Atomic Velocity Distributions Out of Hydrogen Maser Dissociators

Abstract

Velocity distributions are determined for atoms effusing out of radio frequency discharge hydrogen dissociators, of the type used in hydrogen masers. This work was motivated by long-term reliability issues related to the possible use of masers as frequency standards on satellites. A primary issue is the maser's hydrogen budget, because many of the common failure modes of a maser involve either the hydrogen source or sink. Because the focusing properties of the state-selecting magnets are velocity dependent, the overall hydrogen budget will depend not only on the dissociation efficiency but also on the velocity distribution of the hydrogen atoms leaving the dissociation. Many times, that distribution has been tacitly assumed to be Maxwellian at wall temperature, but that assumption is not necessarily valid. Our measurements show the distributions to be much narrower than Maxwellian and to broaden as the hydrogen pressure in the dissociator increases. Operating the dissociator to yield a relatively narrow velocity distribution and using a state-selecting magnet well matched to that distribution may significantly improve the efficiency of hydrogen use by the maser. (jhd)

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Document Details

Document Type
Technical Report
Publication Date
Feb 15, 1990
Accession Number
ADA219500

Entities

People

  • B. Jaduszliwer
  • Y. C. Chan

Organizations

  • The Aerospace Corporation

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies
  • Space

DTIC Thesaurus Topics

  • Air Force
  • Angular Momentum
  • Atomic Beam Masers
  • Atomic Beams
  • Classification
  • Deflection
  • Detectors
  • Magnet Coils
  • Magnetic Fields
  • Magnetic Moments
  • Masers
  • Measurement
  • Physics Laboratories
  • Security
  • Space Systems
  • Standards
  • Total Angular Momentum

Fields of Study

  • Physics

Readers

  • Molecular Photonics/Laser Physics
  • Plasma Physics / Magnetohydrodynamics

Technology Areas

  • Space
  • Space - Hall-Effect Thruster