Overview of Characteristics and Experiments in IPM Plasmatrons

Abstract

Characteristics of IPG series plasmatrons as well as there application for reentry simulation and testing of thermal protection materials are discussed in the presented paper on the basis of 35-years experience of Plasma Laboratory of IPM RAS. Successful application of plasmatrons for simulation of reentry conditions and testing of thermal protection materials is based on using of plasmatron's advantages such as purity of plasma flow, its high stability, excellent reproducibility as well as wide ranges of realized pressure and heat flux. Using of subsonic regimes together with plasmatron's ability for independent smooth regulation of regime parameters such as pressure and power injected in plasma make a plasmatron the most flexible and powerful instrument for simulation of thermochemical action of shock layer on the surface of descent space vehicle, especially when it is necessary to solve problems concerned radiative & convective heating and/or non-equilibrium heat transfer. To the present day long-term aging tests (up to 100 15-minutes testing cycles for one sample) in dissociated gas flow were fulfilled only using plasmatrons. Also there are discussed tests of ablative thermal protection materials, studies of thermo-chemical interaction between dissociated flows and reusable thermal protection materials as well as some %non-space)) applications of plasmatrons as deposition of diamond films and testing of industrial materials on heat shock.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 2000
Accession Number
ADP010736

Entities

People

  • A. N. Gordeev

Tags

Communities of Interest

  • Advanced Electronics
  • Energy and Power Technologies
  • Human Systems

DTIC Thesaurus Topics

  • Ablative Materials
  • Air Flow
  • Boundary Layer
  • Carbon Carbon Composites
  • Coatings
  • Fluid Dynamics
  • Heat Energy
  • Heat Exchangers
  • Heat Transfer
  • High Temperature
  • Measurement
  • Mechanical Properties
  • Spacecraft
  • Stagnation Point
  • Surface Temperature
  • Test Facilities
  • Thermodynamics

Readers

  • Aerospace Test and Evaluation
  • Computational Fluid Dynamics (CFD)
  • Thermal Physics or Thermal Science.

Technology Areas

  • Space
  • Space - Hall-Effect Thruster