DocumentCode :
358974
Title :
Plasma Experiment for Planetary Exploration (PEPE) on DS1
Author :
Nordholt, Jane E. ; Young, David T. ; Funsten, Herbert O.
Author_Institution :
Los Alamos Nat. Lab., NM, USA
Volume :
7
fYear :
2000
fDate :
2000
Firstpage :
597
Abstract :
The Plasma Experiment for Planetary Exploration, PEPE, is a space plasma energy, angle, and mass/charge spectrometer now taking data aboard the Deep Space 1 (DS1) spacecraft. PEPE required several advanced technologies and specialized construction techniques to meet its targeted cost, schedule, mass, power, and volume reductions compared to previous plasma sensor packages such as the NASA Cassini mission Plasma Spectrometer. It was designed to validate technologies and techniques for these resource savings so that future plasma instrumentation can use fewer resources and continue to have frequent access to space. PEPE was also designed to monitor the effect that the ion engine on DS1 has on the spacecraft environment and determine the impact of ion engines on future scientific instrumentation and measurements. PEPE has produced both high quality data and science, fully demonstrating that its new technologies can produce a viable instrument compatible with an ion propelled spacecraft
Keywords :
astronomical instruments; astronomy computing; astrophysical plasma; ion engines; solar wind; space vehicle electronics; space vehicles; spectroscopy computing; time of flight mass spectrometers; COB electronics; Deep Space 1 spacecraft; Plasma Experiment for Planetary Exploration; advanced technologies; cost savings; ion engine effect; plasma sensor packages; resource savings; scientific instrumentation; solar wind; spacecraft environment; specialized construction techniques; top-hat analyzers; Costs; Engines; Instruments; Mass spectroscopy; NASA; Packaging; Plasma applications; Space charge; Space technology; Space vehicles;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Aerospace Conference Proceedings, 2000 IEEE
Conference_Location :
Big Sky, MT
ISSN :
1095-323X
Print_ISBN :
0-7803-5846-5
Type :
conf
DOI :
10.1109/AERO.2000.879327
Filename :
879327
Link To Document :
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