Engineering topics
Brinza, D.
Publications and source records attributed to Brinza, D..
Europa Clipper: Selection and Characterization of Electronic Parts and Materials for the Europa Clipper Mission
No abstract available
Low cost environmental sensors for Spaceflight : NMP Space Environmental Monitor (SEM) requirements
An outstanding problem in spaceflight is the lack of adequate sensors for monitoring the space environment and its effects on engineering systems. By adequate, we mean low cost in terms of mission impact (e.g., low price, low mass/size, low power, low data rate, and low design impact). The New Millennium Program (NMP) is investigating the development of such a low-cost Space Environmental Monitor (SEM) package for inclusion on its technology validation flights. This effort follows from the need by NMP to characterize the space environment during testing so that potential users can extrapolate the test results to end-use conditions. The immediate objective of this effort is to develop a small diagnostic sensor package that could be obtained from commercial sources. Environments being considered are: contamination, atomic oxygen, ionizing radiation, cosmic radiation, EMI, and temperature. This talk describes the requirements and rational for selecting these environments and reviews a preliminary design that includes a micro-controller data logger with data storage and interfaces to the sensors and spacecraft. If successful, such a sensor package could be the basis of a unique, long term program for monitoring the effects of the space environment on spacecraft systems.
Low Cost Environmental Sensors for Spaceflight: NMP Space Environmental Monitor (SEM) Requirements
An outstanding problem in spaceflight is the lack of adequate sensors for monitoring the space environment and its effects on engineering systems. By adequate, we mean low cost in terms of mission impact (e.g., low price, low mass/size, low power, low data rate, and low design impact). The New Millennium Program (NMP) is investigating the development of such a low-cost Space Environmental Monitor (SEM) package for inclusion on its technology validation flights. This effort follows from the need by NMP to characterize the space environment during testing so that potential users can extrapolate the test results to end-use conditions. The immediate objective of this effort is to develop a small diagnostic sensor package that could be obtained from commercial sources. Environments being considered are: contamination, atomic oxygen, ionizing radiation, cosmic radiation, EMI, and temperature. This talk describes the requirements and rational for selecting these environments and reviews a preliminary design that includes a micro-controller data logger with data storage and interfaces to the sensors and spacecraft. If successful, such a sensor package could be the basis of a unique, long term program for monitoring the effects of the space environment on spacecraft systems.
The DS1 hyper-extended mission
The Primary Mission for Deep Space (DS1) was to demonstrate 12 new technologies one of which was the Ion Propulsion System (IPS). After successfully completing its primary mission, DS1 was given a new mission. The objective of this Extended Mission was to fly by the Comet Borrelly. After the successful Borrelly encounter, the ion thruster on DS1 had to be operated for more than 14,000 hours in space. This provided a unique opportunity to investigate the condition of the thruster after long-term operation in space and determine, to the extent possible, if the thruster wear in space is consistent with that observed in long-duration ground tests.
Demonstration of the NSTAR ion propulsion system on the Deep Space One mission
This paper provides an overview of the system performance from the first 14,200 hours of ion propulsion system operation in interplanetary space.
Ultra fast plasma analyzer : an all-sky camera for charged particles
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The Mars Thermal Environment and Radiator Characterizations (MTERC) Experiment
Radiators will be used on Mars to reject excess heat from various processes and surfaces and will help temper the climate of any future manned habitats.
Three-Dimensional Particle Simulation Modeling of Ion Propulsion Plasma Environment for Deep Space One
A fully three-dimentional particle-in-cell simulation model was developed to obtain ion propulsion charge-exchange plasma environment over the entire downstream-to-upstream region for the Deep Space 1 (DS1) spacecraft.
Characteristics of the Spacecraft Local Environment During NSTAR Ion Propulsion System Operations on Deep Space One
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NSTAR Diagnostic Package (NDP) Architecture and Deep Space One (DS1) Spacecraft Event Detection
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NSTAR Diagnostic Package (NDP) Architecture and Deep Space One (DS1) Spacecraft Event Detection
The NDP measures contamination, plasma characteristics, electrical fields, and magnetic fields. This paper describes the NDP requirements, development process, and flight systems functionality.
NSTAR Ion Propulsion
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NSTAR Technology Validation Report
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NSTAR Technology Validation
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Initial Results from the DS1/IPS Diagnostics Sensors (IDS)
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Ion Propulsion Subsystem Environmental Effects on Deep Space 1: Initial Results from the IPS Diagnostics Subsystem
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Ion Propulsion Subsystem Environmental Effects on DS1: Initial Results from the IPS Diagnostics Subsystem
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