Detection of Interstellar Pickup Ions within our Solar System: New Instrument Concept

ORAL

Abstract

We discuss the importance of measuring the composition of the local interstellar medium. Composition measurements of the local interstellar medium pickup ions are confined to mass less than or equal to 20Ne+. It is desireable to extend the mass range up to 56Fe+ if not up to 84Kr+ which will require 2-3 stop coincidence designs. It's not clear the IMAP mission can detect pickup ions with mass > 20Ne+. At present most techniques are similar to the SWICS design, which uses a combination of energy/charge (E/Q) analyzer, post-acceleration VPA > |-15| kV for positive ion measurements, followed by time-of-flight (TOF) section to measure the ion's velocity to give the ion's mass/charge (M/Q). Then by combing the ion's M/Q and E/Q, and then using a solid ststae detector (SSD) to measure the ion's total energy E = (E/Q + VPA)*Q, allows one to separate ion's M and Q for high charge state solar wind ions with 2-stop detection. But for singly charged heavy ions with mass M ≥ 16 it's difficult to detect pulses from the SSD so only a single stop design is achieved. We're developing a Tandem Ion Mass Spectrometer (TIMS) (1 V ≤ E/Q ≤ 50 kV) composed of frontend which measures the ion's approximate E/Q and M/Q, followed by a post-acceleration VPA ~ -15 kV (i.e., ion E/M (keV/nucleon) is estimated) after which the ion enters TIMS 3-stop TOF unit (does not use SSD) where the ions mass resolution is increased (10 ≤ M/ΔM ≤ 60 at FWHM). With the ion approximate E/Q, M/Q and E/M provided by the frontend to the TOF unit, an algorithm that corrects for carbon foil induced ion scattering (path length changes) and energy straggling corrections can be made to make the TOF peaks narrower and boost the instruments mass resolution. In addition dE/dx effects can separate ions of similar M/Q and by making the TOF peaks narrower they can be separated. Finally, the 3-stop design allows for long integration times > years, so the only limiting factor for rare species is signal (i.e., instrument's maximum E/Q and its geometric factor). 

*NASA Goddard Space Flight Center Internal Research and Development funds for FY24 and FY25.

Publication: None at this time except for two non-provisional patents submitted by Goddard's patent office to the U.S. Patent Office.

Presenters

  • Edward C Sittler

    • NASA/GSFC/Geospace Physics Laboratory

Authors

  • Edward C Sittler

    • NASA/GSFC/Geospace Physics Laboratory
  • Marilia Samara

    • NASA/GSFC/Geospace Physics Laboratory
  • Robert G Michell

    • NASA/GSFC/Geospace Physics Laboratory
  • Adam J Schoenwald

    • NASA/GSFC/Instrument Electronics Development Branch Code 694
  • Timothy A Camerson

    • NASA/ADNET, Greenbelt, MD, USA
  • Long Nguyen

    • NASA/ADNET, Greenbelt, MD, USA
  • Albert Risco Patino

    • Catholic University of America, Washington, DC, USA
  • Alejandro Garcia Morilla

    • Catholic University of America, Washington DC, USA
  • Danjing Chen

    • Catholic University of America, Washington DC, USA
  • Dennis J Chornay

    • University of Maryland, College Park, MD
  • Emma R Mirizio

    • University of Maryland, College Park, MD, USA
  • Peter Wurz

    • University of Bern, Switzerland