MODIFICATION OF SUPERSONIC FLOW FIELDS UNDER NEAR SPACE CONDITIONS BY CRYOPUMPING.

Abstract

Results are presented of a test program designed to simulate an air sampling probe utilizing cryosurfaces cooled to liquid helium temperature to capture the impinging gas. Capture coefficients are given for the liquid helium cooled cryosurface under the conditions of normally directed low density gas flow from a Mach 3 nozzle for both clean, polished surfaces and surfaces coated with a thin film of paraffin. Also presented are the effects of micron-size particles in the gas on the cryopumping capabilities of the cryosurface. (Author)

Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1964
Accession Number
AD0601089

Entities

People

  • D. E. Anderson
  • J. A. Collins Jr.
  • W. D. Clement

Organizations

  • Arnold Engineering Development Complex

Tags

DTIC Thesaurus Topics

  • Alkanes
  • Coefficients
  • Cryopumping
  • Films
  • Flow
  • Flow Fields
  • Gas Flow
  • Low Density
  • Particles
  • Sampling
  • Supersonic Flow
  • Thin Films

Fields of Study

  • Physics

Readers

  • Aerosol Science/Aerosol Physics
  • Combustion and Flow Dynamics.
  • Surface Coatings Technology.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow
  • Space
  • Space - Hall-Effect Thruster