The Mushroom: A half‐sky energetic ion and electron detector

We present a time‐of‐flight mass spectrometer design for the measurement of ions in the ~30 keV to 10 MeV range for protons (up to ~40 MeV and ~150 MeV for He and heavy ions, respectively) and ~30 keV to 1 MeV range for electrons, covering half of the sky with 80 apertures. The instrument, known as the “Mushroom,” owing to its shape, solves the field of view problem for magnetospheric and heliospheric missions that employ three‐axis stabilized spacecraft, yet still require extended angular coverage; the Mushroom is also compatible with a spinning spacecraft. The most important new feature of the Mushroom is the method through which uncomplicated electrostatic optics and clean position sensing combine to permit many apertures to fit into a compact, low‐mass sensor head (or wedge), several of which (ideally eight) compose a full instrument. Most of the sensor head's volume is an empty, equipotential region, resulting in the modest 250 g mass of each 10‐aperture wedge. The Mushroom is capable of separating ion species across most of its energy range and angular field of view. For example, separation of the neighboring 3He and 4He isotopes is excellent; the full width at half maximum mass resolution has been measured to be 0.24 amu to 0.32 amu, respectively. Converting this to a Gaussian width σm in mass m, this represents a σm/m mass resolution better than 0.04. This separation is highly desirable for the flight program for which the first Mushroom was built, the Solar Probe Plus mission. More generally, we estimate the mass resolution to be σm/m ≈ 0.1, but this is energy, mass, and angularly dependent. We also discuss the solid‐state detector stack capability, which extends the energy range of protons and helium, with composition, to ~100 MeV.

[1]  Barry H. Mauk,et al.  The Jupiter Energetic Particle Detector Instrument (JEDI) Investigation for the Juno Mission , 2017 .

[2]  M. Lockwood,et al.  The Solar Probe Plus Mission: Humanity’s First Visit to Our Star , 2016 .

[3]  Edmond C. Roelof,et al.  Integrated Science Investigation of the Sun (ISIS): Design of the Energetic Particle Investigation , 2016 .

[4]  K. Nelson,et al.  The “Puck” energetic charged particle detector: Design, heritage, and advancements , 2016, Journal of geophysical research. Space physics.

[5]  M. R. Stokes,et al.  The Energetic Particle Detector (EPD) Investigation and the Energetic Ion Spectrometer (EIS) for the Magnetospheric Multiscale (MMS) Mission , 2016 .

[6]  George C. Ho,et al.  Radiation Belt Storm Probes Ion Composition Experiment (RBSPICE) , 2013, Space Science Reviews.

[7]  M. K. Lockwood,et al.  Solar Probe Plus: A mission to touch the sun , 2013, 2013 IEEE Aerospace Conference.

[8]  D. Lario,et al.  Estimation of solar energetic proton mission‐integrated fluences and peak intensities for missions traveling close to the Sun , 2011 .

[9]  George C. Ho,et al.  The Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) on the New Horizons Mission , 2007, 0709.4428.

[10]  G. T. Moore,et al.  The Pluto Energetic Particle Spectrometer Science Investigation (PEPSSI) on the New Horizons Mission , 2008 .

[11]  R. Ogliore,et al.  The Low-Energy Telescope (LET) and SEP Central Electronics for the STEREO Mission , 2008 .

[12]  Barry H. Mauk,et al.  The Energetic Particle and Plasma Spectrometer Instrument on the MESSENGER Spacecraft , 2007 .

[13]  S. M. Krimigis,et al.  Magnetosphere Imaging Instrument (MIMI) on the Cassini Mission to Saturn/Titan , 2004 .

[14]  R. McNutt,et al.  The Energetic Particles Spectrometers (EPS) on MESSENGER and New Horizons , 2003 .

[15]  A. Dell'Acqua,et al.  Geant4 - A simulation toolkit , 2003 .

[16]  Richard W. McEntire,et al.  Geotail energetic particles and ion composition instrument , 1994 .

[17]  S. Jaskulek,et al.  The Galileo Energetic Particles Detector , 1992 .

[18]  J. F. Mckenzie,et al.  The solar wind ion composition spectrometer , 1992 .

[19]  S. Krimigis,et al.  The Medium-Energy Particle Analyzer (MEPA) on the AMPTE CCE Spacecraft , 1985, IEEE Transactions on Geoscience and Remote Sensing.

[20]  W. I. Axford,et al.  The Low Energy Charged Particle (LECP) experiment on the Voyager spacecraft , 1977 .

[21]  F. Ipavich The Compton-Getting Effect for low energy particles , 1974 .