STUDY OF FORCES ON PROPELLANTS DUE TO HEAT TRANSFER INFLUENCING PROPELLANT TEMPERATURE IN A RECOVERY TYPE VEHICLE.

Abstract

Experimental equipment to measure the thermal conductivities of vapor mixtures was completely assembled with the necessary electrical controls. A detailed analysis of the effect of surface tension variation with temperature as it affects propellant orientation was completed. (Author)

Document Details

Document Type
Technical Report
Publication Date
Oct 31, 1962
Accession Number
AD0615616

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Conduction (Heat Transfer)
  • Conductivity
  • Contracts
  • Energy Transfer
  • Heat Transfer
  • Orientation (Direction)
  • Physical Properties
  • Propellants
  • Recovery
  • Surface Tension
  • Thermal Conductivity

Fields of Study

  • Physics

Readers

  • Rocket Propulsion.
  • Software Engineering
  • Thermal Physics or Thermal Science.