2007
DOI: 10.1007/s11214-007-9177-3
|View full text |Cite
|
Sign up to set email alerts
|

Plasma Experiment for Planetary Exploration (PEPE)

Abstract: The Plasma Experiment for Planetary Exploration (PEPE) flown on Deep Space 1 combines an ion mass spectrometer and an electron spectrometer in a single, low-resource instrument. Among its novel features PEPE incorporates an electrostatically swept field-ofview and a linear electric field time-of-flight mass spectrometer. A significant amount of effort went into developing six novel technologies that helped reduce instrument mass to 5.5 kg and average power to 9.6 W. PEPE's performance was demonstrated successf… Show more

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
14
0

Year Published

2008
2008
2018
2018

Publication Types

Select...
5
2
1

Relationship

1
7

Authors

Journals

citations
Cited by 24 publications
(14 citation statements)
references
References 20 publications
0
14
0
Order By: Relevance
“…Combined sensors (PEPE) option: The mass and power resources for the plasma package can be significantly reduced by adopting a combined EA capable of performing both the fast major species ion sampling and the relatively slower but detailed composition measurements. An example of such a sensor that could be modified and exploited is the PEPE (Plasma Experiment for Planetary Exploration, Young et al 2007) charged-particle spectrometer, flown onboard the Deep Space 1 mission, capable of simultaneously measuring and resolving the velocity distribution of electrons and ions and their mass composition. Modifying the electron analyser to detect ions (usually involving simple reversal of the voltage polarities) and optimising the instrument parameters for fast measurements of the major ion species would satisfy AXIOM's requirements and provide significant resource savings.…”
Section: Pointing Requirements and Configuration Needsmentioning
confidence: 99%
“…Combined sensors (PEPE) option: The mass and power resources for the plasma package can be significantly reduced by adopting a combined EA capable of performing both the fast major species ion sampling and the relatively slower but detailed composition measurements. An example of such a sensor that could be modified and exploited is the PEPE (Plasma Experiment for Planetary Exploration, Young et al 2007) charged-particle spectrometer, flown onboard the Deep Space 1 mission, capable of simultaneously measuring and resolving the velocity distribution of electrons and ions and their mass composition. Modifying the electron analyser to detect ions (usually involving simple reversal of the voltage polarities) and optimising the instrument parameters for fast measurements of the major ion species would satisfy AXIOM's requirements and provide significant resource savings.…”
Section: Pointing Requirements and Configuration Needsmentioning
confidence: 99%
“…Thus, many ESAs now incorporate electrostatic "deflector plates" on the exterior of the aperture. 1,3,5,12,25,34,36,40 Applying an electrostatic potential to the deflector plates steers the incoming beam of particles into the aperture, allowing the instrument to scan the sky without physically moving. The curved nature of the plates acts to pre-focus the particles entering the instrument, raising the focal point of the particles away from the detector.…”
Section: A Electrostatic Analyzer (Esa)mentioning
confidence: 99%
“…A “top hat” electrostatic analyzer [ Carlson et al ., ; Young et al ., ] provides a circularly symmetric field of view, allowing measurement of a full particle distribution function in half a spin. On a three‐axis stabilized spacecraft, additional electrostatic deflectors are required to cover the full range of phase space [e.g., Carlson et al ., ; Young et al ., ]. These detectors are typically symmetrically biased (one is positive, while the other is negative at the same voltage magnitude) using bipolar power supplies.…”
Section: Introductionmentioning
confidence: 99%