THEORY OF ION COLLECTION BY A SUPERSONIC SOUNDING ROCKET IN THE D-REGION,

Abstract

Charged particle collection rates are derived in terms of free stream conditions for a supersonic, blunt-nosed sounding rocket with an electrode at the stagnation point. The analysis applies at altitudes below about 70 km. It is shown that then the electric field at the electrode is sufficiently high to dominate the particle collection, as is possible in practice at the higher altitudes, one obtains an expression for the collection rate which applies to a wide class of rocket geometries and is largely independent of flow effect. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1967
Accession Number
AD0660650

Entities

People

  • Ain A. Sonin

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Altitude
  • Charged Particles
  • Electric Fields
  • Electrodes
  • Flow
  • Free Stream
  • Geometry
  • Particles
  • Rockets
  • Sounding Rockets
  • Stagnation Point

Fields of Study

  • Physics

Readers

  • Astronomy and Astrophysics.
  • Fluid Dynamics.
  • Plasma Physics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight
  • Hypersonics - Hypersonic Flow