Demonstrate the Feasibility of a Detection Method to Separate Neutral Particles from Charged Particles in the MeV/Nucleon Energy Range

Abstract

A breadboard model of a spacecraft borne instrument to measure the neutral atomic fluxes with energies between 1 to 10 Mev/nucleon has been designed and constructed. Differentiation between incident charged and neutral particles will be done by measuring the production rate of convoy electrons by the particles. Calculations indicate that convoy electron production rate is much larger for neutral hydrogen than it is for protons. Incident particles strike a thin carbon foil at the entrance aperture and the resulting convoy electrons are identified using a 180 degrees magnetic spectrometer with a micro channel plate detector at the focal plane. Incident beam particles pass through the spectrometer undeflected and are detected by a solid state detector. The instrument is designed to be tested at accelerator facilities with proton and neutral hydrogen beams. Neutral beams will be generated by a proton beam through a thin carbon foil and selecting the resulting neutral beam particles using a dipole bending magnet downstream of the foil. Keywords; Convoy electrons; Charged/neutral particle differentiation; Neutral particle beams; Space instrumentation.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1988
Accession Number
ADA201114

Entities

People

  • Bronislaw K. Dichter
  • Frederick A. Hanser

Tags

Communities of Interest

  • Energy and Power Technologies
  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Charged Particles
  • Classification
  • Detection
  • Detectors
  • Electrons
  • Focal Planes
  • Hydrogen
  • Magnetic Fields
  • Nucleons
  • Particles
  • Production
  • Production Rate
  • Proton Beams
  • Protons
  • Security
  • Spectrometers

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Nuclear and Radiation Engineering.
  • Plasma Physics.

Technology Areas

  • Directed Energy
  • Microelectronics
  • Microelectronics - Microelectromechanical Systems
  • Space
  • Space - Hall-Effect Thruster