1 / 13

Simulation on Thermal Ion Mass Spectrometer for MIT mission

Simulation on Thermal Ion Mass Spectrometer for MIT mission. KONG Linggao. Background of MIT mission. Four satellites: ITA, ITB, MA, MB The Thermal Ion Mass Spectrometer will aboard on MA and MB. Specification requirements of TIMS . Design of the instrument. ESA

burian
Télécharger la présentation

Simulation on Thermal Ion Mass Spectrometer for MIT mission

An Image/Link below is provided (as is) to download presentation Download Policy: Content on the Website is provided to you AS IS for your information and personal use and may not be sold / licensed / shared on other websites without getting consent from its author. Content is provided to you AS IS for your information and personal use only. Download presentation by click this link. While downloading, if for some reason you are not able to download a presentation, the publisher may have deleted the file from their server. During download, if you can't get a presentation, the file might be deleted by the publisher.

E N D

Presentation Transcript


  1. Simulation on Thermal Ion Mass Spectrometer for MIT mission KONG Linggao

  2. Background of MIT mission • Four satellites: ITA, ITB, MA, MB • The Thermal Ion Mass Spectrometer will aboard on MA and MB

  3. Specification requirements of TIMS

  4. Design of the instrument • ESA • Inner hemisphere diameter:91mm • Outer hemisphere diameter:100mm • Toroidal geometry • TOF: • Flight length: 30mm • Carbon foil thickness: 11nm

  5. Simulation on ESA (1) • Energy range: • E=kV • 0.6eV~500eV • k~5.5 • 0.12V~90.9V • Energy resolution:~11.7%

  6. Simulation on ESA (2) • Focus property: • Focus point is ~10mm below the exit of ESA Top View Side View

  7. Simulation on ESA (3) • Elevation angle range: • ~8°

  8. Simulation on TOF (1) • Carbon foil simulation • SRIM • Ions energy before carbon foil: 15keV, single energy point • Carbon foil thickness: 11nm • H+ • O+

  9. Simulation on TOF (2) • Secondary electrons from carbon foil • Secondary electrons distribution from the carbon foil: • random • Energy range: 0~20eV • Angular distribution: 30° conic • It is better to determine the incident ions’ direction by the location of secondary electrons on start MCP

  10. Simulation on TOF (3) • Mass discrimination • Flight length:30mm • The input ion source for the time of flight is from the simulation results of carbon foil. • For heavier ions, some (<10%) will hit the wall of the TOF part • H+

  11. Comparison between requirements and simulation results • From the simulation point of view, the instrument design can meet the requirements. • More work need to do when it is put into practice…..

  12. For discussion • Serrated for ESA or not? • Not serrated for CASSINI mission for low energy ion measurement • Carbon foil • Gold blacking? • Surface charging • High voltage • Other issues……

  13. Thanks !

More Related