PARTICLE PHASE THERMAL EMISSION OF ROCKET EXHAUST

Abstract

An analysis of particle continuum radiation was made. A small cesium-nitrate aluminum solid propellant rocket attached to an ICBM re-entry vehicle was studied in particular. This effort constitutes one part of an integrated effort to determine the radiative properties of the exhaust products of a rocket system associated with a hypervelocity vehicle. (Author)

Document Details

Document Type
Technical Report
Publication Date
Apr 24, 1962
Accession Number
AD0275413

Entities

People

  • J. Santomieri

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Aluminum
  • Emission
  • Energetic Materials
  • Materials
  • Particles
  • Propellants
  • Radiation
  • Rocket Exhaust
  • Solid Propellants

Fields of Study

  • Physics

Readers

  • Missile Defense Systems.
  • Rocket Propulsion.
  • Spectroscopy.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flight