spacecraft in low altitude, high inclination (including sun-synchronous) orbits are widely used for remote sensing of the Earth s land surface and oceans, monitoring weather and climate, communications, scientific studies of the upper atmosphere and ionosphere, and a variety of other scientific, commercial, and military applications. These systems are episodically exposed to environments characterized by a high flux of energetic (approx.1 to 10 s kilovolt) electrons in regions of very low...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, GEOSYNCHRONOUS ORBITS, AEROSPACE...
Low Earth orbit is usually considered a relatively benign environment for internal charging threats due to the low flux of penetrating electrons with energies of a few MeV that are encountered over an orbit. There are configurations, however, where insulators and ungrounded conductors used on the outside of a spacecraft hull may charge when exposed to much lower energy electrons of some 100's keV in a process that is better characterized as internal charging than surface charging. For example,...
Topics: NASA Technical Reports Server (NTRS), FLUX DENSITY, RADIATION SHIELDING, ELECTRONS, CONDUCTORS,...
Spacecraft charging on the International Space Station (ISS) is caused by a complex mix of the low Earth orbit plasma environment, space weather events, operations of the high voltage solar arrays, and changes in the ISS configuration and orbit parameters. Measurements of the ionospheric electron density and temperature along the ISS orbit and variations in the ISS electric potential are obtained from the Floating Potential Measurement Unit (FPMU) suite of four plasma instruments (two Langmuir...
Topics: NASA Technical Reports Server (NTRS), IONOSPHERIC ELECTRON DENSITY, INTERNATIONAL SPACE STATION,...
Electrostatic potential variations of the International Space Station (ISS) relative to the space plasma environment are dominated by interaction of the negatively grounded 160 volt US photovoltaic power system with the plasma environment in sunlight and inductive potential variations across the ISS structure generated by motion of the vehicle across the Earth's magnetic field. Auroral charging is also a source of potential variations because the 51.6? orbital inclination of ISS takes the...
Topics: NASA Technical Reports Server (NTRS), AURORAS, INTERNATIONAL SPACE STATION, MAGNETIC STORMS, SPACE...
The characterization of the electromagnetic interaction for a solar sail in the solar wind environment and identification of viable charging mitigation strategies are critical solar sail mission design task. Spacecraft charging has important implications both for science applications and for lifetime and reliability issues of sail propulsion systems. To that end, surface charging calculations of a candidate 150-meter-class solar sail spacecraft for the 0.5 AU solar polar and 1.0 AU L1 solar...
Topics: NASA Technical Reports Server (NTRS), SOLAR SAILS, SPACECRAFT CHARGING, SPACE MISSIONS, SPACECRAFT...
The Vision for Space Exploration outlines NASA's development of a new generation of human-rated launch vehicles to replace the Space Shuttle and an architecture for exploring the Moon and Mars. The system--developed by the Constellation Program--includes a near term (approx. 2014) capability to provide crew and cargo service to the International Space Station after the Shuttle is retired in 2010 and a human return to the Moon no later than 2020. Constellation vehicles and systems will...
Topics: NASA Technical Reports Server (NTRS), HELIOSPHERE, SPACE EXPLORATION, NASA SPACE PROGRAMS,...
The near circular, 51.6deg inclination orbit of the International Space Station (ISS) is maintained within an altitude range of approximately 300 km to 400 km providing an ideal platform for conducting in-situ studies of space weather effects on the mid and low-latitude F-2 region ionosphere. The Floating Potential Measurement Unit (FPMU) is a suite of instruments installed on the ISS in August 2006 which includes a Floating Potential Probe (FPP), a Plasma Impedance Probe (PIP), a Wide-sweep...
Topics: NASA Technical Reports Server (NTRS), CIRCULAR ORBITS, INTERNATIONAL SPACE STATION, SOLAR ARRAYS,...
Spectral models of solar particle events and trapped radiation belts are necessary for the design requirements of total ionizing radiation dose, single event effects, and spacecraft charging. Space radiation and plasma environment specifications for hardware design are necessarily conservative to assure system robustness for a wide range of space environments.
Topics: NASA Technical Reports Server (NTRS), CONSTELLATION PROGRAM, SPACECRAFT CHARGING, RADIATION...
Space systems interacting with the space plasma environment charge to potentials of a few tens of volts positive in interplanetary space or on the lunar surface in daylight, a few hundred volts negative in the dark lunar plasma wake and in some regions of the Earth s radiation belts, and to multiple kilovolt negative potentials for worst case conditions in the Earth s magnetosphere near geostationary orbit. Good design practices are required to assure that space systems operate successfully in...
Topics: NASA Technical Reports Server (NTRS), SPACECRAFT CHARGING, PLASMA POTENTIALS, RADIATION BELTS,...
The plasma environment encountered by the Next Generation Space Telescope satellite in a halo orbit about L2 can include the Earth's magnetotail and magnetosheath in addition to the solar wind depending on the orbital radius chosen for the mission. Analysis of plasma environment impacts on the satellite requires knowledge of the average and extreme plasma characteristics to assess the magnitude of spacecraft charging and materials degradation expected for the mission lifetime. This report...
Topics: NASA Technical Reports Server (NTRS), PLASMAS (PHYSICS), GEOMAGNETIC TAIL, MAGNETOSHEATH, SOLAR...
No abstract available
Topics: NASA Technical Reports Server (NTRS), AURORAL ZONES, SPACE WEATHER, DMSP SATELLITES, SPACECRAFT...
