SPECIFIC IMPULSE VALUES FOR HYDROGEN AND RDX

Abstract

The purpose of this study is the parametric investigation of hydrogen and RDX as working materials in rockets propelled by contained nuclear explosions (Project HELIOS). Hydrogen, by virtue of its low molecular weight, is the prime working fluid of chemical rockets. RDX is a chemical explosive used in the construction of nuclear implosion devices. Chemically known as cyclomethylene-trinitramine or cyclonite, RDX has the empirical formula C3H6O6N6. A two-part computational program was carried out for each compound. The results are presented in graphic form. The results of the first of the program are presented in static form, i.e., by the conventional Mollier diagram, in which specific enthalpy is plotted against specific entropy, with cross plots of temperature, pressure, and molecular weight. The results of the second part are presented in dynamic form by a series of diagrams in which specific impulse is plotted against chamber pressure with chamber temperature and exhaust pressure as parameters. The specific impulse of hydrogen heated by a nuclear explosion, neglecting fission products, may then be obtained by taking a linear combination of properly weighted specific impulse values for hydrogen and RDX.

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1965
Accession Number
AD0464592

Entities

People

  • F. J. Krieger

Organizations

  • RAND Corporation

Tags

DTIC Thesaurus Topics

  • Air Force
  • Chemical Explosives
  • Explosions
  • Explosives
  • Fission Products
  • Government Procurement
  • Hydrogen
  • Materials
  • Molecular Weight
  • Nuclear Explosions
  • Propellants
  • Rdx
  • Rocket Propellants
  • Specific Impulse
  • Thermodynamic Properties
  • United States

Readers

  • Combustion science or combustion engineering.
  • Rocket Propulsion.