ENGINEERING PROPERTY DATA ON ROCKET PROPELLANTS

Abstract

The results of the fifth quarter year's effort of a 24-month program on the analytical and experimental characterization of the physical properties of selected liquid propellants are presented in three phases. In Phase I, a continuous review of the literature was conducted to ensure the acquisition and documentation of the latest possible propellant properties data for evaluation and possible inclusion into a propellant properties handbook. Phase II experimental efforts have resulted in the measurement of chlorine trifluoride vapor pressure in the high-temperature region and an estimation of critical properties; sonic velocity in chlorine trifluoride and chlorine pentafluoride under pressurized conditions; nitrogen gas solubility in chlorine pentafluoride; specific heat of saturated liquid chlorine trifluoride; thermal conductivity of MHF-5; and viscosity of chlorine pentafluoride. Phase III efforts included the evaluation and assembly of all data generated in Phases I and II, a curve fit of specific heat data on solid chlorine trifluoride, and a report of unpublished data on the normal boiling point of chlorine pentafluoride and chlorine pentafluoride storability.

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1967
Accession Number
AD0385671

Entities

People

  • J. F. Hon
  • K. J. Youel
  • M. T. Constantine
  • S. E. Rodriguez
  • W. Unterberg

Tags

DTIC Thesaurus Topics

  • Acquisition
  • Air Force
  • Computer Programs
  • Heat Energy
  • Liquid Propellants
  • Liquid Rocket Propellants
  • Materials Laboratories
  • Materials Testing
  • Measurement
  • National Security
  • Physical Properties
  • Propellants
  • Rocket Oxidizers
  • Rocket Propellants
  • Surface Tension
  • Test And Evaluation
  • Vapor Pressure

Readers

  • Business Analytics
  • Organic Chemistry
  • Rocket Propulsion.